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OPERATION AND INSTALLATION MANUAL E-1500

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1. Obr zek 4 2 Sestava vrtule V508 E E AG Strana 4 6 17 1 2014 Figure 4 2 V508 E E AG Propeller assembly KONSTRUK N A PROVOZN INFORMACE 61 10 00 DESIGN AND OPERATION INFORMATION Page 4 6 2014 01 17 AVIA PROPELLER 1 1 Vrtulov list 2 32 Pouzdro 2 68 oup tko 1 2 Odmrazovac t leso 2 33 Vlo ka 2 69 Op rka 1 3 O krou ek 2 34 roub 2 70 Podlo ka 2 35 P ruba krytu 2 71 Pru ina 2 0 Vrtulovy n boj 2 36 Kol k 2 72 Rozp rn vlo ka 2 1 P st 2 37 Kol k 2 73 Pojistn krou ek 2 2 V lec 2 38 Pouzdro zadn 2 74 Reverzn nar ka 2 3 V kov lce 2 39 Vlo ka 2 75 O krou ek 2 4 Matice v lce 2 40 Kol k 2 5 Un e 2 41 Kol k 3 1 P edn kryt 2 6 Trubka 2 42 Pouzdro p edn 3 2 Zadn kryt 27 Vlo ka 2 43 Kol k 3 3 N tovac matice 2 8 Omezova ot ek 2 44 Podlo ka 3 4 N tovac matice 2 9 Obj mka 2 45 roub 3 5 N t 2 10 Op rny krou ek 2 46 roub 3 6 roub 2 11 Beta t hlo 2 47 Korunov matice 3 7 Podlo ka 2 12 Pouzdro listu 2 48 Podlo ka 2 13 K men 2 49 Z vla ka 7 1 P enosov kruhy 2 14 Podlo ka 2 50 roub nebo V ztu n krou ek 2 15 Pojistn krou ek 2 51 roub 7 2 Spojovac vodi 2 16 Vod tko un e e 2 52
2. ze krytu Spinner version 2 Obr zek 4 3 Sestava vrtule V508H Figure 4 3 V508H Propeller assembly Strana 4 8 17 1 2014 Page 4 8 KONSTRUK N A PROVOZN INFORMACE 61 10 00 DESIGN AND OPERATION INFORMATION 2014 01 17 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 1 1 Vrtulov list 2 34 Pojistn krou ek 2 70 Kol k 1 1 Blade 2 34 Snap ring 2 70 Pin 2 35 Matice 2 71 Matice 2 35 Nut 2 71 Nut 2 0 Vitulov n boj 2 36 roub 2 72 Cep 2 0 Hub 2 36 Screw 2 72 Pin 2 1 Matice v lce 2 37 roub 2 1 Gylinder nut 2 37 Screw 2 2 V lec 2 38 Pru ina 3 1 P edn kryt 2 2 Cylinder 2 38 Spring 3 1 Spinnerdome 2 3 P st 2 39 Pru ina 3 2 Zadn kryt 2 3 Piston 2 39 Spring 3 2 Spinner bulkhead 2 4 2 40 K men 3 3 Krou ek 2 4 Piston rod 2 40 Pitch change block 3 3 Ring 2 5 Un e 2 41 Podlo ka 3 4 Gumov pr chodka 2 5 Fork 2 41 Washer 3 4 Rubber ring 2 6 Vlo ka 2 42 Pojistn krou ek 3 5 N t 2 6 Insert 2 42 Retaining ring 3 5 Rivet 2 7 V ko v lce 2 43 Kuli ka 3 6 roub 27 Gylinder plate 2 43 Ball 3 6 Screw 2 8 Kol k 2 44 Vlo ka 3 7 Podlo ka 2 8 Pin 2 44 Spacer 3 7 Washer 2 9 Vod tko un e e 2 45 Pojistn podlo ka 2 9 Fork guide 2 45 Lock plate 2 10 Beta krou ek 2 46 roub 2 10
3. Horn d l svorkovnice Spodn d l vnice Obr zek 5 13 Odmrazov n typ C F MONT ELEKTRICK HO SB RA E Sb ra e 068 5320 076 5300 a 066 5300 1 P ed mont ov te voln chod v ech uhl k Stla te a uvoln te ka d uhl k a sledujte zda nedoch z k drhnut nebo blokov n uhl ku uvnit bloku 2 Instalujte sb ra na sk reduktoru motoru Pojist te v echny mont n rouby v i sob nerezov m dr tem 0 8 mm 0 032 inch 3 Ov te vzd lenost a hlovou polohu sb ra e v i p enosov m kruh m dle obr zku 5 14 1 Vzd lenost mezi sb ra em a p enosov mi kruhy mus b t 1 2 a 2 4 mm 0 047 a 0 095 inch a sb ra mus b t nato en pod hlem 2 k rovin kolm na m d n krou ky v i sm ru rotace p enosov ch kruh V p pad pot eby upravte polohu sb ra e na mont n konzole n sleduj cm zp sobem a Povolte dva rouby p ipev uj c sb ra k mont n konzole viz obr zek 5 15 b Upravte polohu sb ra e na konzoli tak aby byla dodr ena p edepsan vzd lenost a hlov poloha v i p enosov m kruh m dle obr zku 5 14 1 Strana 5 11 18 9 2014 MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL De icing system type C figure 5 13 Put the low
4. E 1500 INSTALLATION AND OPERATION MANUAL FOR PROPELLER V508 Min flight angle Min letovy hel BETA range BETA p smo Flight angle at BETA lamp on Propeller model Verze vrtule Letov hel p i rozsv cen Constant Z for calculation of amp 2 Governor type Lever Sv type dimension Y 2E 5 2 T Beta ring protrusion mo m 9 BRE mo m A at BETA lamp on Typ regul toru Typ p ky Sv Konstanta Z 9 g oo 2 8 o g Wo NOVO 5 2 j pro v po et rozm ru NA 5 e ow cem Deus wore e gt o Vysunut beta krouZku Y Lo LI 05 0 05 0 05 52 p i rozsv cen lampy Go ES L z2 co ES 329 29 Bv 8 S P9 54 233 ES s s SS 6 07 s 2 lt 0 s 2 z E 3 7 z 4 0 mm 0 1575 inch 15 10 8 8 0 1 mm 0 346 0 004 inch LUN7816 LUN7816 01 3 3 mm 0 13 inch 14 9 9 5 0 1 mm 0 374 0 004 inch 2 9 mm 0 114 inch 13 8 10 1 0 1 mm 0 398 0 004 inch 2 5 mm 0 0984 inch 12 7 10 8 0 1 mm 0 425 0 004 inch Hej 7 mm 0 2756 inch 15 10 8 8 0 1 mm 0 346 0 004 inch LUN7816 02 GA 6 3 mm 0 248 inch 14 9 9 5 0 1 mm 0 374 0 004 inch 5 9 mm 0 2323 inch 13 8 10 1 0 1 mm 0 398 0 004 inch 4 ROW1 0101 01 5 5 mm 0 2165 inch 12 7 10 8 0 1
5. Figure 7 5 V510 blade areas referring to Table 7 2 Maxim ln po et TENE nA say dle oprav pons Hate s obr zku 7 5 prendas ea jedn opravy proti sob od pi ky do 60 mm 1 1 5mm 10 mm od pi ky do 2 36 inch 0 2 inch 0 395 inch od 60 mm do 420 mm 5mm 7 5 mm od 2 36 inch do 16 5inch 2 0 2inch 0 295 inch od 420 mm do 720 mm 2 5 mm 4mm od 16 5 inch do 28 35 inch 1 0 1 inch 0 16 inch od 720 mm do konce profilu 0 1 1 2 mm i od 28 35 inch do konce profilu 0 047 inch Tabulka 7 2 P pustn m stn opravy na n b n a odtokov hran listu V510 Strana 7 8 NE 28 2 2012 UDRZBA 61 10 00 Maximum number Maximum Total plade of repairs depth of max depth measured Leadin Trailin single of opposite acc to Figure 7 5 pacing aing 9 ppe edge edge repair repairs from tip to 60 mm 1 1 5mm 10 mm from tip to 2 36 inch 0 2 inch 0 395 inch 60 mm to 420 mm 2 2 5mm 7 5 mm 2 36 inch to 16 5 inch 0 2 inch 0 295 inch 420 mm to 720 mm 1 1 2 5 mm 4mm 16 5 inch to 28 35 inch 0 1 inch 0 16 inch 720 mm to airfoil end 0 1 1 2 mm 28 35 inch to airfoil end 0 047 inch Table 7 2 Local repair allowable limits on the leading and trailing edge of V510 blade Page 7 8 MAINTENANCE 2012 02 28 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL c Postup opravy c Repair procedure 1 Pou ij
6. POZN MKA Zap n n a vyp n n elektrick ho obvodu mikrosp na em zkou ejte p kou Zv po sejmut nosi e kluzn ch kamen nebo ru n m p estavov n m vrtulov ch list s pomocn kem Ovl dac p ku vrtule v kabin letounu p itom nastavte do polohy prapor nosi kluznych kamen na p ce Zv z st v zapojen UPOZORN N LISTY PRI PRET EN UCHOPTE BL E KE KORENI NIKDY ZA PI KY c P esv d te se zda pri zp tn m pohybu do z kladn polohy po preru en elektrick ho obvodu je vrchol kluzn ho epu vzd len od patn plochy va ky 27 minim ln 0 1 mm 0 004 inch Je li tato v le men se i te ji areta n m roubem obr zek 11 20 o jeho hlavu se p ka op r Areta n roub pak pojist te dota en m matice d Bod zapnut elektrick ho obvodu v z vislosti na vysunut op rn ho krou ku vrtule se i te n sleduj c m zp sobem 1 Ru n m p estaven m vrtulov ch list vysu te beta krou ek vrtule ovl dac p ku vrtule v kabin letounu p itom nastavte do polohy prapor Beta krou ek nastavte dle tabulky 11 2 nebo 11 3 podle typu vrtule a v t to poloze vhodn zajist te 2 Okam ik zapnut elektrick ho okruhu se i te pouze nat en m va ky 27 po povolen zaji ovac ho roubku obr zek 11 20 UPOZORN N POD ZAJI OVAC M ROUBKEM JSOU DV PODLO KY Z NICH JEDNA JE P ROV
7. 11 34 ZKOU EN rho vL steer o 11 42 A Vrtulovy regul tor 7815 11 42 B Vrtulov regul tor 0 7816 11 48 DAL 11 52 A Vrtulovy regul tor LUN7815 11 52 B Vrtulov regul tor 7816 11 59 ODSTRA OV N Z VAD 11 61 POSTUPY UDRZBY Sie obo 11 63 SKLADOV N A KONZERVACE 11 70 OBSAH E 1500 11 9 11 10 11 11 61 10 00 INSTALLATION AND OPERATION MANUAL BASIC ADJUSTMENT AFTER INSTALLATION ON ENGINE Exif da AVS o to t edes 11 25 A Propeller governor LUN7815 11 25 B Propeller governor 7816 11 34 TESTING C mE EIS Bout eti b bitis 11 42 A Propeller governor LUN7815 11 42 B Propeller governor 7816 11 48 FURTHER ADJUSTMENT 11 52 A Propeller governor LUN7815 11 52 B Propeller governor LUN7816 11 59 TROUBLESHOOTING 2 x 11 61 MAINTENANCE PRACTICES 11 63 STORAGE AND PRESERVATION 11 70 TABLE OF CONTENT k AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Tato strana je z m rn pr zdn This page is intentionally blank Strana 1 4 Page 1 4 6 2 2012 OBSAH 61
8. c Ovl dac p ku vrtule v kabin pilota p estavte do polohy max ot ek p ka Rn je na dorazu max ot ek 15 d Povolte doraz praporu ovl dac p ky vrtule v kabin letounu asi o 3 mm 0 12 inch Povolte matici dorazu 16 a oto te j m o 2 a 2 5 ot ky ve sm ru hodinov ch ru i ek krok p ky Rn do praporov polohy se zv t f Presu te ovl dac p ku vrtule a na doraz 16 UPOZORN N POKUD Rn NEDOSEDNE NA SE IZOVAC DORAZ 16 JE POHYB P KY OMEZEN UVNIT REGUL TORU PODRZTE P KU Rn VT TO POLOZE A VRA TE DORAZ 16 ZP T A DOSEDNE NA EP P KY A NAV C JE T P L OTO KY ROUBEM ZP T g Upravte v li dorazu praporu ovl dac p ky vrtule v kabin letounu na 2 mm a zajist te h Doraz 16 zajist te v zac m dr tem i Funkci p ezkou ejte dle postupu v odd lu 11 7 j Se zen zapi te do atestu regul toru 4 Se zen ot ek volnob hu plat pro regul tory LUN7815 02 LUN7815 03 pouze dvoumotorov letouny a Se zen minim ln ho letov ho hlu volnob n ch ot ek se prov d dorazem 58 b Se zen prove te pouze v p pad kdy 1 rozd l volnob n ch ot ek vrtul je mimo p edepsanou toleranci 40 ot min Strana 11 56 6 2 2012 SYST M OVL D N VRTULE E 1500 INSTALLATION AND OPERATION MANUAL 3 Fea
9. Tube to feathering pum LUN 7840 Figure 11 8 Connection of LUN7880 and LUN7840 13 4 2010 SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM Page itia 2010 04 13 AVIA PROPELLER 23 Na p ku Bc v z kladn poloze ryska na p ce s va kou se kryje s ryskou min letov ho hlu na stupnici regul toru a ep ovl dac p ky se dot k dorazu obr zek 11 3 zapojte t hlo od ovl d n motoru a pojist te 24 Zapojte z suvku do mikrosp na e a pojist te 25 Prove te z kladn se zen regul toru dle postupu d le v t to kapitole B Vrtulov regul tor LUN7815 03 1 Zkontrolujte stav regul toru nesm b t viditeln po kozen 2 Zkontrolujte zda je na p ce Rn ustavena ta n pru ina obr zek 11 9 3 Zkontrolujte zaji t n v ech element obr zky 11 9 11 10 11 11 4 Zkontrolujte plomby a zaji t n obr zky 11 9 11 10 UPOZORN N V NUJTE ZV ENOU POZORNOST ZAJI T N PRVKU 32 OBR ZKY 11 10 A 11 11 V ZAC DR T A Z VLA KA LEV Z VIT JE OZNA EN ZNA KOU L ZAR KA OBR ZEK 11 10 NESM M T V ZAC DR T VEDEN P ES ELN PLOCHU ESTIHRANN HLAVY ROUBU ZAR KU NELZE POVOLOVAT A P ESTAVOVAT JE SE ZENA V ROBCEM REGUL TORU POZN MKA D ly t5 16 2 3 65 jsou se izovac regula n prvky 5 Sp kou Bc obr zek 11 9 v z kladn poloze ryska na p ce s va kou se kryje s ryskou minim
10. eee eee eee eee eee nan Supposed cause of overspeed if known u eee ee eee nene nn Strana 6 15 Page 6 15 6 2 2012 PROHLIDKY 61 10 00 INSPECTIONS 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL RECORD ON PROPELLER SUBJECT TO OVERTORQUE a overtorque note whether being indicated or estimated AIISDOBU code docere eati Flight Altitude a t re Overtorque tme os reco eame tort ttd ep Flight attitude during overtordle uec ec v xe ea un Ue Flight weight during overtorque ooooono nn on o nennen nennen Supposed cause of overtorque if known sse Strana 6 16 Page 6 16 6 2 2012 PROHLIDKY 61 10 00 INSPECTIONS 2012 02 06 AVIA PROPELLER 7 DRZBA Nen vy adov na dn ast dr ba proto e v echny pohybliv komponenty jsou uvnit vrtulov hlavy a nejsou vystaven vn j m vliv m Ulo en list a stav c mechanismus jsou maz ny pracovn m olejem b hem provozu vrtule Doporu uje se pouze ochrana vn j ho povrchu vrtulov hlavy dk m motorov m olejem nebo antikorozn m sprejem UPOZORN N AVIA PROPELLER D RAZN DOPORU UJE CHR NIT VHODNYM ZP SOBEM ULO EN LIST PROTI VNIKNUT VODY DO ULO EN NETYK SE HANG ROVAN CH LETOUN PRI PRUDK M POKLESU TEPLOT M E ZATE EN VODA ZMRZNOUT A LED ZDEFORMUJE T SN N UVNITR U
11. 20 Connect the control rod from engine to the lever Bc in its basic position guideline on the lever with cam is aligns with minimum flight pitch guideline on the governor scale and the control lever pin touching the stop figure 11 12 and secure 21 Connect plug to the beta switch and secure 22 Adjust the governor according to procedure in this section 11 5 GOVERNOR REMOVAL FROM ENGINE 1 Disconnect control rod from governor lever Bc 2 Disconnect control rod from governor lever Rn CAUTION DISCONNECT BOTH RODS ACCORDING TO INSTRUCTIONS IN ENGINE AND AIRCRAFT MANUAL 3 If feathering valve LUN7880 is enclosed disconnect tube from the governor to the valve 4 If feathering pump LUN7840 is enclosed disconnect the tube from the governor to the pump b Remove cotter pin washer and pin remove the carbon block assembly from lever Zv and from the beta ring 6 Disconnect connector of BETA range signaling circuit 7 Loose screws attaching the governor to the engine and remove with washers 8 Remove the governor CAUTION AVOID DAMAGE OF SLIP RINGS AND THE PROPELLER BULKHEAD Page 11 24 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 9 Pouze LUN7815 Pokud z stala torzn ty ka v h deli v reduktoru vyjm te ji a vlo te do h dele regul toru POZN MKA Torzn ty ka m m t vyzna eno slo demontovan ho regul toru 10 Na p rubu regul toru vlo te neporu en
12. 3 1 4 DESIGN AND OPERATION INFORMATION 4 1 5 INSTALLATION AND OPERATION INSTRUCTION 5 1 ABLE 51 BIals cs ce eR dis 5 1 B Spinner Dome Removal 5 2 Installing the Blades 5 3 D Installing the Propeller on the Engine 5 7 E De icing connection 5 10 F Brush block installation 5 11 G Spinner dome lt 5 12 H Basic adjustment after installation 5 12 CPC E ETE 5 13 J Propeller removal from engine 5 14 K Adjustment of minimum flight angle of model V508H 5215 L Instruction for Installing the Propeller V508H S N 070031 5 18 O INSPECTIONS i a aca rie PP eee qr e P ap nee 6 1 A Pre flight check 6 1 300 Hour Annual 6 2 C 900 Hour Two year 6 3 D Inspection 6 5 E 6 15 61 10 00 TABLE OF CONTENT Paged 2014 10 20 AVIA PROPELLER 7 URAD A tu da o 7 1 MI RR TT NUT DOL DO 7 1 B Dynamick 2 7 1 C Uskladn n provozovan vrtule
13. 7 3 DIEGO ai MER Pm 7 4 E V m na listu v 2 7 10 8 ODSTRA OV N 2 8 1 A B n oak REESE A 8 1 B PIADOFOVAI s toin aee Saee ode buda gt de l d 8 5 GO 2 uds Xue Ram 8 6 D Vrtule hlava listy VIA lk kN NA 8 7 9 DOPRAVA A 9 1 10 SPECI LN N AD uv voe oos peccet 10 1 11 SYST M OVL D N VRTULE 11 1 11 1 VOD a cmi hot adc o pujdes to o 11 2 A Obecn da st a 11 2 11 2 OMEZEN LETOV ZP SOBILOSTI 11 2 11 3 OVL D N VRTULE 22222 11 2 A Dod vka oleje 11 2 B Regulace ot ek 11 2 C Bela zen 5s xs Ste ee eU 11 5 D PIAPO OVAN opo ha ce ipia a ba d 11 5 11 4 MONT REGUL TORU NA MOTOR 11 8 A Vrtulov regul tor LUN7815 02 11 8 B Vrtulovy regul tor LUN7815 03 11 15 C Vrtulov regul tor LUN7816 11 19 11 5 DEMONT REGUL TORU Z MOTORU 11 24 ZE OBSAH E 1500 INSTALLATION AND OPERATION MANUAL 7 MAINTENANGE sad EUER EE eR ELS 7 1 ACS MT 7 1 B Dynamic 7 1 C Storage of serviced propeller 7 3 P Blade repalr eec eos ete es 7 4 E
14. Page 11 52 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER P ka Rn Doraz max ot ek 15 Obr zek 11 29 Se zen dorazu maxim ln ch ot ek Regul tor Vrtule Max ot ky LUN7815 02 V 508 2080 LUN7815 03 V 508Z 1900 Tabulka 11 4 Maxim ln ot ky vrtule 2 Ser zen praporov polohy plat pro regul tor LUN7815 02 E 1500 INSTALLATION AND OPERATION MANUAL Lever Rn Maximum X RPM stop lt d 15 Figure 11 29 Maximum RPM stop adjustment Governor Propeller Max RPM LUN7815 02 V 508 2080 LUN7815 03 V 508Z 1900 Table 11 4 Maximum propeller RPM 2 Feather position adjustment Se zen praporov polohy regul toru se prov d v sestav vrtulov ho syst mu s pomocn m erpadlem LUN7840 a Prov d se se zen m dorazu praporu 16 pokud zjist te e p ka Rn nedosahuje hlov p edepsan hodnoty INDIE v z stavb s praporovac m erpadlem Strana 11 53 13 4 2010 SYST M OVL D N VRTULE as p i pou it RU N HO PRAPOROV N p esahuje max hodnotu 8 s 61 10 00 for governor LUN7815 02 Governor feather position adjustment is performed with feathering pump LUN7840 installed It is performed with adjusting the feather stop 16 when The lever Rn doesn t reach angle position Time at MANUAL FEATHERING exceeds maximum val
15. byla aktualizov na P id na verze vrtule V508H kapitoly 3 4 5 6 P id ny informace o za tku kalend n ho TBO Kapitola Omezen letov zp sobilosti byla aktualizov na P id ny odkazy na Servisn bulletin 1 Strana 6 2 6 3 P id na tolerance p edepsan ch interval prohl dek Strana 6 15 Dopln na pozn mka e p i p eto en p ekro en krout c ho R 46 10 R 106 10 R 113 10 R 130 10 R 47 11 R 137 11 61 10 00 April 13 2010 June 30 2010 July 20 2010 September 3 2010 April 11 2011 May 10 2011 June 30 2011 December 6 2011 All 1 1 11 1 1 1 5 4 6 1 a 6 12 11 1 11 1 6 2 11 1 11 1 5 6 11 1 11 1 6 5 1 1 111 1 1 1 9 1 4 1 to 4 3 7 5 1 to 5 17 6 4 9 1 X 4 2 4 1 1 1 1 2 1 2 2 1 1 Il 2 1 1 6 2 6 3 6 15 6 17 to 6 20 9 1 11 48 LIST OF REVISIONS 2nd Issue Sections 4 5 6 7 9 11 was updated Chapter titles was changed due to changes in chapter Inspections Type of grease used to the blade thread was defined Section Inspections was completely updated Revision is signed only in beginning of the chapter Pre flight check Checking the propeller function after engine start up newly refers to Pilot Operating Handbook The same components for de icing type B and C may be alternatively used New tightening procedure of governo
16. B elektrick 28V DC 2 vyhr van sekce C elektrick 3x200V AC Vrtule pro ur itou kombinaci letoun motor je v dy definov na podle kombinace hlava listy kryt Aktu ln nastaven vrtulov ch list v z vislosti na typu letounu je uvedeno v z znamn ku vrtule TYPOV ZNA EN E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Propeller V510 Type series V510 T 9 A A 1 2 34 5 1 Hubtype 2 Hub modification blank z kladn verze AG AGRO version T aerobatic version 3 Propeller diameter in inches 4 Blade type according to certified hub blade combination 5 De icing A notinstalled B electrical 28V DC dual heating elements C electrical 3x200V AC The propeller for a certain aircraft engine combination is always defined according the hub blade spinner combination For the actual blade settings depending on the aircraft model the propeller logbook must be considered Page 3 2 MODEL DESIGNATION Boz AVIA PROPELLER 4 KONSTRUK N A PROVOZN INFORMACE Staviteln vrtule se skl daj z n sleduj c ch celk Vrtulovy n boj s ulo en m list Stav c mechanismus list Vrtulov listy Z va Vrtulovy kryt Odmrazov n voliteln Regul tor vrtule Olej POZN MKA Sledujte vyobrazen v t to kapitole pro konstruk n e en ur it vrtule Vrtulov n boj s ulo en m list Jednod ln vrtulov n boj je vyroben z oceli s kad
17. Celkov plocha v ech oprav nesm p es hnout 40 cm 6 2 square inch Opravy v ce listu mus b t od sebe vzd leny minim ln 40 mm 1 57 inch a jejich celkov ka nesm p es hnout polovinu ky listu v opravovan m m st Pr m r opraven ho m sta m b t 30 kr t v t ne jeho hloubka Vrtulov list V510 Do vzd lenosti 590 mm 23 2 inch od za tku profilov sti listu jsou p pustn vrypy a z seky do hloubky max 0 12 mm 0 005 inch kter nevy aduj opravu viz obr zek 7 2 Od vzd lenosti 590 mm 23 2 inch ke pi ce jsou p pustn vrypy a z seky do hloubky max 0 35 mm 0 014 inch kter nevy aduj opravu viz obr zek 7 2 ANCE NEPRESAHUJ C mm 0 014 inch JSOU TI PR PUSTN A NEVY ADUJ OPRAVU Strana 7 7 1 2015 Obr zek 7 2 Pr pustn po kozen na sac a tlakov stran listu V510 Opravy mo no prov d t do hloubky max 0 8 mm 0 032 inch ale ne v ce ne 10 procent tlou ky profilu v m st opravy Celkov plocha v ech oprav nesm p es hnout 30cm 4 65 sauare inch Opravy v ce listu mus b t od sebe vzd leny minim ln 40 mm 1 57 inch a jejich celkov ka nesm p es hnout polovinu ky listu v opravovan m m st Pr m r opraven ho m sta m b t 30 kr t v t ne jeho hloubka 3 DRZBA 61 10 00 E 1500 INSTALLATION AND OPERA
18. Follow the instructions from the eguipment manufacturers for dynamic balance If the dynamic imbalance is bigger than 1 2 ips the propeller must be removed from service and statically rebalanced 2 Inspection procedures prior to dynamic balancing a Visually inspect the propeller assembly after it has been reinstalled on the aircraft NOTE The first run up of a new or overhauled propeller assembly may leave oil on the blades and inner surface of the spinner dome This is normal and do not mean that it will be a continuing oil leakage Use a mild solvent to completely remove any oil from the blades or inner surface of the spinner dome b Prior to dynamic balance record the number and location of all balance weights from the static balance c Using of AN3 type bolts with self locking nuts for balancing is acceptable d All hole balance weight locations must take into consideration and must avoid any possibility of interfering with the adjacent airframe de icing and engine components 3 Placement of balance weights for dynamic balance a The preferred method of dynamic balance is to add the weights to the spinner bulkhead Subsequent removal of the dynamic balance weights if they exist will return the propeller to its original static balance condition The static balance weights are only allowed to remove exceptionally b Use only stainless washers or plated steel washers as dynamic balance weights podlo ky on th
19. INSTALLATION AND OPERATION MANUAL Figure 5 16 Adjustment of minimum flight angle of model V508H gaspom ZON YY approximately 1 turn E 2 turn 590 3 turn pum 1 turn ET 2 iurn RES 3 turn 590 Table 5 1 INSTALLATION AND OPERATION INSTRUCTION AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL b Vlo te veden pru iny s pru inou zp t na beta t hlo a zasu te do n boje b Put the spring guide with the spring back on the beta rod and insert to the hub 6 Namontujte kryc v ko zp t na vrtuli Ut hn te rouby a pojist te je v i sob 6 Install the cover cap back on the hub Tighten the screws and secure them nerezov m dr tem 0 8 mm 0 032 inch podle obr zku 5 17 against each other with 0 8 mm 0 032 inch stainless steel wire according to Figure 5 17 7 Stejn m zp sobem namontujte i ostatn kryc v ka 7 Install other cover caps in the same way Obr zek 5 17 Figure 5 17 Strana 5 17 6 2 2012 Page 5 17 MONT ZN A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION INSTRUCTION A AVIA PROPELLER L INSTRUKCE PRO INSTALACI VRTULE V508H S N 070031 POZN MKA Instalujte vrtuli na motor dle postupu uveden ho v e v t to kapitole p i dodr en informac a postup uveden ch v tomto odd lu 1 Pro zasunut beta krou ku k p rub vrtule je nutn u vrtule V508H S N 070031 pou t
20. K MEN ZP TN VAZBY d 5 Qr Stranov v le 0 15 0 18 mm H 0 006 0 007 inch p i instalaci Povoleno max 0 4 mm 0 016 inch ST CARBON BLOCK ASSY A GI Side clearance 0 15 to 0 18 mm 0 006 to 0 007 inch at installation Max 0 4 mm 0 016 inch permitted Obr zek 5 11 1 Figure 5 11 1 K MEN ZP TN VAZBY CARBON BLOCK ASSY BETA KROUZEK BETA RING r Stranov v le 0 025 0 05 mm 0 001 0 002 inch p i instalaci Povoleno max 0 25 mm 0 01 inch Side clearance 0 025 to 0 05 mm 0 001 to 0 002 inch at installation Max 0 25 mm 0 01 inch permitted Obr zek 5 11 2 Figure 5 11 2 Strana 5 9 3 TE Page 5 9 3 20 10 2014 MONT N A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E ZAPOJEN ODMRAZOVAC HO SYST MU Pro spr vn zapojen sledujte zna en kontakt Pou ijte rouby ozuben podlo ky pro rouby kontakt ploch podlo ky pro upev ovac rouby a ostatn komponenty dodan v robcem Postupujte dle instrukc uveden ch d le Odmrazovac syst m typ B1 obr zek 5 12 Um st te gumovou svorkovnici dle dr ek na obj mce a p ipojte kabel na odmraz t leso P ilo te plechov dr k a gumovou vlo ku a p ipevn
21. Propeller blades are made from aluminium alloy They are screwed into the blade bushings and secured by the clamps Connection with the pitch change mechanism is make through the pitch change blocks installed on the pins in the blade bushings faces Counterweights Propellers are equipped with counterweights designed as part of the clamps Force from counterweights assist to move the blades into the high pitch position and if oil supply lost from governor move the blades into the feather position Page 4 2 DESIGN AND OPERATION INFORMATION 2011 05 10 AVIA PROPELLER Z va Vrtule jsou vybaveny z va mi konstruovan jako sou st obj mek S la od z va pom h p estavovat vrtulov listy do velk ho hlu a dojde li k p eru en dod vky oleje od regul toru p estav vrtulov listy do praporov polohy Vrtulov kryt P edn i zadn kryt jsou vyrobeny ze slitiny hlin ku V pln na zadn m krytu zvy uj tuhost p edn ho krytu v m stech v ez pro listy Na zadn v ztuze jsou um st ny vyva ovac podlo ky Odmrazov n Vrtule m e b t vybavena syst mem odmrazov n vrtulov ch list Odmrazovac t lesa instalov na na vrtulov ch listech oh vaj listy a spole n s odst edivou silou a proud n m vzduchu pom haj odstra ovat n mrazu z povrchu list Sb rac krou ek a elektrick sb ra p iv d energii do odmrazovac ch t les p es kabely Sb rac krou ek je
22. figure 11 6 CAUTION DO NOT INSTALL THE GOVERNOR WITH THE CARBON BLOCK ASSEMBLY INSTALLED WHEN THE PROPELLER IS INSTALLED Page 11 22 SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM S 13 4 2010 AVIA PROPELLER 14 Pou ijte spr vn a ist t sn n Ustavte regul tor na reduktor motoru ozuben torzn ty inky mus zapadnout do n honu v reduktoru 15 P ipevn te regul tor ty mi rouby obr zek 11 7 p i pou it vnodn ho kl e Pru n podlo ka je pod hlavou roubu a dal podlo ka je vlo ena do vybr n v p rub regul toru sra en m dovnit Pojist te nejm n t i rouby nerezov m v zac m dr tem obr zek 11 7 16 Pokud vrtule nen v praporov poloze nato te listy do praporu tak aby beta krou ek dosedl na p rubu vrtule UPOZORN N m A VRTULOV LISTY UCHOPTE V KORENOV STI NIKDY NE U PI KY POZN MKA P ku Rn m ete p i p estavov n vrtulov ch list oto it k dorazu praporu 16 aby olej ze servomechanismu prot kal a nekladl odpor 17 Instalujte nosi kluznych kamen obr zek 11 6 na p ku Zv a na beta krou ek Na ep nosi e nasa te podlo ku a zajist te z vla kou 1 6x10 POZN MKA P i ka d instalaci pou ijte novou z vla ku 18 Pokud je instalov n elektrohydraulick ovlada LUN7880 a pomocn erpadlo LUN7840 postupujte n sledovn a Odjist te dut roub obr zek 11 8 a povo
23. 1 Z vrtule demontujte p edn kryt a U verz s p i roubovanou v ztuhou uvnit p edn ho krytu nevyj mejte p ipev ovac rouby p ibli n uprost ed v ky p edn ho krytu obr zek 5 1 Pokud do lo k demont i v ztuhy z p edn ho krytu vlo te v ztuhu zp t do p edn ho krytu podle zna en na d lech a znovu p ipevn te UPOZORN N TOTO NEPLAT PRO VRTULI V508H S N 070031 KDE JE V ZTUHA P IPEVN NA K VRTULOV HLAV U T TO VRTULE MUS B T ROUBY P IPEV UJ C V ZTUHU K P EDN MU KRYTU VYJMUTY JINAK NELZE DEMONTOVAT P EDN KRYT Z VRTULE U verz s p i roubovan mi v ztuhami na zadn m krytu v m stech vrtulov ch list nevyj mejte p ipev ovac rouby obr zek 5 1 Pokud do lo omylem k demont i v ztuh ze zadn ho krytu p ipevn te v ztuhy zp t podle zna en na d lech TYTO ROUBY NEDEMONTUJTE POKUD JSOU NEN LI STANOVENO JINAK X TYTO ROUBY DEMONTUJTE LN TYTO ROUBY gt NEDEMONTUJTE POKUD JSOU Obr zek 5 1 MONT N A PROVOZN INSTRUKCE E 1500 INSTALLATION AND OPERATION MANUAL B SPINNER DOME REMOVAL 1 Remove the spinner dome from the propeller a The screws at half of the spinner dome indicate that the front plate is 61 10 00 mounted inside Figure 5 1 Do not remove these screws to remove the spinner dome from the propeller However if the front plate has been removed reinstall it back
24. Po p estaven p ky ovl d n motoru se pooto vn j koaxi ln oup tko a pr tok koaxi ln mi oup tky se otev e Tlakov olej proud kan lem mal ho nebo velk ho hlu do vrtule obr zek 11 2B Kdy vrtule dos hne po adovan pozice dojde pohybem zp tn vazby od op rn ho krou ku k uzav en pr toku koaxi ln mi oup tky obr zek 11 2C D Praporov n Za letu m e p i vysazen motoru nastat pot eba zapraporov n vrtule Dvoumotorov letouny jsou obvykle vybaveny praporovac m syst mem s elektrohydraulick m ovlada em a praporovac m erpadlem Syst m se uv d do innosti z kabiny letounu nebo automaticky a Ru n praporov n Pilot stisknut m tla tka v kabin uvede do innosti praporovac erpadlo a p epne elektrohydraulick ovlada Ovlada propoj regula n obvod tak e olej z erpadla je veden p mo do vrtule a p estavuje listy na praporov hel innost praporovac ho erpadla je signalizov na v kabin kontroln rovkou Po restartu motoru a nastaven volnob hu dojde k odpraporov n vrtule Strana 11 5 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL C Beta mode of operation Beta mode of operation is used to decrease propeller thrust at taxiing or to set negative thrust after landing It allows to set any position between minimum flight pitch and maximum reverse at control of engine power
25. V POLOZE KDY EP KLOU E NA VRCHOLOV PLO E VA KY P EZKOU EJTE LEHCE PRSTEM RUKY ZDA LZE JE T P KOU SE SE IZOVAC M SROUBEM 88 ZATLA IT VE SM RU IPKY TLA TKO MIKROSP NA E D LE DO MECHANICK HO Strana 11 38 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL CAUTION Propeller manufacturer not allowed different flight angle setting from angles specified in tables 11 2 and 11 3 Figure 11 24 Rod 32 adjustment and securing 2 BETA range microswitch adjustment Perform when the propeller governor is installed the engine installation a Energize BETA range circuit in the aircraft cockpit NOTE During adjustment ask another person for assistance in the aircraft cockpit b Adjust the setting screw 38 on the lever contacting the microswitch such way that the microswitch switches on when the pin is 0 8 mm 0 0315 inch above the cam base 27 figure 11 20 This adjustment ensures correct microswitch switching at right pin position CAUTION WHEN THE JOURNAL IS SLIDING OVER THE PEAK SURFACE CHECK LIGHTLY WITH FINGER WHETHER IT IS STILL POSSIBLE TO PUSH THE LEVER WITH THE ELEMENT 38 IN THE DIRECTION OF THE ARROW THE PUSH BUTTON OF THE Page 11 38 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER DORAZU VOPACN M P PAD BY DO LO KPOSKOZEN MIKROSP NACE SERIZOVAC ROUB 38 ZAJIST TE MATIC
26. Z VAD A B ZNY PROVOZ Z vada Ot ky vrtule na volnob hu jsou vy ne po adovan Mo n p ina a V le mezi beta krou kem a kameny nosi e je v t ne 0 4 mm 0 016 inch b Po n vratu z reverzn polohy se BC p ka regul toru nevrac do z kladn polohy na rysku c Minim ln letov hel je nastaven na ni hodnotu d Vy v kon motoru na volnob hu N prava a Vym te nosi kluzn ch kamen na p ce zp tn vazby podle kapitoly Mont n a provozn instrukce v tomto manu lu b P ekontrolujte a se i te kinematick ovl d n motoru podle instrukc v robce motoru c Se i te minim ln letov hel Verze V508H kapitola Mont n a provozn instrukce v t to p ru ce Instalace s regul torem Jihostroj LUN7815 nebo LUN7816 kapitola Syst m ovl d n vrtule v t to p ru ce Instalace s regul tory jin ch v robc p ru ka v robce motoru nebo regul toru d Sni te pozemn volnob n v kon motoru dle instrukc v robce motoru Z vada Ot ky vrtule na volnob hu jsou ni ne po adovan Mo n p ina a Minim ln letov hel je nastaven na vy hodnotu b Ni v kon motoru na volnob hu N prava a Se i te minim ln letov hel Verze V508H kapitola Mont n a provozn instrukce v t to p ru ce Instalace s regul torem Jihostroj LUN7815 nebo L
27. a Po kozen t sn c krou ek mezi p rubou vrtule a motoru b Po kozen t sn c krou ek ve vod c m pouzdru beta krou ku N prava a Demontujte vrtuli z motoru a t sn c krou ek vym te b Vrtuli za lete k v robci nebo do autorizovan ho servisn ho st ediska Z vada Net snost v prostoru omezova e ot ek vrtule Mo n p ina a Po kozen t sn c krou ek pod omezova em N prava a Vrtuli za lete k v robci nebo do autorizovan ho servisn ho st ediska Z vada V le vrtulov ho listu Mo n p ina a Voln ulo en listu Velk v le stav c ho mechanismu N prava a Prove te kontrolu v l listu dle postupu v kapitole Prohl dky V p pad e v le p ekra uj povolen limity vrtule mus b t ihned sta ena z provozu a odesl na k v robci nebo do autorizovan ho servisn ho st ediska Strana 8 8 6 2 2012 ODSTRANOV N Z VAD E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Trouble Blade bearing leakage Probably cause a Defective sealing in the blade bearing Remegy a Send the propeller to manufacturer or authorized repair centre Trouble Leakage in the propeller flange area Probably cause a Defective o ring between propeller and engine flange b Defective o ring in the guide bushing of the beta ring Remegy a Remove the propeller from engine and replace the o ring b Send the propeller to manufacturer or aut
28. en letounu vrtule mus b t zkontrolov na v Avia Propeller nebo autorizovan m servisn m E 1500 INSTALLATION AND OPERATION MANUAL 4 Exposure to fire or heat Exposure to fire or extreme heat reguires the inspection of the propeller and engine mounted accessories manufactured by Avia at manufacturer or authorized service centre 5 Engine oil contamination Engine oil contamination reguires the inspection of the propeller and engine mounted accessories manufactured by Avia at manufacturer or authorized service centre 6 Hard landin The hard landing occurs when the airplane hits the ground with a greater speed and force than usual with no contact of the propeller with the ground a The hard landing within the load limit of the airplane does not require any action on the propeller b The hard landing above the load limit of the airplane requires inspection of the propeller in Avia Propeller or authorized repair center st edisku Strana 6 14 h Page 6 14 12 5 2015 PROHLIDKY 61 10 00 INSPECTIONS 2015 05 12 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL RECORD ON PROPELLER SUBJECT TO OVERSPEED vao overspeed note whether being indicated or estimated ode toe aree beca uote Flight Altitude oec a attis Overspeed nn Flight attitude during overspeed eo Flight weight during overspeed
29. eno vyhled n p iny niku POZN MKA U nov nebo nov opraven vrtule m e b hem prvn ch n kolika hodin provozu doch zet k m rn m nik m oleje co m e b t zp sobeno sed n m t sn n a rozst ikem maziva pou it ho p i mont i vrtule Tyto uniky oleje by m ly po p ibli n 10 hodin ch provozu ustat a P inou niku oleje je obvykle vadn t sn n Zkontrolujte vrtuli a zjist te zdroj niku Mo n zdroje niku oleje jsou vyobrazeny na obr zku 6 2 POHLED OD MOTORU VADN T SN N MEZI VRTULOVOU HLAVOU A MOTOREM VADN T SN N HYDRAULICK HO V LCE BETA TAHLA VADN T SN N VADN T SN N ULOZENI LISTU OMEZOVA E OT EK Obr zek 6 2 Mo n p iny niku oleje vyobrazena vrtule V508 POZN MKA Pokud je p inou niku oleje vadn t sn n mezi p rubou vrtule a p rubou motoru sejm te vrtuli z motoru a prove te v m nu vadn ho o krou ku za nov z n hradn ch d l vrtule V ostatn ch p padech kontaktujte Avia Propeller b V p pad e nebylo zji t no unik n oleje z d vodu vadn ho t sn n prohl dn te d kladn cel povrch vrtulov hlavy na v skyt trhliny Strana 6 6 30 6 2010 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 1 Grease or oil leakage CAUTION Do not clean the propeller parts It can complicate the detection of the sourc
30. pr zdn This page is intentionally blank Strana 111 2 13 4 2010 Page 111 2 P EHLED PLATN CH STRAN 61 10 00 LIST OF EFFECTIVE PAGES Koos AVIA PROPELLER 1 OMEZEN LETOV ZP SOBILOSTI Odd l Omezen letov zp sobilosti je schv len EASA dle Part 21A 31 a 3 a CS P40 b a 14 CFR Part 35 4 A35 4 Jak koliv zm ny z vazn ch Zivotnostn ch limit interval prohl dek a souvisej c ch postup uveden ch v tomto odd lu mus b t schv leny Odd l Omezen letov zp sobilosti je schv len FAA a obsahuje dr bu po adovanou dle 43 16 a 91 403 americk ch leteck ch p edpis FAR pokud nebyl FAA schv len alternativn program A Omezen ivotnosti 1 N kter d ly vrtule mohou m t stanoven limit celkov ivotnosti tzn Ze po dosa en stanoven ho po tu provozn ch hodin TSN Time Since New mus b t takov d l vym n n 2 V tomto odd lu jsou uvedeny d ly s omezenou ivotnost vrtul obsa en ch v t to p ru ce 3 Limit ivotnosti vrtulov ho listu nen nijak ovlivn n t m zda m i nem instalovan komponenty odmrazovac ho syst mu 4 Nen li v slovn uvedeno jinak jsou d le uveden limity ivotnosti d l shodn pro v echny verze vrtul a kombinace vrtule letoun motor 5 D ly s omezenou ivotnost vrtul ady V508 D l ivotnost List ostrea 15 000 hodin 2 000 hodin N boj 15 000 hodin 2 000 hodin Pouzdro
31. roub v ek beta t hel pokud jsou rouby zaji t ny Demontujte rouby a sejm te v ka z vrtule VAROV N V KA BETA T HEL JSOU PREDEPJATA PRU INAMI VE VRTULI P I DEMONT I P IDR UJTE V KO JEDNOU RUKOU PRO ZABR N N ZRAN N b Z vrtule vyjm te pru iny a veden pru in 2 Zav ste vrtuli na je b jak je pops no v e v t to kapitole V KO BETA T HLA Obr zek 5 8 MONT N A PROVOZN INSTRUKCE 61 10 00 CAUTION V508H PROPELLER S N 070031 REQUIRES A SPECIAL INSTALLATION PROCEDURE REFER TO THE END OF THIS CHAPTER 1 V508H propeller only To allow installing the mounting bolts the beta ring must be pulled toward the propeller mounting flange Refer to Figure 5 8 a Remove safety wire from cover caps screws if safety wired and remove cover caps from the propeller WARNING THE COVER CAPS ARE PRELOADED WITH THE SPRINGS IN THE PROPELLER TO AVOID INJURY HOLD THE COVER CAP WITH ONE HAND WHEN REMOVING THE SCREWS b Remove the springs and the spring guides from the propeller 2 Hang the engine on the hoist as described above in this chapter COVER CAP SPRING SPRING GUIDE Figure 5 8 Page 5 7 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 3 Z p ruby vrtule demontujte p epravn z tku POZN MKA P epravn z tka je p ipevn na k vrtuli rouby kter budou pou ity k uchycen vrtule na motor
32. v lce 2 39 Vlo ka 2 4 Matice v lce 2 40 Kol k 7 1 P enosov kruhy 2 5 Un e 2 41 Kol k nebo V ztu n krou ek 2 6 Trubka 2 42 Pojistn krou ek 7 2 Spojovac vodi 27 Vlo ka 2 43 Kol k 7 3 Poutko vodi e 2 8 Omezova ot ek 2 44 Podlo ka 7 4 roub 2 9 Obj mka 2 45 roub 7 5 Matice 2 10 Op rn krou ek 2 46 roub 7 6 Podlo ka 2 11 Beta t hlo 2 47 Korunov matice 7 7 Dr k vodi e 2 12 Pouzdro listu 2 48 Podlo ka 7 8 roub 2 13 K men 2 49 Z vla ka 7 9 Podlo ka 2 14 Podlo ka 2 50 roub 7 10 roub 2 15 Pojistn krou ek 2 51 roub 7 11 roub 2 16 Vod tko un e e 2 52 Pojistn podlo ka 7 12 Matice 2 17 Krou ek lo iska 2 53 roub 7 13 Svorkovnice 2 18 Kuli ka 2 54 Samojistn matice 7 14 Mezivlo ka 2 19 Separ tor kuli ek 2 55 Podlo ka 7 15 Vlo ka 2 20 Matice 2 56 O krou ek 7 16 Sestava sb ra e 2 21 roub obj mky 2 57 O krou ek 7 17 roub 2 22 Matice obj mky 2 58 T sn c man eta 7 18 Podlo ka 2 23 Z vla ka 2 59 O krou ek 2 24 roub 2 60 O krou ek 2 25 Podlo ka 2 61 O krou ek 2 26 Op rka 2 62 O krou ek 2 27 Pojistny krouzek 2 63 O krou ek 2 28 Pru ina 2 64 O krou ek 2 29 Pojistka 2 65 O krou ek 2 30 Pojistn podlo ka 2 66 Reverzn nar ka 2 31 ep 2 67 O krou ek Tabulka 4 1 Seznam d l k obr zku 4 1 Strana 4 5 6 2 2012 KONSTRUK N A PROVOZN INFORMACE E 1500 INSTALLATION AND OPERATION MANUAL 1 1 Blade 2 32 Bushing 3 1 Spinnerdom
33. vazby a beta krou kem a Pro vrtule pou vaj c beta krou ek typu L je p edeps na stranov v le mezi kamenem zp tn vazby a beta krou kem 0 15 0 18 mm 0 006 0 007 inch p i prvotn instalaci nov nebo opraven vrtule Obr zek 5 11 1 Maxim ln p pustn stranov v le je 0 4 mm 0 016 inch b Pro vrtule pou vaj c beta krou ek typu U je p edeps na stranov v le mezi kamenem zp tn vazby a beta krou kem 0 025 0 05 mm 0 001 0 002 inch p i prvotn instalaci nov nebo opraven vrtule Obr zek 5 11 2 Maxim ln p pustn stranov v le je 0 25 mm 0 01 inch Strana 5 9 2 20 10 2014 MONT N A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION MANUAL SEQUENCE A SEQUENCE B All models except V510T Step 1 Torque all bolts in sequence A to 35 45 Nm 25 33 Ib ft Step 2 Torque all bolts in sequence B to 95 100 Nm 70 74 Ib ft if installing on L410 aircraft 125 130 Nm 92 96 Ib ft if installing on other aircrafts Model V510T only Step 1 Torque all bolts in sequence A to 75 85 Nm 55 63 Ib ft Step 2 Torque all bolts in sequence A to 115 125 Nm 85 92 Ib ft Step 3 Torque all bolts in sequence B to 140 145 Nm 103 107 Ib ft Figure 5 11 12 Make sure the specified side clearance is established between the carbon block and the beta ring a For propeller models that use L Type beta ring the side clearance of 0 15 to 0 18 mm 0 006 to 0 007 inch
34. ABY V M NEVYPADLA KULICKA 92 5 16 Z HRDLA S TRYSKOU 44 A HLAVN ABY BYLA ZP T NAMONTOV NA Namontujte zp t ob hrdla 44 a 46 pozor na kuli ku 92 a dot hn te Na hrdlo s tryskou 44 p ipojte trubku 86 od pomocn ho erpadla LUN7840 8 je li instalov no a dot hn te jej matice na obou konc ch Strana 11 68 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Figure 11 36 Sealing ring replacement 6 Replacement of non return valve body sealing rings In case of leakage from the non return valve body replace sealing with following procedure Remove lock wire from tube cap nuts 86 figure 11 37 or the tube cap nut 87 or both Remove the tube 86 and 87 or both NOTE Before you will remove the tubes it is necessary to loose also the second end of the tube Replace the sealing ring 90 or 91 with new one after fitting 46 removal or the fitting 44 from the non return valve body CAUTION BE CAREFUL TO DON T LOOSE THE BALL 92 5 16 FROM THE FITTING 44 AND VERIFY WHETHER IT IS REINSTALLED Reinstall both fittings 44 and 46 and tighten be careful with ball 92 Connect tube 86 from the feathering pump LUN7840 8 if installed to the fitting 44 and tighten cap nuts on both ends Page 11 68 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Na hrdlo 46 p ipojte trubku 87 k ovlada i LUN7880 0 je li instalov n a dot hn te ji na obou konc ch matic
35. Blade replacement in the field 7 10 8 TROUBLESHOOTING AR a K U 8 1 A Normal 8 1 B bealliGrhg 8 5 GL does oro 8 6 D Propeller hub blades naana 8 7 9 SHIPPING AND 9 1 10 SPECIAL TOOL by aa ces Send ou 10 1 11 PROPELLER CONTROL 11 1 11 1 INTRODUGTION RR RR es RR 11 2 ANAT SU bi arua 11 2 11 2 AIRWORTHINESS LIMITATION 11 2 11 3 PROPELLER CONTROL esed kl we 11 2 P OI SUDDI dede Er eet VA 11 2 B OBPM GODIUUODL s 5 35 43 tenir n oka da id r v PODES 11 2 C Beta mode of 11 5 D 11 5 11 4 GOVERNOR INSTALLATION ON ENGINE 11 8 A Propeller governor 7815 02 11 8 B Propeller governor LUN7815 03 11 15 C Propeller governor LUN7816 11 19 11 5 GOVERNOR REMOVAL FROM ENGINE 11 24 61 10 00 TABLE OF CONTENT Pages S 2015 07 07 AVIA PROPELLER 11 6 11 7 11 8 11 9 11 10 11 11 Strana 1 3 6 2 2012 Z KLADN SER ZEN PO MONT ZI NA MOTOR een 11 25 A Vrtulovy regul tor LUN7815 11 25 B Vrtulov regul tor LUN7816
36. D KONTROLN POSTUPY POZN MKA V tomto odd lu jsou uvedeny kontroln postupy pro odhalen p in z vad zji t n ch b hem pravideln ch prohl dek dle odd l A a C vt to kapitole V n kter ch p padech jsou zde uvedeny postupy pro odstran n z vady Strana 6 5 11 4 2011 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 7 GOVERNOR COVER Figure 6 1 Overspeed governor test g Propeller speed in the 3rd to 5th cycle should not exceed 2000 RPM Possible propeller surging at the overspeed governor test is acceptable if the setting value of the governor will not be exceeded NOTE If propeller RPM during the test exceeded the value setting on governor governor must be replaced 7 Screw back the cover by hand until it stops and then tighten additionally by wrench about approx 5 degrees Safety the cover with stainless steel wire 8 Make an entry into the propeller log book to document this inspection D INSPECTION PROCEDURES NOTE This section contains inspection procedures to evaluate reason of troubles determined within inspections per sections A through C in this chapter In some instances the repair procedure is included Page 6 5 INSPECTIONS AVIA PROPELLER 1 Unik oleje nebo maziva UPOZORN N Neot rejte d ly vrtule Ot en m oleje m e b t zt
37. E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 3 Painting after repair Treat the repaired area to prevent corrosion Apply chemical conversion coating and finish coating as follows 1 Wipe the surface with acetone or MEK 2 Apply corrosion preventive coating Alodine 1200 or Alodine 1132 Touch N Prep to the bare aluminum surface Follow manufacturer s directions 3 Apply the finish coating Refer below for approved aerosol paints Tempo A 150 Epoxy Black Tempo A 151 Epoxy Gray Tempo A 152 Epoxy White CAUTION REPAIR PROCEDURES CAN ALTER PROPELLER BALANCE THAT MAY LEAD TO EXCESSIVE VIBRATIONS OF THE PROPELLER IN OPERATION THE DYNAMIC BALANCING OF THE PROPELLER MAY BE NECESSARY REFER TO DYNAMIC BALANCE SECTION IN THIS CHAPTER E BLADE REPLACEMENT IN THE FIELD 1 Remove the blade from the hub 2 Install the new blade into the hub per Installation and Operation Instruction section in this manual 3 The blades for each propeller are precisely matched Subsequent replacement of one or more blades in the field and setting the new blade in the same position as was the original blade can cause mismatch of the blades resulting in aerodynamic unbalance To prevent this follow these steps a Using the feathering pump move the propeller to the low pitch If the feathering pump is not installed start the engine and stop it with the propeller at the low pitch b Using a protractor measure the angle of all blades
38. IW IN 1 NOTE Specified value for RPM is only for information It depends on engine performance and atmospheric conditions Feathering pump heating leg pressure check only when the feathering pump is installed Move engine control lever to maximum continuous power position Feathering Pump is not lit IN I Page 11 45 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 g Kontrola funkce ovl dac p ky vrtule 9 1 Ovl dac p ka motoru v poloze max trval ho vykonu 2 Ovl dac p ku vrtule nastavte ot ky vrtule na 1900 ot min po ust len sni ujte ot ky ovl dac p kou vrtule na 1700 ot min a zp t do v choz polohy 3 Ot ky vrtule mus sledovat p estavov n ovl dac p ky vrtule v obou sm rech UPOZORN N KROUT C MOMENT NESM P EKRO IT 100 h Kontrola reverzn ch ot ek a reverzn ho v konu h 1 Ovl dac p ku vrtule nastavte do polohy max ot ek 2 Ovl dac p ku motoru nastavte na doraz volnob hu 3 P esu te ovl dac p ku motoru za doraz a pomalu a plynule sm rem do polohy max reverzu na dobu pot ebnou pro ode ten provozn ch hodnot ng nv Mk reverzn v kon podle zji t n ch hodnot kontrolujte podle provozn p ru ky motoru 4 B hem p echodu do reverzu kontrolujte rozsv cen signalizace BETA zen POZN MKA Reverzn ot ky se mus pohybovat v rozsahu 1880 2030 v rozmez okoln ch teplot 50 od 58 F do 1
39. b Engine has lower power at idle Remegy a Adjust minimum flight angle Model V508H chapter Installation and Operation Instructions of this manual Installation with governor Jihostroj LUN7815 or LUN7816 chapter Propeller Control System of this manual Installation with other governors instruction of engine of governor manufacturer b Adjust engine idle per instruction of engine manufacturer Page 8 1 TROUBLESHOOTING 2012 02 06 AVIA PROPELLER Z vada P kou ovl d n vrtule nelze m nit ot ky vrtule Mo n p ina a Rozpojen ovl d n voli e ot ek na regul toru b Nefunk n regul tor ot ek vrtule N prava a Zkontrolujte a opravte ovl d n voli e ot ek vrtule na regul toru dle instrukc v robce motoru b Vym te regul tor ot ek vrtule dle instrukc v robce motoru Z vada P estavov n vrtule prob h velmi pomalu Mo n p ina a N zk se zen reduk n ho ventilu v regul toru b Vadn regul tor vrtule c Vadn pry ov t sn c krou ky ve vlo ce vrtulov ho h dele motoru d Net snost rozvad e v motoru N prava a Zkontrolujte pop pad se i te tlak pod reduk n m ventilem dle instrukc v robce motoru b Vym te regul tor vrtule dle instrukc v robce motoru c Vrtuli demontujte z motoru p ekontrolujte t sn n vadn o krou ky vym te Postupujte dle kapitoly Mont n
40. dac p ka motoru do reverzn polohy nebo obr cen N prava Se i te axi ln v li prvkem B7 dle postupu v t to p ru ce Strana 11 62 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Trouble Leakage at turning screw of feedback body Probably cause a Defective sealing Remegy a Replace the sealing Trouble Axial clearance locking valve at rear cover increased in reverse position Probably cause a Engine control lever was moved to reverse position when propeller control lever was in feather position or vice versa Remegy a Adjust axial clearance with element 37 according to procedure in this manual Page 11 62 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 11 10 POSTUPY DRZBY V t to kapitole jsou pops ny postupy dr by a oprav spole n pro v echny modely regul tor LUN7815 a LUN7816 nen li uvedeno jinak 1 Myt a ist n NEPOU VEJTE ZA ZEN PRO TLAKOV MYT TLAKOV MYT M E ZP SOBIT ZATE EN VODY A NEBO MYC HO P PRAVKU DO P STROJE CO M E V ST KE KOROZI VNIT N CH KOMPONENT A NEBO NESPR VN FUNKCI P STROJE NEPOU VEJTE DN P PRAVKY NA B ZI RAVIN NEBO KYSELIN PRO MYT JAK KOLIV STI REGUL TORU P ED POU IT M KA D HO P PRAVKU SE UJIST TE E P PRAVEK NEM DN NEGATIVN INKY NA KOVOV POVRCHY A N T RY POHYB
41. ed op tovnou instalac vrtule na motor ot ete vn j povrch vrtule od oleje a postupujte dle kapitoly Mont n a provozn instrukce Strana 7 3 13 4 2010 k E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL c Do not exceed maximum weight per location of 25g This is approximately egual to six AN970 3 style washers d Weights are to be installed using aircraft guality 10 32 inch screws bolts Balance weight screws attached to the spinner bulkhead must protrude through the self locking nuts a minimum of one thread and a maximum of four threads All propellers which have been dynamically balanced must install a decal on blade no 1 This will alert repair station personnel that the existing balance weight configuration may not be correct for static balance f Record number and location of dynamic balance weights and static balance weights if they have been reconfigured in the Propeller Logbook C STORAGE OF SERVICED PROPELLER Remove the blades from the hub if the propeller is removed from the engine to be long term stored Wipe all visible parts of the hub and the blades to be dry and clean CAUTION Give attention to any propeller and blade portion be free from any moisture and or water Give special attention to the blade root Moisture or water in the blade thread and or centerbore causes the corrosion Such blade will be scrapped during overhaul Protect the propeller metal parts with thin film
42. ek 15 7 RPM stop 15 Ll Ta n pru ina a Spring Ovl dac e p Control TON Mikrosp na V lever A Microswitch V Doraz 5 etr eE Z k Connector volnob hu Idle sto P ka Sv Obr zek 11 12 Regul tor LUN7815 03 Pohled sm rem k motoru Figure 11 12 Governor LUN7816 View to engine UPOZORN N CAUTION V NUJTE ZV ENOU POZORNOST ZAJI T N PRVKU 32 OBR ZKY 11 13 A 11 14 V ZAC DR T A Z VLA KA LEV Z VIT JE OZNA EN ZNA KOU L POZN MKA D ly 15 16 a 32 jsou se izovac regula n prvky 5 S p kou Bc obr zek 11 12 v z kladn poloze ryska na p ce s va kou se kryje s ryskou minim ln ho letov ho hlu na stupnici regul toru a ep ovl dac p ky se dot k dorazu p ekontrolujte chod p ky Rn od dorazu 15 k dorazu 16 Strana 11 20 13 4 2010 SYSTEM OVLADANI VRTULE 61 10 00 BE CAREFUL AT SECURING ELEMENT 32 FIGURES 11 13 AND 11 14 LOCKING WIRE AND COTTER PIN LEFT THREAD IS MARKED WITH L NOTE Parts 15 16 and 32 are adjustable 5 With Bc lever figure 11 12 in basic position guideline on the lever with cam aligns with minimum flight pitch guideline on the governor scale and the control lever pin touches the stop verify Rn lever travel between stops and ej Page 11 20 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER P ka Bc Op rn krou e
43. isku vrtulov ho h dele a dodr te tuto polohu b hem cel ho se izov n e Mezi zar ku a dorazov ep sledovac p ky obr zek 11 15 vlo te m rku 1531 042 z n ad pro motor Je li v le mezi zar kou a dorazov m epem men a m rku nelze vsunout zkra te t hlo prvek 32 ot en m UPOZORN N A TAHLO ZKRACUJTE POUZE NAMONTOVANE NA REGULATORU TAHLO NESMI BYT ANI NA JEDNOM KONCI SEJMUTO Z PAKY f Pohybem sledovac p ky sev ete m rku 1531 042 a se i te d lku prvku 32 tak aby nosi kluzn ch kamen na p ce Zv p i zasunut m op rn m krou ku a povyta en vrtuli viz bod 4 nebyl jednostrann p itla en kluzn mi kameny k op rn mu krou ku Nosi kluzn ch kamen mus b t voln a axi ln v le mezi beta krou kem a kameny je p ibli n stejn na ob strany Beta krou ek Dorazov ep Sledovac p ka T hlo prvek 32 Obr zek 11 15 Se zen prvkem 32 Obr zek 11 16 V le beta krou ku Strana 11 26 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL c Remove lock wire at both ends of 32 securing both nuts to the rod and loose the nuts NOTE Left thread is marked with letter L d Pull the propeller using blade part as close as possible to blade shank in flight direction to eliminate axial play and k
44. kluznych kamen z p ky Zv obr zek 11 6 UPOZORN N NEINSTALUJTE REGUL TOR S NASAZENYMI KLUZNYMI KAMENY POKUD JE VRTULE INSTALOV NA NA MOTORU 17 Pou ijte spr vn a ist t sn n Ustavte regul tor na reduktor motoru ozuben torzn ty inky mus zapadnout do n honu v reduktoru Strana 11 12 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Safety rings 7 Carbon block Cotter pin holder Figure 11 6 Carbon block assembly 14 Verify governor flange and gear box flange Both surfaces must be clean and free from any damage Use a clean cloth eventually with cleaning solvent to wipe seating faces 15 Insert drive rod into the governor shaft with square inward figure 11 4 Try to turn with drive rod The rod should rotate freely CAUTION THE DRIVE ROD MUST BE IDENTIFIED WITH GOVERNOR S N 16 If the propeller is installed remove carbon block assembly from lever Zv figure 11 6 CAUTION DO NOT INSTALL THE GOVERNOR WITH THE CARBON BLOCK ASSEMBLY INSTALLED WHEN THE PROPELLER IS INSTALLED 17 Use correct and clean packing Place the governor onto engine gear box Drive rod gearing must be correctly inserted into the gear box drive Page 11 12 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 18 P ipevn te regul tor ty mi rouby obr zek 11 7 p i pou it vhodn ho kl e Pru n po
45. kozen uvnit vrtulov hlavy Jak koliv kontakt vrtule s ciz m objektem p i kter m dojde k viditeln mu po kozen vrtulov ch list mimo mal ch po kozen od kam nk vy aduje proveden gener ln opravy u v robce nebo v autorizovan m servisn m st edisku Strana 6 13 6 2 2012 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 2 Lightning strike In the event of a propeller lightning strike an inspection is required before further flight It may be permissible for a propeller to be operated for an additional 10 hours of operation if the propeller is not severally damaged For additional 10 hours of operation before propeller removal disassembly and inspection is necessary inspect the propeller according to following instructions a Remove the spinner dome and visually inspect the propeller spinner and de icing system for damage that would require repair before flight such as broken de icing wires or arcing damage to the propeller hub b Inspect the propeller blades for damage caused by the lightning strike c Check operation of the propeller de icing system d Regardless of the degree of damage make a log book entry to document the lightning strike CAUTION Regardless of the outcome of the inspection after 10 additional hours the propeller must be sended to manufacturer or authorized service centre for proper inspection 3 Foreign object strike Foreign object strike is any e
46. ln ho letov ho hlu na stupnici regul toru a ep ovl dac p ky se dot k dorazu 58 p ekontrolujte chod p ky Rn od dorazu 15 k dorazu 16 6 S p kou Rn na dorazu max ot ek p ekontrolujte chod p ky Bc ze z kladn polohy do reverzu kdy ryska na p ce s va kou je proti toleran n mu poli reverzu na stupnici regul toru Pot p estavte p ku Bc d le a na bezpe nostn doraz UPOZORN N Chod p ky Be nesm b t tuh Strana 11 15 13 4 2010 SYSTEM OVL DAN VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 23 Connect the control rod from engine to the lever Bc in its basic position guideline on the lever with cam is aligns with minimum flight pitch guideline on the governor scale and the control lever pin touching the stop 58 figure11 3 and secure 24 Connect plug to the beta switch and secure 25 Adjust the governor according to procedure in this section B Propeller Governor LUN7815 03 1 Verify governor condition for damage No damage acceptable 2 Verify installation of spring on the lever Rn figure 11 9 3 Verify locking devices of appropriate elements figures11 9 11 10 11 11 4 Verify seals and securing figures 11 9 11 10 CAUTION BE CAREFUL AT SECURING ELEMENT 32 FIGURES 11 10 AND 11 11 LOCKING WIRE AND COTTER PIN LEFT THREAD IS MARKED WITH L THE STOP FIGURE 11 10 MUST HAVE THE SAFETY WIRE ACROSS THE HE
47. n motoru a pojist te 21 Zapojte z suvku do mikrosp na e a pojist te 22 Prove te z kladn se zen regul toru dle postupu d le v t to kapitole 11 5 DEMONT REGUL TORU Z MOTORU 1 Odpojte t hlo od ovl d n motoru od p ky Bc regul toru 2 Odpojte t hlo od ovl dac p ky vrtule od p ky Rn regul toru UPOZORN N TORT ODPOJEN OBOU T HEL PROVEDTE PODLE POKYNU V PROVOZN PR RUCCE MOTORU A LETOUNU 3 Odpojte trubku vedouc od regul toru k ovlada i LUN7880 pokud je zapojen ve vrtulov m syst mu 4 Odpojte trubku vedouc od regul toru k praporovac mu erpadlu LUN7840 pokud je zapojeno ve vrtulov m syst mu 5 Sejm te z vla ku s podlo kou a ep nosi e kluzn ch kamen sejm te z p ky Zv a op rn ho krou ku nosi kluzn ch kamen 6 Odpojte z suvku signalizace BETA p sma 7 Povolte rouby p ipev uj c regul tor k motoru a s podlo kami je vyjm te 8 Uvoln te regul tor z centr e a sejm te z p ruby reduktoru UPOZORN N i DBEJTE ABY NEDO LO K POSKOZEN SB RAC CH KROU K A ZADN HO KRYTU Strana 11 24 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL e Verify whether the ball 5 16 is inside the fitting and tighten the nut Secure the connection with locking wire figure 11 12 19 Connect rod from RPM control system to the lever Rn figure 11 12 and secure
48. per Electric de icing system in this chapter O lt Inspect safety of mounting bolts If safety wire is loosen broken or if missing check correct torque of mounting bolts and safety the bolts with wire per nstallation on engine in this manual zl Install the spinner dome per Spinner dome installation in this manual 8 Make an entry into the propeller log book to document this inspection C 900 HOUR TWO YEAR INSPECTION NOTE Detailed inspection must be performed at 900 hour intervals of operation not to exceed 24 calendar months For possibility of flexible inspection schedule the required hour interval may vary plus minus 30 flight hours CAUTION 900 hour includes 300 hour inspection 1 Remove the spinner dome 2 Disconnect the electric de icing cables if de icing installed NOTE Observe visibility of position lines on the blade and bushing prior removing the blades Use the sharp needle to renew the lines as necessary 3 Remove the cotter pins loose the clamp bolts and remove the blades from the bushing 4 Thoroughly inspect the threads of all blades and blade bushings for corrosion For further operation is acceptable a Very light corrosion marks in the blade thread CAUTION Do not remove the corrosion marks in the blade thread with file grinder or any other tool Use only clean cloth to wipe the surface Page 6 3 INSPECTIONS 112130 AVIA PROPELLER b Stopy povrchov koroze v z vi
49. pokra ov n Table 10 1 Special tool cont d Page 10 3 Strana 10 3 L N M SPECIALNI NARADI 61 10 00 SPECIAL TOOLS 2014 10 20 20 10 2014 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Tato strana je z m rn pr zdn This page is intentionally left blank Strana 11 1 6 2 2012 Page 11 1 SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER 11 SYST M OVL D N VRTULE 11 1 VOD A Obecn Tato kapitola je zam ena pouze na instalace kde je pro ovl d n vrtule pou it regul tor Jihostroj P N LUN7815 nebo LUN7816 Informace o ovl d n vrtule s regul torem Avia jsou uvedeny v Provozn a mont n p ru ce Avia E 1707 Informace o ovl d n nastaven a dal informace o instalac ch s regul tory jin ch v robc jsou uvedeny v p ru ce v robce motoru 11 2 Zru eno 11 3 OVL D N VRTULE A Dod vka oleje Regul tor ot ek se skl d z olejov ho erpadla a d c sti Olejov erpadlo zaji uje dod vku tlakov ho oleje pro pr ci vrtule Skl d se ze zubov ho erpadla a pojistn ho ventilu kter udr uje tlak na v stupu z erpadla na po adovan rovni B Regulace ot ek Regulace ot ek znamen udr ov n ot ek vrtule na konstantn hodnot Zaji uje ji regul tor vrtule kter porovn v skute n ot ky s navolen mi a vhodn prestavuje vrtulov listy Princip reg
50. provozn ch Ih t nebo v konov ch limit m e zp sobit nespr vnou funkci vrtule V robce nebo autorizovan servisn st edisko nenesou dnou odpov dnost za kody zp soben nedodr en m instrukc nebo postup uveden ch v tomto manu lu SERVISN DOKUMENTACE U ivatel je odpov dn za udr ov n platn ho stavu t to p ru ky dle vyd van ch zm n Platn revize t to p ru ky je voln k dispozici na www aviapropeller com Na t chto str nk ch jsou uvedeny servisn dopisy bulletiny a rady souvisej c s vrtulemi v tomto manu lu POZN MKA Ilustrace obr zky a v kresy v tomto manu lu slou pouze jako p klad zobrazovan ho objektu a nemohou b t pova ov ny za z vazn pro jak koliv typ vrtule nebo jej st Z RUKA Z ru n podm nky pro ka dou vrtuli jsou stanoveny v kupn smlouv D KUJEME E JSTE SI VYBRALI V ROBEK AVIA PROPELLER dn udr ovan v m zaru mnoho let spolehliv ho provozu E 1500 INSTALLATION AND OPERATION MANUAL ATTENTION FOR OWNERS USERS AND SERVICE STAFF This installation and operation manual contains descriptions technical informations and instructions for operation and maintenance of V508 and V510 propeller type series All activities associated with propellers operation and maintenance must be practices according to this manual Activities exceeding scope of this manual shall be practices only by manufacturer or authorized service
51. t leso 2 37 Ball 2 76 O krou ek De icer 2 37 Ball 2 76 O ring 2 38 Vod tko un e e 2 77 O krou ek 2 38 Fork guide 2 77 O ring 2 0 Vrtulovy n boj 2 39 Pru ina 2 78 O krou ek 2 0 Hub 2 39 Spring 2 78 O ring 2 1 P st 2 40 Podlo ka 2 79 O krou ek 2 1 Piston 2 40 Washer 2 79 O ring 2 2 V lec 2 41 Deska 2 80 O krouzek 2 2 Cylinder 2 41 Plate 2 80 O ring 2 3 V ko v lce 2 42 Pouzdro pru iny 2 81 T sn c man eta 2 3 Cylinder plate 2 42 Spring bushing 2 81 Sealing 2 4 Kol k 2 43 Pojistka 2 82 O krou ek 2 4 Pin 2 43 Lock piece 2 82 O ring 2 5 Matice v lce 2 44 Pojistka 2 83 O krou ek 2 5 Cylinder nut 2 44 Lock piece 2 83 O ring 2 6 Un e 2 45 Matice 2 84 O krou ek 2 6 Fork 2 45 Nut 2 84 O ring 2 7 Pouzdro predn 2 46 Sroub 2 85 O krou ek 2 7 Front bushing 2 46 Screw 2 85 O ring 2 8 Pouzdro zadn 2 47 roub 2 8 Back bushing 2 47 Screw 2 9 roub 2 48 Kol k 3 1 P edn kryt 2 9 Screw 2 48 Pin 3 14 Spinnerdome 2 10 Vlo ka 2 49 Pr rubovy roub 3 2 Zadn kryt 2 10 Liner 2 49 Flange bolt 3 2 Spinner bulkhead 2 11 Trubka 2 50 Podlozka 3 3 N tovac matice 2 11 Tube 2 50 Washer 3 3 Nutplate 2 12 Vlo ka 2 51 Prf ruba krytu 3 4 N tovac matice 2 12 Insert 2 51 Spinner flange 3 4 Nutplate 2 13 2 52 Kol k 3 5 N t 2 13 Pin 2 52 Pin 3 5 Rivet 2 14 Omezova ot ek 2 53 Pouzdro 3 6 roub 2 14 Overspeed governor 2 53 Bushing 3 6 Screw 2 15 Obj mka 2 54 roub 3 7 Podlo ka 2 15 Clamp 2 54 Screw 3 7 Washer 2
52. te v echny d ly pomoc roub s podlo kami k obj mce P ed uta en m roubu vlo te mezi obj mku a dr k vlo ku Upev ovac rouby maj rozd lnou d lku krat roub pou ijte spole n s vlo kou Pojist te rouby nerezov m dr tem 0 8 mm 0 032 inch V AS Dm h k a MY Z N Kabel S S IN 0 Disk Vlo ka Svorkovnice Obr zek 5 12 Odmrazov n typ Odmrazovac syst m typ B2 P ipojte kabel k odmrazovac mu t lesu rouby s ozuben mi podlo kami rouby pojist te barvou Odmrazovac syst m typ B P ipojte kabel k odmrazovac mu t lesu rouby s ozuben mi podlo kami rouby pojist te barvou POZN MKA Od z 2010 mohou b t alternativn pou ity shodn komponenty s odmrazov n m C V takov m p pad postupujte dle mont n ch instrukc na dal stran Strana 5 10 6 2 2012 MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL E DE ICING CONNECTION See the contacts marking for right connection Use the screws toothed washers for contacts screws plane washers for fixing screws and other components delivered by manufacturer Follow instructions shown below De icing system type B1 figure 5 12 Put the rubber terminal board in line with grooves on the clam
53. v t to p ru ce 2 Pokud je na motoru instalov n elektrick sb ra p ed instalac vrtule ho demontujte jinak m e doj t k jeho po kozen 3 P ed instalac vrtule na motor demontujte k men zp tn vazby z p ky regul toru MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL INSTALLATION AND OPERATION INSTRUCTION GENERAL CAUTION DO NOT STAND THE PROPELLER ON THE BETA RING OTHERWISE IT MAY BE DAMAGED LEADING TO INCORRECT FUNCTION OF THE BETA SYSTEM REMOVE THE SHIPPING PLUG FROM PROPELLER MOUNTING FLANGE AFTER IS HANGED ON THE CRANE FOR INSTALLING ON ENGINE 1 Install the propeller on the engine with a suitable hoist and lifting slings WARNING THE HOIST AND SLINGS MUST BE RATED UP TO 200 KG 440 LBS CAUTION TAKE CARE NOT TO DAMAGE THE DE ICERS IF INSTALLED ON THE BLADES FROM THE SLINGS WHEN LIFTING THE PROPELLER a When installing the propeller on engine before installing the blades use a special hanger screwed into one of the blade bushing Refer to Special Tool chapter of this manual 2 Remove the brush block if installed from the engine before installing the propeller otherwise it could be damaged 3 Remove the carbon block from the beta linkage before installing the propeller on the engine Page 5 1 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 Strana 5 2 20 10 2014 AVIA PROPELLER DEMONT Z PREDN HO KRYTU VRTULE
54. zac m dr tem obr zek 11 3 22 Na p ku Rn zapojte t hlo od ovl dac p ky vrtule obr zek 11 3 a pojist te LUN 7880 T leso zp tn ho ventilu Hrdlo Dut roub Kuli ka 5 16 s tryskou m D ac ASSISI S NE OH PRES nay N D erpadlu Trubka k S DS S Matice LUN 7840 Obr zek 11 8 P ipojen LUN7880 a LUN7840 Strana 11 14 INSTALLATION AND OPERATION MANUAL a Remove locking wire on the turning screw figure 11 8 and loose it Loose tube at the valve LUN7880 and tube from the auxiliary pump LUN7840 at the engine wall b Connect the tube from valve LUN7880 to the fitting with arrow and lightly tighten CAUTION Arrow on non return valve must point up as shown on the figure Keep tubes clean C Connectthe tube from the auxiliary pump LUN7840 to fitting marked with T with ball 5 16 inside and lightly tighten d Tighten the turning screw at synchronous tightening of tube connections CAUTION The turning screw must not get jammed thread in the governor could be damaged e Verify whether the ball 5 16 is inside the fitting and tighten the nut Secure the connection with locking wire figure 11 3 22 Connect rod from RPM control system to the lever Rn figure 11 3 and secure LUN 7880 T M Tube to feathering valve 2 Zm h PZZZON RA vi p ANA AAO ka C222 2 Ra 2
55. zen mikrosp na e BETA p sma Strana 11 35 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Lever Bc pw Minimum fligth lt A pitch guideline L DA Figure 11 23 Lever Bc basic position b Remove lock wire at both ends of 32 securing both nuts to the rod and loose the nuts left and right thread c Find dimension X in the governor documentation d Add to the dimension X appropriate constant Z tables 11 2 or 11 3 for specific propeller type so the final dimension will be Y X Z mm CAUTION The Y value has not to be less than 1 9 mm 0 075 inch for governors LUN7816 and LUN7816 01 with lever P N 1535 002 NOTE With lever Sv P N 1535 002 the adjustment of minimum flight angle is not possible in all range of angles according to tables 11 2 and 11 3 because the Y value has not be less than 1 9 mm 0 075 in ch Therefore the replacement of governor lever Sv P N 1535 002 by lever P N 4 ROW1 0101 01 is possible Replacement must be carried out by person authorized by propeller engine or governor manufacturer After replacement the new governor version LUN7816 02 must be signed in the ID plate CAUTION After replacement of lever Sv the BETA range microswitch must be adjusted Page 11 35 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER PRO VRTULI V508
56. zky 11 3 11 4 11 5 POZN MKA Zaji t n dut ho roubu matic trubek hrdel a uzav rac matice obr zek 11 8 prove te a po mont i trubek 4 Zkontrolujte plomby a zaji t n obr zky 11 3 a 11 4 UPOZORN N V NUJTE ZV ENOU POZORNOST ZAJI T N PRVKU 32 OBR ZKY 11 4 A 11 5 V ZAC DR T A Z VLA KA LEV Z VIT JE OZNA EN ZNA KOU L ZAR ZKA OBR ZEK 11 4 NESM M T V ZAC DR T VEDEN P ES ELN PLOCHU ESTIHRANN HLAVY ROUBU ZAR KU NELZE POVOLOVAT A P ESTAVOVAT JE SE ZENA V ROBCEM REGUL TORU E 1500 INSTALLATION AND OPERATION MANUAL b Automatic feathering Action is similar to manual feathering only the activation is automatic based on engine torque evaluation Usually the automatic system is limited to some engine condition lever range Automatic feathering is indicated by a lamp in the cockpit the circuit can be Switched off c Emergency Feathering It is used when the feathering pump is out of operation or it is not installed Emergency feathering is activated by moving the propeller condition lever onto feather stop Blades are forced into feather position by counterweights moment and eventually by oil pressure Feathering time is about three times longer than manual and automatic feathering Emergency feathering can be used at engine stop 11 4 GOVERNOR INSTALLATION ON ENGINE A Propeller Governor LUN7815 02 1 Verify governor condition
57. 042 p itla te lehce nosi kluzn ch kamen k jedn stran op rn ho krou ku obr zek 11 16 a celkovou v li zm te listov mi m rkami Setting at minimum flight angle Nastaven min letov ho hlu 15 Only Pouze V508D AG with blades s listy 84 99A 99B All models V echny verze with blades s listy 106 12 Tabulka 11 1 Nastaven min letov ho hlu vrtul ady V508 s regul torem LUN7815 SYST M OVL D N VRTULE E 1500 CAUTION INSTALLATION AND OPERATION MANUAL TOTAL CLEARANCE BETWEEN BETA RING AND CARBON BLOCKS FIGURE 11 16 IS 0 15 0 18 mm 0 006 0 007 inch NOT LESS MAXIMUM OPERATION ACCEPTABLE CLEARANCE IS 0 4 mm 0 016 inch g Measure total clearance as follows Without gage 1531 042 press lightly the carbon block assembly to one side of the beta ring figure 11 16 and measure the total clearance using feeler gauge Po kone n m se zen a zm en v le u nosi e kluzn ch kamen dot hn te ob h After adjustment and clearance measurement tighten both nuts of the rod 32 and matice t hla 32 a pojist te doporu en m v zac m dr tem secure with lock wire Beta ring protrusion at minimum flight angle Vysunut beta krou ku p i nimim ln m letov m hlu 4 5 mm 0 177 inch BETA range BETA p smo Flight angle Beta ring protrusion at BETA lamp on at BETA lamp on Letovy hel pri rozsv cen Vysunut b
58. 1 2 Il 5 1 1 5 11 1 7 5 7 10 7 11 11 17 R 103 15 July 07 2015 LIST OF REVISIONS Page 4 3 Added missing change bars from previous changes and corrected date of the page Page 4 11 Item 2 81 was corrected in table 4 4 english text only Page 5 8 Added caution regarding tightening the blade clamp Page 5 11 6 10 Added brush block assy P N 066 5300 Page 5 11 1 Added checking the brush block after installing Page 5 12 The figure 5 14 2 from page 5 11 1 Pages 5 1 to 5 9 3 Updated installation procedure on engine Pages 5 18 5 19 Special procedure for installing the propeller S N 070031 Page 10 3 Updated list of tools Added procedure after hard landing Updated Shipping and storage Updated Brush block installation section Added Blade replacement in the field 7 5 11 17 Typo corrections Page II 5 2015 07 07 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL This page is intentionally blank Tato strana je z m rn pr zdn Strana 11 6 Page 11 6 18 9 2014 SEZNAM ZM N 61 10 00 LIST OF REVISIONS 2014 09 18 AVIA PROPELLER Page Cover 1 1 1 2 1 3 1 4 11 1 1 2 Il 3 Il 4 Il 5 Il 6 11 1 1 2 1 1 1 2 2 1 2 8 3 1 3 2 4 1 4 2 4 3 4 4 4 5 4 7 4 8 Strana 111 1 7 7 2015 P EHLED PLATN CH STRAN Date of Rev 2015 07 07 2014 10 20 2015 07 07 2012 02 06 2012 02 06 2011 12 06 2012 02 06 2012 02 06 2014 01 17 2015 07 07 2014 09 1
59. 11 11 STORAGE AND PRESERVATION 1 Preservation of governor removed from the engine It is necessary to preserve the governor removed from the engine Use following procedure First wipe outer surfaces with clean brush using clean suitable cleaner WARNING TAKE CARE WHEN THE SURFACE IS CLEANED TO DON T ENTER CLEANER INTO THE GOVERNOR THROUGH GOVERNOR FLANGE AROUND COAXIAL VALVES 18 19 LOCKING VALVE 35 AND INTO THE MICROSWITCH HOUSING 23 DON T DEGREASE ROD BEARINGS 29 32 AND 65 LEVER Sv 66 TRACE AND LEVER CAMS 34 AND ALSO CARBON BLOCK ASSEMBLY PINS 22 Coat outer surfaces except painted ones with preservation oil using a brush Record the preservation to the governor documentation Page 11 70 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 2 Skladov n regul toru 2 Storage of the governor Regul tor skladujte v ist m stnosti bez agresivn ch v par dob e v tran s teplotou The governor prepared for storage at user store only in a clean room without aggressive vzduchu 10 30 50 86 F a relativn vlhkosti vzduchu do 70 Regul tory skladujte na vapors well ventilated at ambient temperature 10 30 50 86 F and humidity to 70 reg lech nebo na pap rov ch sk n ch Mezi jednotliv mi regul tory ponechte odpov daj c Store the governors at shelves or boxes Ensure free access to each one prostor POZNAMKA Storing on floor is not
60. 16 Beta krou ek 2 55 roub 2 16 Beta ring 2 55 Screw 2 17 Beta t hlo 2 56 Matice 7 1 P enosov kruhy 2 17 Beta rod 2 56 Nut 7 1 Slip ring assy 2 18 Matice 2 57 Z vla ka nebo V ztu n p ruba 2 18 Nut 2 57 Cotter pin or Spacer ring 2 19 Podlozka 2 58 Pojistn podlozka 7 2 Sestava kabelu 2 19 Washer 2 58 Lock washer 7 2 Cable assy 2 20 Z vla ka 2 59 roub 7 3 Uzem ovac vodi 2 20 Cotter pin 2 59 Screw 7 3 Earthing wire 2 21 Pouzdro listu 2 60 roub 7 4 Poutko vodi e 2 21 Blade bushing 2 60 Screw 7 4 Gable clip 2 22 K men 2 61 Pojistn podlo ka 7 5 roub 2 22 Pitch change block 2 61 Lock washer 7 5 Screw 2 23 Podlo ka 2 62 Pouzdro 7 6 Samojistn matice 2 23 Washer 2 62 Bushing 7 6 Selflocking nut 2 24 Pojistny krouzek 2 63 oup tko 7 7 Podlo ka 2 24 Retaining ring 2 63 Slide valve 7 7 Washer 2 25 Cep 2 64 Op rka 78 roub 2 25 Pin 2 64 Support 7 8 Screw 2 26 Vn j krou ek 2 65 Podlo ka 7 9 Pojistn podlo ka 2 26 Outer ring 2 65 Washer 7 9 Lock washer 2 27 Krou ek lo iska 2 66 Pru ina 7 10 Spodn svorkovnice 2 27 Bearing ring 2 66 Spring 7 10 Low terminal board 2 28 Matice 2 67 Rozp rn vlo ka 7 11 Horn svorkovnice 2 28 Nut 2 67 Spacer 7 11 Upper terminal board 2 29 Pojistny krouzek 2 68 Pojistn krou ek 7 12 Dr k vodi e 2 29 Lock ring 2 68 Retaining ring 7 12 Cable holder 2 30 Pojistn podlo ka 2 69 roub 7 13 roub 2 30 Lock washer 2 69 Screw 7 13 Screw 2 31 Klec lo iska 2 70 Samojistn matice
61. 2 CAUTION THE O RING PREVENTS MOISTURE TO PENETRATE INTO THE THREAD THE CORROSION OF THE BLADE AND OR BLADE BUSHING THREAD MAY RENDER THE PROPELLER UNAIRWORTHY Slightly lubricate the thread and end portion of the blade shank with Aeroshell Grease 5 or 6 Figure 5 2 CAUTION DO NOT LUBRICATE CYLINDRICAL PORTION OF THE BLADE FROM END OF THE THREAD TOWARD THE TIP MAKE SURE THAT THIS SURFACE IS DRY BEFORE INSTALLING THE BLADE INTO THE HUB Page 5 3 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL DO NOT LUBRICATE THIS SURFACE TENTO POVRCH NEMAZAT SLIGHTLY LUBRICATE THE THREAD AND END PORTION LEHCE NAMAZAT Z VIT A KONEC LISTU POZI N RYSKA LISTU s P d O KROUZEK LISTU Obr zek 5 2 Figure 5 2 5 pln za roubujte list po sm ru hodinov ch ru i ek do pouzdra listu Pot 5 Fully screw the blade clockwise into the blade bushing Then observe position zkontrolujte pozi n rysky na ko enu listu a na hran pouzdra listu a oto te list marks on the blade shank and on the edge of the blade bushing and turn the v pouzdru zp t tak aby rysky byly proti sob obr zek 5 3 blade back so that both marks are opposite to each other Figure 5 3 Obr zek 5 3 Figure 5 3 Strana 5 4 20 10 2014 Page 5 4 MONT N A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER 6 Nastavte obj mku
62. 4 O ist te p rubu vrtule a p rubu motoru rozpou t dlem nebo benz nem Oba povrchy mus b t such a ist UPOZORN N ZABRA TE KONTAKTU ROZPOU T DLA S O KROU KY 5 Na p rubu motoru instalujte o krou ek dodan s vrtul obr zek 5 9 UPOZORN N NEPOU VEJTE O KROU EK Z P EPRAVN Z TKY 6 Pouze dvoj inn vrtule Ov te e na vlo ce v p rub motoru jsou instalov ny dva o krou ky obr zek 5 9 O KROU EK VRTULE L O KROUZEK VRTULE O KROU KY MOTORU JEDNO INN APLIKACE DVOJ INN APLIKACE Obr zek 5 9 7 Zarovnejte otvory pro kol ky v p rub vrtule proti kol k m v p rub motoru a opatrn nasu te vrtuli na p rubu motoru Strana 5 8 20 10 2014 MONT N A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION MANUAL 3 Remove the shipping plug from propeller engine flange NOTE The shipping plug is attached to the propeller with mounting screws that will be used for attaching the propeller to the engine 4 Clean the propeller and engine mounting flange with solvent or gasoline Both surfaces must be dry and clean CAUTION AVOID CONTACT OF SOLVENT WITH THE O RINGS 5 Install the propeller o ring onto the engine flange Figure 5 9 CAUTION DO NOT USE THE O RING FROM SHIPPING PLUG 6 Dual acting application only Make sure the two engine o rings are installed in the insert in engine flange Figure 5 9 P
63. 6 1 Otherwise push the spring support and release several times b Install the spinner dome c Start and warm up the engine according to the flight manual Cycle the propeller condition lever from minimum flight angle to feather at least three times to purge air from propeller hydraulic system e Move the propeller condition lever to maximum RPM f Move the engine condition lever slowly to RPM corresponding to overspeed governor action RPM no further increased approx 1950 RPM then increase the power by approx 296 generator speed Repeat this operation five times The propeller condition lever is in maximum RPM Page 6 4 INSPECTIONS 2012 02 06 AVIA PROPELLER OMEZOVACE Obr zek 6 1 Zkou ka omezova e ot ek g Ot ky vrtule nesm p i t et m a p t m cyklu p ekro it hodnotu 2000 ot min P padn kol s n ot ek p i funkci omezova e je p pustn za p edpokladu e ot ky nep ekro uvedenou hodnotu POZN MKA Pokud b hem zkou ky ot ky vrtule p ekro uvedenou hodnotu mus b t omezova ot ek vym n n Kontaktujte Avia Propeller J Na roubujte v ko omezova e ru n na doraz a pot dot hn te kl em o dal ch cca 5 Pojist te v ko nerezov m dr tem 8 Provedte z znam o proveden prohl dce do z znamn ku vrtule
64. 81 Ib ft Only if non self locking nuts are used at installation safety the nuts with 0 81 mm 0 032 inch stainless steel safety wire two nuts per safety Decompress the beta system and remove the puller from the propeller after is installed on the engine Page 5 18 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Obr zek 5 18 Figure 5 18 Obr zek 5 19 Figure 5 19 Strana 5 19 20 10 2014 Page 5 19 MONT ZN A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER 6 PROHL DKY UPOZORN N M m VE KER DEMONT N MONT N OPRAV RENSK POSTUPY MOHOU PROV D T POUZE OSOBY S P SLU NOU KVALIFIKAC POZN MKA T PROHL DKY UVEDEN V T TO KAPITOLE NENAHRAZUJ PROHL DKY UVEDEN V P RU K CH V ROBC LETOUNU A MOTORU A P EDLETOV PROHL DKA POZN MKA P edletov prohl dka se prov d p ed ka d m letem 1 Prohl dn te vrtulov listy na v skyt vrub z sek mechanick ho opot eben trhlin a koroze Zji t n z vady mus b t p ed dal m letem odstran ny p slu n kvalifikovanou osobou Postupujte dle kapitoly Udr ba v t to p ru ce 2 Zkontrolujte povrch list a krytu na zn mky deru blesku V p pad n lezu nebo podez en postupujte dle odd lu Uder blesku v t to kapitole POZN MKA Zn mkou deru blesku m e
65. A PROVOZN INSTRUKCE 5 1 Ar Obecn az ce x d ata 5 1 B Demont p edn ho krytu vrtule 5 2 Instalace vrtulov ch list 5 3 D Instalace vrtule na 5 7 E Zapojen odmrazovac ho syst mu 5 10 F Mont elektrick ho sb ra e 5 11 G Mont krytu 5 12 Z kladn nastaven po instalaci 5 12 I IZKOUSODI eot atri dee aee a na ae a ed 5 13 J Demont vrtule z 5 14 K Se zen minim ln ho letov ho hlu verze V508H 5 15 L Instrukce pro instalaci vrtule V508H S N 070031 5 18 6 tetto ode 6 1 A P edletov prohl dka 6 1 B 300 hodinov Ro n prohl dka 6 2 C 900 hodinov Dvoulet prohl dka 6 3 D Kontroln 6 5 E Speci ln prohl dky A soku tee RUE TENES QUU 6 15 1 OBSAH E 1500 INSTALLATION AND OPERATION MANUAL TABLE OF CONTENT LIST OF REVISIONS dn e ecu Il 1 LIST OFEFFEGTIVE PAGES seu b LAA Ab baba Ill 1 1 AIRWORTHINESS LIMITATION 1 1 2 GENERAL s zna NEN O aeris ot 2 1 3 MODEL DESIGNATION
66. Beta ring 2 46 Screw 2 11 Beta t hlo 2 47 roub 2 11 Beta rod 2 47 Screw 2 12 V ko 2 48 Podlo ka 2 12 Cover cap 2 48 Washer 2 13 Nastavovac matice 2 49 roub 2 13 Adjusting nut 2 49 Screw 2 14 Podlo ka 2 50 Podlozka 2 14 Washer 2 50 Washer 2 15 Podlo ka 2 51 Matice 2 15 Washer 2 51 Nut 2 16 Pru ina 2 52 roub 2 16 Spring 2 52 Screw 2 17 Veden pru iny 2 53 Matice 2 17 Spring guide 2 53 Nut 2 18 V ko pru iny 2 54 Podlo ka 2 18 Spring cover 2 54 Washer 2 19 Veden pru iny 2 55 Prf rubovy roub 2 19 Spring guide 2 55 Flange bolt 2 20 Pouzdro listu 2 56 Podlozka 2 20 Blade bushing 2 56 Washer 2 21 P ruba 2 57 O krou ek 2 21 Flange 2 57 O ring 2 22 Kol k 2 58 O krou ek 2 22 Pin 2 58 O ring 2 23 Kol k 2 59 O krouzek 2 28 Pin 2 59 O ring 2 24 Obj mka 2 60 Podp rny krouzek 2 24 Clamp 2 60 Backup ring 2 25 roub obj mky 2 61 Vod c krou ek 2 25 Clamp bolt 2 61 Guide ring 2 26 Matice obj mky 2 62 O krou ek 2 26 Clamp nut 2 62 O ring 2 27 Z vla ka 2 63 O krou ek 2 27 Cotter pin 2 63 O ring 2 28 Kol k 2 64 O krou ek 2 28 Pin 2 64 O ring 2 29 Zadn pouzdro 2 65 O krou ek 2 29 Back bushing 2 65 O ring 2 30 Vod c pouzdro 2 66 O krou ek 2 30 Guide bushing 2 66 Screw 2 31 Krou ek lo iska 2 67 T sn c man eta 2 31 Bearing ring 2 67 Sealing 2 32 Pouzdro beta t hla 2 68 Beta k men 2 32 Beta rog guide 2 68 Beta block 2 33 Vlo ka 2 69 Pojistn krou ek 2 33 Insert 2 69 Tabulka 4 3 Seznam d l k
67. Energize BETA range circuit in the aircraft cockpit NOTE INSTALLATION AND OPERATION MANUAL During adjustment ask another person for assistance in the aircraft cockpit b Adjust the setting screw 38 on the lever contacting the microswitch such way that the microswitch switches on when the pin is 0 8 mm 0 0315 inch above the cam base 27 figure 11 20 This adjustment ensures correct microswitch switching at right pin position CAUTION WHEN THE JOURNAL IS SLIDING ON THE CAM PEAK CHECK LIGHTLY WITH FINGER WHETHER IT IS STILL POSSIBLE TO PUSH THE LEVER WITH THE ELEMENT 38 IN THE DIRECTION OF THE ARROW THE PUSH BUTTON OF THE MICROSWITCH V TOWARD THE MECHANICAL STOP OTHERWISE THE DAMAGE OF THE MICROSWITCH COULD HAPPEN LOCK THE ELEMENT 38 A Microswitch screw 38 Connector Figure 11 20 BET A range microswitch adjustment A circuit closed B circuit open SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM WITH NUT Page 11 31 2012 02 06 AVIA PROPELLER POZN MKA Zap n n a vyp n n elektrick ho obvodu mikrosp na em V zkou ejte p kou Zv po sejmut nosi e kluzn ch kamen nebo ru n m p estavov n m vrtulov ch list s pomocn kem Ovl dac p ku vrtule v kabin letounu p itom nastavte do polohy prapor nosi kluznych kamen na p ce Zv z st v zapojen UPOZORN N E LISTY PRI PRET CEN UCHOP
68. INSTALLATION AND OPERATION MANUAL D BLADE REPAIR CAUTION Rework which involves cold working the metal resulting in concealment of a damaged area is not permitted A stress concentration may exist which can result in a blade failure WARNING DO NOT ATTEMPT TO PRE STRAIGHTEN A BLADE PRIOR TO DELIVERY TO PRODUCTION FACILITY OR AN APPROVED PROPELLER REPAIR STATION THIS WILL CAUSE THE BLADE TO BE SCRAPPED REPAIR OF A BENT BLADE IS CONSIDERED A MAJOR REPAIR THIS TYPE OF REPAIR MUST BE ACCOMPLISHED ONLY BY MANUFACTURER OR APPROVED PROPELLER REPAIR STATION CAUTION ANY REPAIR IN THE BLADE SHANK AREA IS NOT ACCEPTABLE 1 Local repair of camber and face side a V508 propeller blade Nicks and scratches not deeper than 0 15 mm 0 006 inch located in area of 580 mm 22 8 inch from airfoil beginning are acceptable and not required to be repaired Refer to figure 7 1 Nicks and scratches not deeper than 0 4 mm 0 016 inch are acceptable in area from 580 mm 22 8 inch to the tip and not required to be repaired Refer to figure 7 1 0 15 mm ne 4 9 ARE ACCEPTABLE IN THIS A AND NO ACC B AND NOT TO BE REPAIRED Figure 7 1 Allowable damage on camber and face side of the V508 blade Page 7 4 MAINTENANCE 2012 02 06 AVIA PROPELLER b Opravy mo no prov d t do hloubky max 1 5 mm 0 06 inch ale ne v ce ne 20 procent tlou ky profilu v m st opravy
69. LISTY PRI PRET EN UCHOPTE BL E KE KORENI NIKDY ZA PI KY 3 Po se zen pojist te op t va ku 27 dota en m zaji ovac ho roubku POZN MKA Okam ik zapnut el obvodu mikrosp na em je t mo no zkou et p ipojen m vhodn ho slaboproud ho zdroje max 12 V se rovkou na kol ky 3 4 z str ky obr zek 11 20 e V echny rouby kter mi se prov d lo se izov n pojist te poji ovac m lakem Strana 11 39 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL MICROSWITCH V TOWARD THE MECHANICAL STOP OTHERWISE THE DAMAGE OF THE MICROSWITCH COULD HAPPEN LOCK THE ELEMENT 38 WITH NUT NOTE Closing and breaking of the electric circuit by the microswitch V should be tested either by the lever Zv after removing the carrier of the slide blocks or with help of two mechanics by manual resetting of the propeller blades at the suitable position of the propeller control lever naturally with the engaged carrier of the slide blocks CAUTION HOLD BLADES NEAR BLADE SHANK NEVER AT BLADE TIP c Make sure that during the reverse motion to the initial position after breaking the electric circuit the top of the journal is spaced from the base position minimum 0 1 mm 0 004 inch If this clearance is less adjust it by adjusting element figure 11 20 and this screw is then locked by tightening its nut d Adjust when the
70. NOTE This additional turning with the stop 16 by 0 75 1 turn ensures clearance between locking valve and the pilot valve j k P esu te ovl dac p ku vrtule na doraz 16 a zajist te palcem p es p ku BI stla te k blokovac oup tko dle obr zku 11 31 P i tomto stla en mus b t patrna mal v le 0 1 mm 0 004 inch I Funkci p ezkou ejte dle odd lu 11 7 m Se zen a zji t n hodnoty ot ek zapi te do atestu regul toru P ka BI Blokovac oup tko P ka Rn nen kreslena cel Obr zek 11 31 Kontrola v le blokovac ho oup tka Strana 11 55 13 4 2010 SYST M OVL D N VRTULE 61 10 00 Secure the stop 16 by tightening the nut Move propeller control lever to the stop 16 and fix manually through the lever BI press the locking valve according to figure 11 31 Small clearance 0 1 mm 0 004 inch must be evident Verify functionality according to section 11 7 Record in the logbook partially Figure 11 31 Blocking valve clearance check Page 11 55 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 3 Se zen praporov polohy plat pro regul tor LUN 7815 03 a Prov d se se zen m dorazu 16 pokud zjist te e as pro dosa en praporov parkovac polohy p esahuje 15 s b Sejm te plombu a v zac dr t z dorazu 16 obr zek 11 30
71. POZN MKA P ku Rn m ete p i p estavov n vrtulov ch list oto it k dorazu praporu 16 aby olej ze servomechanismu prot kal a nekladl odpor 17 Instalujte nosi kluznych kamen obr zek 11 6 na p ku Zv a na beta krou ek Na ep nosi e nasa te podlo ku a zajist te z vla kou 1 6x10 POZN MKA P i ka d instalaci pou ijte novou z vla ku 18 Na p ku Rn obr zek 11 9 zapojte t hlo od ovl dac p ky vrtule a zajist te 19 Na p ku Bo v z kladn poloze zapojte t hlo od ovl d n motoru a zajist te 20 Zapojte z suvku do mikrosp na e a pojist te 21 Prove te z kladn se zen regul toru dle postupu d le v t to kapitole C Vrtulov regul tor LUN7816 1 Zkontrolujte stav regul toru nesm b t viditeln po kozen 2 Zkontrolujte zda je na p ce Rn ustavena ta n pru ina obr zek 11 12 3 Zkontrolujte zaji t n v ech element obr zky 11 12 11 13 11 14 POZN MKA Zaji t n dut ho roubu matic trubek hrdel a uzav rac matice obr zek 11 8 prove te a po mont i trubek 4 Zkontrolujte plomby a zaji t n obr zky 11 12 11 13 Strana 11 19 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 16 If the propeller is not in feather move it to feather by turning blades to move the beta ring that it seats at the propeller hub CAUTION CATCH THE BLADES AT ITS SHANK NEVER AT B
72. Pojistn podlo ka 7 3 Poutko vodi e 2 17 Krou ek lo iska 2 53 roub 7 4 roub 2 18 Kuli ka 2 54 Samojistn matice 7 5 Matice 2 19 Separ tor kuli ek 2 55 Podlo ka 7 6 Podlo ka 2 20 Matice 2 56 O krou ek 7 7 Dr k vodi e 2 21 roub obj mky 2 57 O krou ek 7 8 roub 2 22 Matice obj mky 2 58 T sn c man eta 7 9 Podlo ka 2 23 Z vla ka 2 59 O krou ek 7 10 roub 2 24 roub 2 60 O krou ek 7 11 roub 2 25 Podlo ka 2 61 O krou ek 7 12 Matice 2 26 Op rka 2 62 O krou ek 7 13 Svorkovnice 2 27 Pojistn krou ek 2 63 O krou ek 7 14 Mezivlo ka 2 28 Pru ina 2 64 O krou ek 7 15 Vlo ka 2 29 Pojistka 2 65 O krou ek 7 16 Sestava sb ra e 2 30 Pojistn podlo ka 2 66 roub 7 17 roub 2 31 ep 2 67 Pouzdro 7 18 Podlo ka Tabulka 4 2 Seznam d l k obr zku 4 2 KONSTRUK N A PROVOZN INFORMACE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 2 27 2 28 2 29 2 30 2 31 Blade De icer O ring Hub Piston Cylinder Cylinder plate Cylinder nut Fork Tube Insert Overspeed governor Clamp Beta ring Beta rod Blade bushing Pitch change block Washer Retaining ring Fork guide Bearing ring Ball Separator Nut Clamp bolt Clamp Nut Cotter pin Flange bolt Washer Support Snap ring Spring Lock piece Lock washer Pin 2 32 2 33 2 34 2 35 2 36 2 37 2 38 2 39 2 40 2 41 2 42 2 43 2 44 2 45 2 46 2 47 2 48 2 49 2 50 2 51 2 52 2 53 2 54 2 55 2 56 2 57 2 58 2 59
73. REGUL TORU MOHLO BY SE VZP IT A DO LO BY KV ZNUT JEHO OUP TKA 77 PROJEV SE NEST LOST TLAKU A KMIT N M TAKT OV EM T LESO VENTILU NESM B T NEDOTA EN NEBO DOKONCE UVOLN N Reduk n ventil pojist te v zac m dr tem Odvzdu n n se provede standardn m zp sobem p i motorov zkou ce 4 Odstran n net snosti reduk n ho ventilu Net snost reduk n ho ventilu m e b t zp sobena povolen m v kem nebo vadn m t sn n m Dota en v ka se provede tak e v ko odjist te kl em podr te t leso reduk n ho ventilu 71 proti dotahov n a dot hnete v ko 72 Reduk n ventil pojist te v zac m dr tem Jestli e je p inou vadn t sn c krou ek reduk n ventil odjist te Podr te kl em t leso reduk n ho ventilu 71 a vy roubujte v ko 72 POZN MKA P i sn m n v ka dejte pozor aby v m nevypadla podlo ka y 73 a aby na pru in 75 z stal ep 74 Strana 11 66 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL NOTE Use shims with thickness of 1 and 1 5 mm 0 04 and 0 06 inch for adjustment In the case that the pressure will be adjusted using sealing washers element 76 under the cover then adding removing of a washer will reduce increase the pressure Washer thickness of 1 mm 0 04 inch means pressure change as for the element 73 see above NOTE Use washers with thicknes
74. Sv 65 using lock wire to the governor such way that its movement will not be restricted c Propeller condition lever must be placed in maximum RPM position and then the lever Rn must be at maximum RPM stop 15 d Place the propeller condition lever into the feather position and fix the lever Rn must be at its feather stop 16 Place the propeller condition lever back to the maximum RPM e Place the engine condition lever to the idle stop guideline on the cam lever must align with minimum flight pitch guideline on the governor scale figure 11 274 If not adjust according to engine operational manual The pin of outer coaxial valve must touch the stop 58 CAUTION IF THE ENGINE CONDITION LEVER IS PLACED OVER IDLE STOP INTO BETA RANGE DON T MOVE THE PROPELLER CONDITION LEVER INTO FEATHER POSITION AND VICE VERSA Page 11 42 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Toleran n pole reverzu Ryska minim ln ho letov ho hlu Obr zek 11 27 Regul tor LUN7815 02 Kontrola z kladn ho se zen f Ovl dac p ku motoru p estavte do polohy max reverz ryska na p ce s va kou mus b t proti toleran n mu poli reverzu na stupnici regul toru obr zek 11 27B Pokud nen prove te se zen podle Provozn p ru ky motoru g Zapojte t hlo Sv 65 na roubujte matici a pojist te z vla kou UPOZORN N P i ka d instalaci
75. TOOLS Page 10 1 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL N zev Popis Vyobrazen Designation Description Illustration N str n estihrann kl 427 Hexagon key wrench Kl pro mont a demont roub krytu P Wrench to install and remove spinnerdome C 57 screws T B Kl omezova e ot ek P N 800 120 Overspeed governor wrench P N 800 120 nahrazuje kl P N 066 7103 replaces wrench P N 066 7103 Kl pro demont a mont v ka omezova e ot ek v r mci 900 hodinov 2 ro n prohl dky Nen pot eba pro verze V508Z a V508H T k se pouze vrtul vybaven ch omezova em Wrench to remove and install overspeed governor cover during the test at 900 hour 2 year inspection Not apply to hub models V508Z and V508H ot ek Jihostroj dr kovan v ko Apply only to hubs equipped with overspeed Net k se vrtul vybaven ch omezova em ot ek governor Jihostroj slotted cover Avia estihrann v ko Not apply to hubs egipped with overspeed governor Avia hexagon cover Vod c ep P N 900 0221 2 kusy Guide pin P N 900 0221 2 pcs Doporu eno pro zabr n n po kozen p ruby motoru p i instalaci a demont i vrtule viz kapitola Mont n a provozn instrukce Recommended to prevent damage of engine flange during propeller installation and removal refer to Installat
76. WASHER CAUTION HOLD THE BLADES NEAR BLADE SHANK AT TURNING NEVER AT TIP 3 Safety the cam 27 after adjustment with the securing screw NOTE It is possible to check when the circuit is energized using power supply max 12V and a suitable lamp connected to connector pins 3 and 4 figure 11 20 e All screws used for adjusting should be secured with suitable paint Page 11 32 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER 4 Ser zeni maxim ln ho reverzn ho v konu 8 Strana 11 33 13 4 2010 plat pro regul tor LUN7815 02 Zjist te zda je vypojeno t hlo Sv 65 z kulisy Sv Pokud ne odjist te a vy roubujte matici a vyjm te ep Potom t hlo vysu te mimo kulisu Sv obr zek 11 17 Uvoln n t hlo Sv 65 p iva te v zac m dr tem k pevn sti regul toru tak aby jeho pohyb v dal m pr b hu se izov n nebyl omezen Se zen max reverzn ho v konu prove te na motoru podle Provozn p ru ky motoru Po se zen max reverzn ho v konu p estavte ovl dac p ku motoru do polohy max reverz ryska na p ce s va kou je proti toleran n mu poli reverzu na stupnici regul toru obr zek 11 21 Pokud nen prove te se zen podle provozn p ru ky motoru Zapojte t hlo Sv 65 ut hn te matici epu a kontrolujte se zen sdru en vazby na stupnici podle t to kapitoly Poji t n matice z vla kou pro
77. Zv E x NT sn n N Packing N M Obr zek 11 10 Regul tor LUN7815 03 Pohled sm rem od motoru Figure 11 10 Governor LUN7815 03 View from engine 11 Verify governor flange and gear box flange Both surfaces must be clean and free 11 Kontrolujte dosedac plochu pr ruby regul toru s centr z a pr rubu na reduktoru from any damage Use a clean cloth eventually with cleaning solvent to wipe seating motoru Plochy mus b t ist bez po kozen povrchu Plochy o ist te ist m hadrem p padn namo en m do rozpou t dla faces 12 Insert drive rod into the governor shaft with square inward figure 11 10 Try to turn 12 Do h dele regul toru obr zek 11 10 vlo te torzn ty inku ty hranem dovnit with drive rod The rod should rotate freely Zkuste ot et torzn ty inkou jej pohyb mus b t voln UPOZORN N ne CAUTION TORZN TY INKA MUS M T VYZNA ENO SLO MONTOVAN HO REGUL TORU THE DRIVE ROD MUST BE IDENTIFIED WITH GOVERNOR S N 13 Pokud je instalov na vrtule sejm te nosi kluznych kamen z p ky Zv obr zek 13 If the propeller is installed remove carbon block assembly from lever Zv figure 11 6 11 6 Sr SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM U 7 1 2015 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Obr zek 11 11 Regul tor LUN7815 03 Pohled sm rem od vrtule Figure 11 11 Governor LUN7
78. a provozn instrukce v t to p ru ce d Z vadu odstra te dle instrukc v robce motoru Z vada Nesv t kontrolka BETA re imu Mo n p ina a Vadn mikrosp na b Z vada na obvodu signalizace N prava a Postupujte dle instrukc v robce motoru b Postupujte dle instrukc v robce letounu Strana 8 2 6 2 2012 ODSTRA OVAN Z VAD E 1500 INSTALLATION AND OPERATION MANUAL Trouble It is not possible to change propeller rpm using the propeller condition lever Probably cause a Disconnected the governor control linkage b Propeller governor failure Remegy a Verify and repair the governor control linkage per instruction of engine manufacturer b Replace the governor per instruction of engine manufacturer Trouble Sluggish rpm change Probably cause a Low governor relief valve setting b Propeller governor failure c Defective o rings in engine shaft insert d Leakage in oil channels in engine Remegy a Verify and adjust pressure of the relief valve per instruction of engine manufacturer Replace the propeller governor per instruction of engine manufacturer Remove the propeller from engine check sealing and replace defective o rings Follow chapter Installation and Operation Instruction of this manual Follow instruction of engine manufacturer b c 2 Trouble Beta lamp does not lit Probably cause a Defective microswit
79. adjusting lever on the governor is connected through linkage with propeller condition lever in the aircraft cockpit Position of the adjusting lever determines loading of the speeder spring This loading represents RPM requested The governor shaft which is driven from engine gear box and which RPM are proportional to propeller RPM is connected with flyweight head and both are rotating Page 11 2 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER Odst ediv s la z va p sob proti d c pru in Tato s la p edstavuje skute n ot ky vrtule Odst ediv s la od z va p sob na op rku d c ho oup tka Opa n m sm rem p sob na op rku s la d c pru iny Op rka je spojena s d c m oup tkem kter d dod vku oleje do vrtule nebo z vrtule Rozezn v me t i z kladn stavy syst mu ovl d n vrtule rovnov n stav p et en a nedot en a Rovnov n stav Sledujte obr zek 11 1A Odst ediv s la p sob c na z va je v rovnov ze se silou od d c pru iny a d c oup tko nedod v olej do ani z vrtule Skute n ot ky vrtule odpov daj ot k m navolen m b P et en Sledujte obr zek 11 1B Odst ediv s la p sob c na z va je v t ne s la od d c pru iny Z va se vyklon sm rem ven a zvednou d c oup tko d c oup tko otev e kan l mal ho hlu do odpadu list
80. at maximum RPM stop 16 WARNING BEFORE YOU WILL MOVE WITH PROPELLER CONTROL LEVER VERIFY ENGINE CONTROL LEVER WHICH SHOULD BE AT IDLE STOP VERIFY BATTERY BREAKER IT SHOULD BE SWITCHED OFF e Loose the stop nut 16 and turns it 2 to 2 5 clockwise lever Rn travel to feather position will increase f Move propeller control lever easy up to the stop which is not the stop 16 but blocking valve to which the pilot valve inside the governor moved by the lever Rn will hit g Secure propeller control lever in this position Page 11 54 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER h Dorazem 16 ot ejte proti sm ru hodinov ch ru i ek a nastavte jej p esn na dotek h epu p ky Rn i Odjist te a odsu te ovl dac p ku vrtule na zar ku max ot ek a dorazem oto te nav c je t o 0 75 1 ot ku proti sm ru hodinov ch ru i ek POZN MKA Oto en m dorazu 16 o 0 75 1 ot ku nav c vznikne v le mezi blokovac m oup tkem a hlavn m oup tkem j Doraz 16 zajist te dota en m matice E 1500 INSTALLATION AND OPERATION MANUAL Turn counterclockwise the stop 16 and adjust it so that exactly touching the lever Rn pin 16 i Loose and move propeller control lever to maximum RPM stop and turn counterclockwise the stop 16 another 0 75 1 turn
81. atmosf rick ch podm nk ch Kontrola tlaku v proh vac v tvi praporovac ho erpadla jen p i z stavb syst mu praporov n s praporovac m erpadlem 1 Ovl dac p ku motoru p estavte do polohy max trval ho v konu 2 Signalizace PRAPOROVE ERPADLO se nerozsv t Kontrola funkce ovl dac p ky vrtule Ovl dac p ka motoru v poloze max trval ho v konu Ovl dac p kou vrtule nastavte ot ky vrtule na 1900 ot min po ust len sni ujte ot ky ovl dac p kou vrtule na 1700 ot min a zp t do v choz polohy Ot ky vrtule mus sledovat p estavov n ovl dac p ky vrtule v obou sm rech IN 1 Ico UPOZORN N KROUT C MOMENT NESM PREKRO IT 100 Kontrola reverzn ch ot ek a reverzn ho v konu kontrola funkce sekund rn zar ky Ovl dac p ku vrtule nastavte do polohy max ot ek Ovl dac p ku motoru nastavte na doraz volnob hu Odjist te mechanick doraz a p esu te ovl dac p ku motoru pomalu a plynule sm rem do reverzu sou asn sledujte 17 1 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 4 Repeatthe cycle 3 times wait about 40 s at the idle between the cycles Propeller RPM check at idle only for twin engine aircrafts 1 Setengine condition lever to idle 2 Move the propeller condition lever to maximum RPM position 3 RPM difference should be 40 RPM max If higher correct it a
82. b t odli n zbarven m sto na povrchu d lu stopy op len nebo rozte en kovu nebo chyb j c materi l v m st deru blesku 3 Zkontrolujte povrch list na zn mky niku oleje z vrtule Postupujte dle odd lu Unik oleje nebo maziva v t to kapitole pro zji t n zdroje niku oleje POZN MKA U nov nebo nov opraven vrtule m e b hem prvn ch n kolika hodin provozu doch zet k m rn m nik m oleje co m e b t zp sobeno sed n m t sn n a rozst ikem maziva pou it ho p i mont i vrtule Tyto uniky oleje by m ly po p ibli n 10 hodin ch provozu ustat 4 Pouze verze V510 E Zkontrolujte ru n vrtulov listy na v li v ulo en Z dn v le listu krom hlov v le nen p pustn V p pad zji t n v le prove te kontrolu dle odd lu V le listu kde jsou uvedeny maxim ln povolen v le listu Strana 6 1 6 2 2012 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 6 INSPECTIONS CAUTION ALL REMOVAL INSTALLATION AND REPAIR PROCEDURES MUST BE CARRIED OUT BY PERSONNEL WITH APPROPRIATE QUALIFICATION NOTE INSPECTIONS DESCRIBED IN THIS CHAPTER DO NOT SUPERSEDE INSPECTIONS DESCRIBED IN AIRCRAFT AND ENGINE MANUFACTURER S MANUALS A PRE FLIGHT CHECK NOTE Perform the pre flight check before each flight 1 Visually inspect the blades for nicks gouges erosion cracks and corrosion Repair before further flight by an a
83. c ho momentu Strana 9 1 Skladovac teplota uveden v F p epo tena na Strana 11 48 Zkou ka funkce vrt syst mu na zemi nemus b t nov prov d na po v m n vrtule Strany 1 2 a 1 4 V kapitole 7 dopln n odd l D Oprava listu Dopln na kapitola 11 Syst m ovl d n vrtule Strany 1 1 1 2 P id n odd l Omezen ivotnosti s uveden m d l s omezenou ivotnost a jejich limit Strana 2 1 Odd l Gener ln oprava byl aktualizov n Strana 2 2 P id ny odd ly Souvisej c dokumenty a Rozm ry Strana 4 3 Odd l Regul tor vrtule byl vyjmut Strany 4 4 a 4 11 Aktualizov ny obr zky sestav vrtul a prid ny seznamy d l Strany 5 2 5 6 5 10 5 11 Pr m r v zac ho dr tu v palc ch 0 03 inch opraven na 0 032 inch Strany 5 3 5 11 5 17 Desetinn rka u rozm ru v palc ch zm n na na te ku R 137 11 cont d R 10 12 February 06 2012 61 10 00 l 2 to 1 4 11 2 to 11 4 11 1 1 1 1 2 2 1 to 2 3 4 3 to 4 11 5 2 to 5 4 5 6 5 10 5 11 9 13 5 14 5 17 6 1 6 2 6 4 6 7 6 9 to 6 16 7 4 to 7 9 8 1 to 8 8 9 1 10 1 10 2 11 1 11 2 11 27 11 29 to 11 32 11 35 to 11 39 11 41 11 45 11 46 11 48 11 56 11 57 11 60 11 63 11 65 to 11 67 11 71 LIST OF REVISIONS must be filled out Page 6 17 Added note that foreign object strike event resulted in overhaul Page 6 18 Actions in case
84. centre CAUTION All activities contains in this manual shall be practices only by persons with commensurating qualification Breach of the operating instructions and procedures in this manual exceeding of rated operational terms or performance limits can cause incorrect propeller function Manufacturer or authorized service centre doesn t bear any responsibility for damages incurred non performance instructions or procedures stated in this manual SERVICE DOCUMENTATION Product user is responsible for this manual up dating according to issued changes Latest revision of this manual is freely disposable at www aviapropeller com See this website for service letters bulletins and advisories associated with propellers in this manual NOTICE Illustrations pictures and drawings in this manual are only by example for displayed object and it s not to be regarded as binding on any propeller type or her section GUARANTEE Guarantee conditions for each one propeller are determined in contract of purchase THANK YOU FOR CHOOSING AVIA PROPELLER PRODUCT Properly maintained it will give you many years of reliable service AVIA PROPELLER OBSAH SEZNAM ZM N s Rocco etcetera M d Il 1 P EHLED PLATN CH Ill 1 1 OMEZEN LETOV ZP SOBILOSTI 1 1 s OBECN 2 1 3 TYPOV ZNA EN n ore qe RARE 3 1 4 KONSTRUK N A PROVOZN INFORMACE 4 1 5 MONT N
85. chr nit kart e sb ra e jinak m e doj t k jejich po kozen Sejm te nosi kluzn ch kamen z t hla beta a z beta krou ku Demontujte p edn kryt vrtule Pro zav en vrtule na je b pou t popruhy p padn pokud jsou vyjmut listy speci ln z v s instalovan do jednoho pouzdra listu Strana 5 14 6 2 2012 MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL CAUTION IF THE PROPELLER BLADES MOVE FROM REVERSE POSITION IT IS NECESSARY TO STAY POWER AT GROUND IDLE UNTIL THE BETA LAMP IN THE COCKPIT SWITCHED OFF POWER INCREASING AT BETA LAMP SWITCH ON CAN CAUSED THE PROPELLER OVERSPEEDING Shut down the engine in accordance with the Flight Manual After ground runs check propeller for oil leaks blade shake and condition of de icing components Flight test Perform test in accordance with the description in the Flight Manual CAUTION MOVE POWER LEVER AND RPM LEVER ALWAYS SLOWLY TO AVOID OVERSPEED J PROPELLER REMOVAL FROM ENGINE NOTE The propeller must always have the beta ring fully inserted to the hub for access to mounting bolts nuts For model V508H the beta puller P N 900 0175 is necessary for full insertion of the beta ring to the hub Use the beta puller in same manner as described in Installation of model V508H on engine in this chapter NOTE Remove the blades from the hub after cables are disconnected from the de icers and clamp bolts ar
86. control system with other governors refer to engine manufacturer s manual I TESTING Engine and propeller manufacturers recommend not to use high engine speed on ground Before running the engine clean the ground to avoid damage of the propeller blade and the de icers i e stone nicks De icing function check Ground test runs with installed electrical de icing system are only allowed with a mounted spinner otherwise the wiring will be damaged With running propeller no time limit for de icing switch on is reguired With non running engine the switch on time of the de icing system is limited for only 2 cycles Otherwise overheating of the de icers will occur Ground test Propeller check Perform engine start and perform warm up per the Flight Manual Adjust power lever for approximately 1700 rpm the propeller condition lever is at maximum rpm stop Pull the propeller lever back out until the rpm decreased by 200 to 400 rpm Push the propeller condition lever full forward in for take off position and observe rpm increase to the adjusted value Repeat this procedure at least three times to purge air from the propeller hydraulic system and to introduce warmed oil to the cylinder Adjust the power lever at approximately 1950 rpm Pull the propeller lever back until rpm drops about 100 rpm now and increase engine power by approximately 596 to 1096 generator speed Observe the governor function rpm must stabilize to decreased lev
87. demontujte rouby a sejm te kryc v ko UPOZORN N Postupujte opatrn kryc v ko je m rn p edepnut pru inou uvnit 2 Vyjm te veden pru iny a pru inu 3 Stejn m zp sobem demontujte i ostatn kryc v ka POZN MKA Dbejte aby nedo lo ke ztr t dn ho z demontovan ch d l 4 Nasu te dut kl 900 0176 na t hlo v otvoru a vsu te do n boje Nastaven minim ln ho letov ho hlu se prov d ot en m se izovac matice na t hlu p es adapt r na matici Vliv ot en matice na zm nu ot ek vrtule je uveden E 1500 INSTALLATION AND OPERATION MANUAL NOTE Make sure the sling is rated up to 200kg 440Lbs Remove two flange bolts from the engine flange Install two guide pins into opened threaded holes in the hub flange NOTE It is recommended to use the guide pins to avoid heavy damage of the engine flange during propeller removal Remove the propeller from the engine Remove guide pins from the hub flangeside NOTE Use a transport plug to close the hub flangeside to avoid oil flowing from the hub and flange damage Install flange o ring on the plug and use the flange bolts and washers to attach the plug to the hub K ADJUSTMENT OF MINIMUM FLIGHT ANGLE OF MODEL V508H Adjustment of minimum flight angle is possible after removing the cover caps of the beta rods Perform the following steps see figure 5 16 1 Remove the safety wire from the cover cap scr
88. determine the corrective action to be taken In case of overspeed and or overtorque event resulted in inspection or overhaul is required to fill out the report in the end of this chapter and send it with propeller to manufacturer or authorized service centre OVERSPEED INSPECTION NO ACTION NECESSARY 90 00 90 200 250 300 350 400 Duration of Overspeed in Seconds Figure 6 7 Overspeed event Page 6 11 INSPECTIONS 2012 02 06 AVIA PROPELLER GENER LN OPRAVA v procentech P eto en DN OPAT EN 50 100 150 200 250 300 350 400 Trv n p eto en v sekund ch Obr zek 6 8 P ekro en krout c ho momentu Pro p stroje montovan na motoru regul tory erpadla d c jednotky vrtule vyroben Avia Propeller je v p pad p eto en vrtule stupn a trv n kter vy aduje minim ln kontrolu vrtule po adov na kontrola p stroje obn ej c jeho rozeb rku a kontrolu dle p slu n oprav rensk dokumentace Bez ohledu na stupe po kozen mus b t jak koliv ud lost p eto en zaznamen na do z znamn ku vrtule N pravn opat en Pokud nejsou vy adov na dn opat en neprov d se dn dr ba pouze se ov zda p i p eto en nedo lo k mechanick z vad Pokud je vy adov na prohl dka po p eto en nebo gener ln oprava vrtule mus b t sta ena z provozu a odesl na k prohl dce n
89. dojde k p eto en vrtule na turb nov m motoru postupujte podle obr zku 6 7 pro stanoven n pravn ch opat en Pokud dojde k p ekro en krout c ho momentu motoru postupujte podle obr zku 6 8 pro stanoven n pravn ch opat en V p pad p eto en vrtule a nebo p ekro en krout c ho momentu vy aduj c nutnost prohl dky nebo gener ln opravy mus b t o ud losti vypln n protokol na konci t to kapitoly a zasl n spole n s vrtul k v robci nebo do autorizovan ho servisn ho st ediska VY AZEN GENER LN OPRAVA v procentech P eto en DN OPAT EN Trv n p eto en v sekund ch Obr zek 6 7 P eto en vrtule Strana 6 11 6 2 2012 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL E SPECIAL INSPECTIONS 1 Overspeed Overtorque Overspeed occurs if the propeller RPM exceeds the maximum RPM published in Type Certificate Data Sheet of applicable propeller type Overtorque occurs when the engine load exceeds the limits established by the engine propeller and airframe manufacturer The corrective action is based on the severity and the duration of overspeed or overtorque for a single event When a propeller installed on a turbine engine has an overspeed event refer to figure 6 7 to determine the corrective action to be taken When a propeller installed on a turbine engine has an overtorque event refer to figure 6 8 to
90. ek hl uvnit vrtule nen mo n s v jimkou verze V508H viz d le v t to kapitole v echny zar ky jsou nastaveny b hem v roby Nicm n je pot eba prov st z kladn nastaven na regul toru vrtule Mus b t provedena tato nastaven nastaven minim ln ho letov ho hlu nastaven maxim ln ho reverzn ho v konu nastaven mikrosp na e p sma BETA Strana 5 12 18 9 2014 MONT N A PROVOZN INSTRUKCE 61 10 00 TWO SCREWS ATTACHING X THE BRUSH BLOCK TO THE K S MOUNTING BRACKET X Ns Figure 5 15 G SPINNER DOME INSTALLATION Right position of the spinner dome is marked with mounting marks on the one of bulkhead filler plate and on the one of the spinner dome cutout usually at blade No 1 Lubricate a rubber ring inside the spinner dome with grease prior to be installed on the hub Use the delivered screws and washers to attach the spinner dome After right installation the numbers stamped on bulkhead filler plate and near the spinner dome cutout should be side by side H BASIC ADJUSTMENT AFTER INSTALLATION Adjustment of the pitch stops inside the hub is not possible except model V508H see below in this chapter all stops are set during manufacturing But basic adjustment has to be performed with the propeller governor See below for parameters have to be adjusted after propeller is installed on the engine minimum flight angle adjustment maximum reverse
91. ek od p ruby vrtule sm rem k motoru a Pull the beta ring by hand away from the propeller flange toward the engine b Na beta t hla vlo te veden pru in a pru iny a zasu te do vrtule b Insert the spring guides and the springs onto the beta rods and into the propeller c Na vrtuli vlo te v ka beta t hel a p ipevn te rouby s podlo kami Pojist te rouby v i sob nerezov m v zac m dr tem 0 81 mm 0 032 c Cover the beta rods with the cover caps and attach the cover caps to the inch propeller with the screws and washers Safety the screws against each other with 0 81 mm 0 032 inch stainless steel wire Strana 5 9 1 20 10 2014 Page 5 9 1 MONT N A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 PORAD A PORAD B V echny verze krom V510T Krok 1 Ut hn te v echny rouby v po ad A momentem 35 45 Nm 25 33 Ib ft Krok 2 Ut hn te v echny rouby v po ad B momentem 95 100 Nm 70 74 Ib ft p i instalaci na letoun L410 125 130 Nm 92 96 Ib ft p i instalaci na ostatn letouny Pouze verze V510T Krok 1 Ut hn te v echny rouby v po ad A momentem 75 85 Nm 55 63 Ib ft Krok 2 Ut hn te v echny rouby v po ad A momentem 115 125 Nm 85 92 Ib ft Krok 3 Ut hn te v echny rouby v po ad B momentem 140 145 Nm 103 107 Ib ft Obr zek 5 11 12 Ov te p edepsanou v li mezi kamenem zp tn
92. electric circuit is energized based on the beta ring position using following procedure 1 Setthe cockpit propeller condition lever into feather position protrude beta ring by turning propeller blades Set the beta ring according to table 11 2 or 11 3 depending on propeller type support the ring in this position using suitable insert ID Moment when the electric circuit is energized shall be adjusted only by turning the cam 27 figure 11 20 CAUTION TWO WASHERS ARE PLACED UNDER THE SECURING SCREW ONE OF THEM IS SPRING WASHER HOLD THE BLADES NEAR BLADE SHANK AT TURNING NEVER AT TIP 3 Safety the cam 27 after adjustment with the securing screw NOTE It is possible to check when the circuit is energized using power supply max 12V and a suitable lamp connected to connector pins 3 and 4 figure 11 20 e All screws used for adjusting should be secured with suitable paint Page 11 39 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER 3 Se zen maxim ln ho reverzn ho v konu Prov d se po mont i regul toru ot ek vrtule po mont i motoru a Odpojte drakov ovl d n ovl dac p ky motoru na motoru b povolte a demontujte matici a roub z p ky Sv obr zek 11 25 a p ku opatrn povyt hn te tak aby p i ot en proch zela mimo dorazov kol k p ky POZN MKA P ku Sv nesn mejte z vnit n ho koaxi ln ho oup tka M e doj t ke z
93. for damage No damage acceptable 2 Verify installation of spring on the lever Rn figure 11 3 3 Verify locking devices of appropriate elements figures 11 3 11 4 11 5 NOTE Secure turning bolt tube cap nut sockets and closing nut figure11 8 after tubing installation 4 Verify seals and securing figures11 3 and 11 4 CAUTION BE CAREFUL AT SECURING ELEMENT 82 FIGURES 11 4 AND 11 5 LOCKING WIRE AND COTTER PIN LEFT THREAD IS MARKED WITH L THE STOP FIGURE 11 4 MUST HAVE THE SAFETY WIRE ACROSS THE HEXAGON HEAD OF THE BOLT STOP MUST NOT BE RELEASED AND RE ADJUSTED IT IS ADJUSTED BY GOVERNOR MANUFACTURER POZN MKA NOTE D ly 19 16 29 B2 7 8 a 65 jsou se izovac regula n prvky Parts 15 te P9 B2 B7 8 and 65 are adjustable Strana 11 8 SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM Page 118 13 4 2010 2010 04 13 AVIA PROPELLER b S p kou Bc obr zek 11 3 v z kladn poloze ryska na p ce s va kou se kryje s ryskou minim ln ho letov ho hlu na stupnici regul toru a ep ovl dac p ky se dot k dorazu 58 p ekontrolujte chod Rn od dorazu 15 k dorazu 16 UPOZORN N P KA Rn MIMO DORAZ 15 NEP ESUNUJTE P KU Be ZE Z KLADN POLOHY Z RYSKY MIN LETOV HO HLU SM REM DO REVERZN POLOHY NEBEZPE PO KOZEN BLOKOVAC HO MECHANISMU 6 Sejm te z vla ku vy roubujte matici a vyjm
94. listu 15 000 hodin 2 000 hodin WUn e c vx 15 000 hodin 2 000 hodin M leCus miedo 15 000 hodin 2 000 hodin Limit ivotnosti 2000 hodin plat pouze pro d ly vrtule V508E AG 106 A provozovan na letounu Turbo Shark Sukhoi 26MX s motorem Walter M601T Strana 1 1 6 2 2012 OMEZEN LETOV ZP SOBILOSTI E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 1 AIRWORTHINESS LIMITATIONS This Airworthiness Limitations Section is EASA approved in accordance with Part 21A 31 a 3 and CS P40 b and 14 CFR Part 35 4 A35 4 Any change to mandatory replacement times inspection intervals and related procedures contained in this section must also be approved The Airworthiness Limitations Section is FAA approved and specifies maintenance required under 88 43 16 and 91 403 of the Federal Aviation Regulations unless an alternate program has been FAA approved A Life Limits 1 The life limit should be established for certain part of the propeller assembly This limit requires the replacement of such part after a specified number of hours of operation TSN Time Since New 2 This section summarizes the life limited parts of propeller models covered by this manual 3 The blade life limit is not affected whether or not the de icing components are installed 4 Below mentioned life limits of the parts apply to all of propeller models and propeller aircraft engine combinations unless specifically note
95. mu na zemi Strana 11 44 13 4 2010 plat pro regul tory LUN 7815 02 LUN7815 03 Prove te v pln m rozsahu po v m n motoru vrtule nebo regul toru ot ek vrtule SYST M OVL D N VRTULE E 1500 INSTALLATION AND OPERATION MANUAL 2 Basic adjustment check a only for governor LUN7815 03 Propeller condition lever must be placed in maximum RPM position and then the lever Rn must be at maximum RPM stop 15 Place the propeller condition lever into the feather position and fix the lever Rn must be at its feather stop 16 Place the propeller condition lever back to the maximum RPM Place the engine condition lever to the idle stop guideline on the cam lever must align with minimum flight pitch guideline on the governor scale figure 11 284 If not adjust according to engine operational manual Place the engine condition lever to the ground idle stop guideline on the cam lever must align with minimum ground pitch guideline on the governor scale fig 11 28 B Verify clearance between tracking lever pin and stop acc to procedure in section 11 6 Verify clearance between beta ring and carbon block assembly according to procedure in section 11 6 Minimum ground pitch guideline Figure 11 28 Governor LUN7815 03 Basic adjustment check 3 Propeller control system ground testing for governors LUN7815 02 LUN7815 03 Perform after engine propeller or propeller governo
96. obr zku 4 3 Table 4 3 Partlist reffering to Figure 4 3 R KONSTRUK N A PROVOZN INFORMACE 61 10 00 DESIGN AND OPERATION INFORMATION AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL N Xen n TE i Y M Obr zek 4 4 Sestava vrtule V510 Strana 4 10 17 1 2014 Figure 4 4 V510 Propeller assembly KONSTRUK N A PROVOZN INFORMACE 61 10 00 DESIGN AND OPERATION INFORMATION a AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 1 1 Vrtulovy list 2 36 Kuli ka 2 75 O krou ek Blade 2 36 Ball 2 75 O ring 1 2 Odmrazovac
97. of anti corrosive oil NOTE Prior the propeller will be re installed on the engine wipe the outer surface to remove the oil and refer to section Installation and operation instruction Page 7 3 MAINTENANCE 2010 04 13 AVIA PROPELLER D OPRAVA LISTU UPOZORN N Opravy listu tv en m kovu za studena za elem skryt po kozen ch ploch jsou nep pustn Vznik koncentrace nap t m e vy stit v ulomen listu VAROV N P POKUD JE LIST OHNUTY NEPOKOUSEJTE SE O JEHO NAROVN N PRED ODESL N M DO OPRAVY M E TO ZAP INIT JEHO POZD J VY AZEN OPRAVA OHNUT HO LISTU JE POVA OV NA ZA SPECI LN PROCES TAKOVOU OPRAVU MOHOU PROV D T POUZE V ROBCE NEBO AUTORIZOVAN SERVISN ST EDISKA UPOZORN N V KORENOV C STI LISTU JSOU JAK KOLIV OPRAVY NEPR PUSTN 1 M stn oprava na sac a tlakov stran a List vrtule V508 Do vzd lenosti 580 mm 22 8 inch od za tku profilov sti listu jsou p pustn vrypy a z seky do hloubky max 0 15 mm 0 006 inch kter nevy aduj opravu viz obr zek 7 1 Od vzd lenosti 580 mm 22 8 inch ke pi ce jsou p pustn vrypy a z seky do hloubky max 0 4 mm 0 016 kter nevy aduj opravu viz obr zek 7 1 CE NEP ESAHUJ C ich JSOU Obr zek 7 1 P pustn po kozen na sac a tlakov stran listu V508 Strana 7 4 p 6 2 2012 UDRZBA 61 10 00 E 1500
98. of exposure to fire and engine oil contamination events was implemented Page 6 19 6 20 Added reports on overspeed and overtorque events Page 9 1 Storage temperature in celsius grades added to the fahreinheit grades Page 11 48 Ground test of propeller control system newly not necessary after propeller replacement Pages 1 2 to 1 4 Added section D Blade repair to chapter 7 Added chapter 11 Propeller control system Pages 1 1 1 2 Added section Life limits with list of life limited parts and their limits Page 2 1 Section Overhaul was updated Page 2 2 Added sections Related documents and Dimensions Page 4 3 Section Propeller governor was removed Pages 4 4 to 4 11 Propeller assembly figures updated and partlist tables added Pages 5 2 5 6 5 10 5 11 Safety wire diameter in inches changed from 0 03 inch to 0 032 inch Page 5 3 5 11 5 17 Decimal coma in inch dimension changed to dot Page 11 2 2012 02 06 AVIA PROPELLER C slo zm ny SEZNAM ZM N Datum vyd n Zm n n strany E 1500 Stru n popis Revised Page INSTALLATION AND OPERATION MANUAL LIST OF REVISIONS Short Description R 10 12 pokra Strana 5 4 U p pravk proti zad en bylo p vodn uveden nebo podobn zm n no na nebo ekvivalent Strana 5 13 Aktualizov ny informace o instalac ch s jin mi regul tory ne Jihostroj Strana 5 14
99. p ibli n approximately Tabulka 11 5 Vliv se zen dorazu 58 na volnob n ot ky Table 11 5 Stop 58 influence onto idle RPM POZN MKA NOTE P estaven m doraz 53 o polovi n hodnotu z rozd lu volnob n ch ot ek vrtul se sn volnob n ot ky vrtule s vy mi ot kami a zv se volnob n ot ky vrtule s ni mi ot kami Toto se zen sn rozd l volnob n ch ot ek obou vrtul na minimum 1Odstra te zaji t n doraz 58 jedn m kl em p idr te roub druh m povolte zaji ovac matici 2 Pooto te dorazem 58 na obou regul torech ve sm ru o hodnotu dle tabulky 11 5 U obou regul tor kontrolujte rozm r B kter se od p vodn ho p i oto en o p l kola zm n o 0 35 mm 0 014 inch nebo p i oto en o 1 kolo o 0 7 mm 0 028 inch Pokud zjist te odchylku upravte nov rozm r B na vypo tenou hodnotu Pro se zen m ete pou t pooto en dorazu b8 o 1 3 nebo 1 4 kola UPOZORN N POOTO EN DORAZEM 58 O V CE NEZ 1 KOLO NEN DOVOLENO Strana 11 58 13 4 2010 Kl em p idr te roub v nastaven poloze druh m kl em dot hn te zaji ovac matici a znovu kontrolujte rozm r B postupn u obou regul tor Nov m nastaven m dorazu 58 se poru kryt rysky na p ce s va kou s ryskou minim ln ho let hlu na stupnici re
100. p ky motoru pokra uje 190 Rozsv cen signalizace BETA n sleduje prudk vzestup ot ek na hodnotu cca 1400 1500 ot min c Ot ky gener toru p i rozsv cen BETA vzestup Pokud pr b h ot ek vrtule a gener toru a v etn zapnut signalizace odpov d popsan mu pr b hu je funkce sekund rn zar ky bez z vad P esu te ovl dac p ku motoru d le plynule sm rem do polohy max reverzu na dobu pot ebnou pro ode ten provozn ch hodnot Ov te reverzn v kon podle Provozn p ru ky motoru Maxim ln ot ky v reverzu jsou 2030 ot min Ovl dac p ku motoru p estavte pomalu a plynule zp t na zar ku volnob hu Ot ky vrtule sleduj pohyb ovl dac p ky motoru plynule klesaj na volnob h Ot ky gener toru okam it pokles na volnob n a setrv n na nich Zhasnut signalizace BETA zen p i cca 1100 ot min IO IO 100 Ot ky vrtule mus odpov dat v choz hodnot ot ek i Kontrola praporov n vrtulov ho syst mu i Z stavba s praporovac m erpadlem 1 Strana 11 50 13 4 2010 Kontrola funkce AUTOMATICK PRAPOROV N jen pri z stavb syst mu s automatickou funkc praporov nf a Kontrolujte funkci AUTOMATICK PRAPOROV N podle letov p ru ky letounu Kontrola funkce RU N PRAPOROV N a Kontrolujte funkci RU N PRAPOROV N podle letov p ru ky letounu b Na palubn ch stopk c
101. permitted Take care to external governor parts Skladov n na zemi nen p pustn Dbejte aby se nepo kodily vn j sti regul toru Strana 11 71 2 R M Page 11 71 6 2 2012 SYSTEM OVL DAN VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER Avia Propeller Ltd since 1919 Stroj rensk firma s dlouholet mi zku enostmi z v voje v roby oprav servisu a prodeje letadlov ch kovov ch staviteln ch leteck ch vrtul a jejich d l D N tym pracovn k v voje m dlouholet zku enosti spojen s v vojem vrtul Jedn m z posledn ch kol je roz en ady na ich v robk o nov vrtule ady AV leh duralov n boj Ve v rob se pou vaj nov CNC obr b c stroje kter ve spojen s tradi n profesionalitou person lu umo uj dos hnout vysok kvality na ich v robk D Modern vybaven odd len technick kontroly podporuje vysokou rove v robk dod van ch na im z kazn k m N syst m kvality spl uje po adavky Evropsk ho adu pro bezpe nost letectv EASA Na e obchodn odd len spolupracuje se z kazn ky s cca 50 zem cel ho sv ta Na im c lem je uspokojit v echny na e z kazn ky Na e v robky a innosti Celokovov letadlov vrtule pro p stov a turb nov motory do v konu 1200 HP pou van na letounech region ln dopravy zem d lsk ch letounech letounech v eobecn ho
102. procedure in section 11 6 j Check clearance between blocking and the pilot valve acc to procedure in section 11 6 k Verify clearance between beta ring and carbon block assembly according to procedure in section 11 6 Page 11 43 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 2 Kontrola z kladn ho se zen a plat pro regul tor LUN 7815 03 Ovl dac p ku vrtule nastavte do polohy max ot ek p ka Rn mus b t na dorazu max ot ek 15 Ovl dac p ku vrtule nastavte do praporov polohy a zajist te p ka Rn mus b t na dorazu praporu 16 Ovl dac p ku vrtule p estavte zp t do polohy max ot ek Ovl dac p ku motoru nastavte na zar ku volnob hu ryska na p ce mus b t proti rysce minim ln ho letov ho hlu na stupnici regul toru obr zek 11 28A Pokud nen prove te se zen podle provozn p ru ky motoru Ovl dac p ku motoru p estavte do koncov polohy volnob hu ryska na p ce mus b t proti rysce min pozemn ho hlu na stupnici regul toru obr zek 11 28B Kontrolujte v li mezi epem sledovac p ky a zar kou dle postupu v kapitole 11 6 Kontrolujte v li mezi beta krou kem a kameny nosi e dle postupu v kapitole 11 6 Ryska minim ln ho pozemn ho hlu Ryska minim ln ho letov ho hlu Obr zek 11 28 Regul tor LUN7815 03 Kontrola z kladn ho se zen 3 Zkou ka funkce vrtulov ho syst
103. regul tor ady LUN7816 se jedn o se zen tlaku pod reduk n m ventilem 1 RV Sejm te v zac dr t z reduk n ho ventilu Se i te tlak se izovac m prvkem 73 podlo kou uvnit reduk n ho ventilu nebo prvkem 76 t sn c podlo kou pod v kem 72 Kl em podr te t leso reduk n ho ventilu 71 aby se neuvolnilo a vy roubujte v ko 72 POZN MKA Pru ina reduk n ho ventilu je p edepjat pozor p i uvol ov n v ka Obr zek 11 35 Reduk n ventil V p pad e budete tlak se izovat p id n m ub r n m t sn c ch podlo ek prvek 73 pod pru inou 75 uvnit reduk n ho ventilu pak p i p id v n ub r n podlo ek se tlak zv sn Tlou ka podlo ky 1 mm 0 04 inch znamen zm nu tlaku asi o 0 07 MPa u regul tor ady LUN 7815 a 0 10 MPa u regul tor ady LUN 7816 UPOZORN N CELKOV TLOUSTKA VSECH PODLOZEK SM BYT MAXIM LN 4 mm 0 16 inch V PRUZIN 75 MUS Z STAT CEP 74 Strana 11 65 6 2 2012 SYSTEM OVLADANI VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL NOTE For governor LUN7816 it concerns check of relief valve pressure for the valve No 1 RV Remove seal from the relief valve Adjust the pressure either using element 73 shim inside the relief valve or element 76 sealing washer under the cover 72 Hold relief valve body 71 with suitable wrench to don t lo
104. reverse position for period sufficient to read operational values Verify power in reverse mode of operation with engine operational manual Observe switching on the BETA lamp during transition into reverse IW IN NOTE RPM in reverse should be in the range of 1880 2030 rpm at ambient temperature 50 58 F to 122 and V 0 km h Move engine control lever slowly and smoothly back over idle stop observe switching off the BETA lamp during transition from reverse Idle RPM must be the same like before Check of feathering installation with feathering pump 1 AUTOMATIC FEATHERING check only when this function is involved a Verify AUTOMATIC FEATHERING function according to aircraft flight manual 2 MANUAL FEATHERING check Verify MANUAL FEATHERING according to aircraft flight manual Verify time between switching on and off for FEATHERING PUMP lamp the time must be 12 15 s IO 10 Page 11 46 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER 3 Kontrola funkce NOUZOV PRAPOROV N ID IQ IO ID 190 Vypn te jisti e PRAPOROV N Ovl dac p ku motoru nastavte na doraz volnob hu Ovl dac p ku vrtule p estavte z polohy max ot ek do praporov polohy Po zapraporov n vrtule jsou ot ky cca 350 ot min Ovl dac p ku vrtule p estavte zp t do polohy max ot ek Ot ky p ed a po praporov n mus b t shodn 4 Kontrola funkce
105. simultaneously For the propeller governors LUN 7815 01 and 02 the engine power increases up to maximum reverse power depending on the blade position and the propeller model For the propeller governor LUN 7815 03 the engine power remains engine power at idle up to maximum reverse angle Beta control is realized by pilot using the engine condition lever Pilot valve is out of operation at beta control Blade position is controlled by coaxial valve which controls oil flow to the propeller The outer valve which determines requested position is controlled by engine condition lever behind idle stop The inner valve is turned from beta ring feedback The feedback also switches on the cockpit beta lamp When the blades are in reguired position no oil flows through the coaxial valve figure 11 2 1A When the engine condition lever is moved the outer valve is turned and oil channels are opened Pressurized oil flows either through low pitch channel or through high pitch channel into the propeller figure 11 2 1B When the propeller reaches required position the channels are again closed by moving of beta ring feedback figure 11 2 1C D Feathering If engine failure in an flight it is necessary to feather the propeller Twin engine aircrafts are usually eguipped with feathering system with feathering valve and feathering pump The system is initialized by a cockpit button or automatically a Manual Featherin Pilot activates by
106. speci ln stahov k V ka beta t hel se u t to vrtule nedemontuj pokud to nen nezbytn viz d le a Sestavte stahov k P N 900 0175 dle obr zku 5 18 b O Strana 5 18 20 10 2014 Vnit n p ipojovac z vit t hla stahov ku d kladn nama te p pravkem proti zad en Loctite Moly 50 Loctite 8023 nebo ekvivalent UPOZORN N NENAMAZ N Z VITU ZP SOB JEHO ZADREN UVNIT VRTULE STAHOV K NEBUDE MO N DEMONTOVAT A VRTULE BUDE MUSET B T OPRAVENA V SERVISN M ST EDISKU Instalujte stahov k na vrtuli a skrz otvor ve v ku p i roubujte na p stnici uvnit vrtule obr zek 5 19 Stla te beta syst m vrtule a zasu te beta krou ek k p rub vrtule POZN MKA Pokud zasunut beta krou ku nen dostate n demontujte v ka beta t hel dle postupu v t to kapitole a zasu te beta krou ek ru n Vrtule se p ipev uje na p rubu motoru pomoc matic Ut hn te matice ve dvou kroc ch n sledovn 1 Ut hn te matice v po ad A dle obr zku 5 11 na 40 50 Nm 30 40 Ib ft 2 Ut hn te matice v po ad B dle obr zku 5 11 na 95 110 Nm 70 81 Ib ft Pokud jsou p i instalaci pou ity nesamojistn matice pojist te je nerezov m v zac m dr tem 0 81 mm 0 032 inch v dy dv matice v i sob Po instalaci vrtule na motor uvoln te beta syst m vrtule a demontujte stahov k z vrtule MONT N A PROVOZN INSTRUKCE E 1500 INSTALLA
107. t sn n a ist kryt p ruby 11 Nap ku Zv namontujte zp t nosi kluzn ch kamen s epem podlo kou a z vla kou 12 Hrdla p vod chra te vhodn mi z slepkami 13 Regul tor o ist te nakonzervujte a vlo te do vhodn ho obalu 11 6 Z KLADN SE ZEN PO MONT I NA MOTOR V STRAHA e VSECHNY DEMONT ZN MONT ZN A OPRAV RENSK POSTUPY UVEDEN VT TO PR RU CE MUS B T PROVEDENY PRACOVN KY S P SLU NOU KVALIFIKAC A Vrtulov regul tor LUN7815 1 Se zen regul toru ot ek prvkem B2 plat pro regul tory LUN7815 02 LUN7815 03 POZN MKA Toto se zen prov d jte p i namontovan vrtuli POZN MKA Z kladn se zen minim ln ho letov ho hlu vrtul V508 s regul torem LUN7815 je uvedeno v tabulce 11 1 a Kontrolujte zda je vrtule v praporov poloze a beta krou ek nen vysunut a dosed na vrtulov n boj b Pokud nen vrtule v praporov poloze p estavte ji oto en m za listy sm rem do praporov polohy tak aby beta krou ek dosedl na vrtulov n boj UPOZORN N s VRTULOV LISTY UCHOPTE V KORENOV STI NIKDY NE U PI KY Strana 11 25 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 9 LUN7815 only If the drive shaft is in gear box drive remove it and place into governor shaft NOTE The drive shaft must have marked governor S N 10 Cover the g
108. the slip ring contacts odmrazovac m t les m V p pad pot eby dot hn te Srouby kontakt po and to the de icers Tighten if required Safety the contact screws with red safety dota en pojist te ervenou poji ovac barvou paint after tightening C Zkontrolujte kabely na po kozen c Inspect the cables for damage Strana 6 9 h Page 6 9 6 22012 PROHLIDKY 61 10 00 INSPECTIONS 2012 02 06 AVIA PROPELLER d Zkontrolujte kart e sb ra e na po kozen e Zkontrolujte opot eben kart n sledovn 1 lt Strana 6 10 18 9 2014 Sb ra P N P3560 7 Sejm te zadn kryt sb ra e Zasu te ty inku o pr m ru 2 5 mm 0 1 inch do v ech kontroln ch otvor ve sb ra i Pokud je d lka zasunut do kter hokoliv otvoru v t ne 33 5 mm 1 3 inch v echny uhl ky mus vym n ny Sb ra e P N 068 5320 076 5300 066 5300 Zasu te ty inku o pr m ru 2 5 mm 0 1 inch do v ech kontroln ch otvor v zadn sti sb ra e Pokud je d lka zasunut do kter hokoliv otvoru v t ne 9 mm 0 35 inch v echny uhl ky mus b t vym n ny Sb ra P N LUN7850 7 Zasu te dr t o pr m ru 0 8 mm 0 03 inch do v ech kontroln ch otvor na boku sb ra e Pokud je d lka zasunut do kter hokoliv otvoru v t ne 8 mm 0 315 inch v echny uh lky mus b t vym n ny PROHL DKY E 1500 INSTALLATION AND OPERATION MANUAL d Inspect the brushes of the brush block
109. to the governor to don t obstruct at following works d Ovl dac p ku motoru v kabin letounu p esu te do reverzn polohy P ka Bc na d Move engine condition lever in aircraft cockpit into reverse position Governor lever regul toru se t m p esune do polohy dle obr zku 11 18 ryska p ky s va kou je proti Bc thus moves to position as shown on figure 11 18 guideline at the lever aligns toleran n mu poli reverzu na stupnici regul toru with reverse range at governor scale V STRAHA u WARNING JE ZAK Z NO PRESUNOUT OVL DAC P KU MOTORU DO REVERZN POLOHY IT IS FORBIDDEN TO MOVE ENGINE CONDITION LEVER INTO REVERSE POSITION POKUD OVL DAC P KA VRTULE NEN V POLOZE MAXIM LN CH OT EK WHEN PROPELLER CONDITION LEVER IS NOT IN MAXIMUM RPM POSITION Bc s kulisou Sv Obr zek 11 17 Rozpojen t hla Sv Strana 11 28 13 4 2010 SYST M OVL D N VRTULE Lever Lever wirh gate Sv p Figure 11 17 Rod Sv disconnection Page 11 28 61 10 00 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Toleran n pole reverzu P ka Bc 0 1 0 3mm Prvek37 Obr zek 11 18 Se zen axi ln v le blokovac ho oup tka JE ZAK Z NO P ESUNOUT OVL DAC P KU VRTULE Z POLOHY MAXIM LN CH OT EK DO POLOHY PRAPOR POKUD JE OVL DAC P KA MOTORU V REVERZN POLOZE e Zatla te ru n blokovac oup tko na doraz a l
110. zek 11 9 10 Kulov lo iska prvk dal p slu n povrchy nama te vazel nou Strana 11 16 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Minimum d 29 ground pitch quideline Lever Bc Minimum flight pitch 954 uideline Z Lever Lever Rn bolts BETA rin fiy Feathering stop 16 Maximum RPM stop 15 Spring Control lever T A N 7 Pa Spring Vem Nel Stop 58 Safety stop Figure 11 9 Governor LUN7815 03 View to engine 7 Verify the carbon block assembly figure 11 6 for damage and completeness 8 Grease carbon block assembly pins WARNING REMOVE DAMAGED ASSEMBLY FROM OPERATION 9 Verify function of the microswitch V figure 11 9 by moving lever Zv in the direction of arrow figure 11 10 10 Grease bearings of elements pg and other appropriate surfaces Page 11 16 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL P ka Bc Lever Bc 152 CA A A Upev ovac Mounting roub bolts Op rn krou ek E BETA rin N Governor P regul toru shaft Nosi kluzn ch n AP Carbon block n R kamen 1 assembl EE 1 S41 di d q A 1 OZ SS Om AY k Shaft WW ty ka i drive P ka Zv TE Lever
111. 0 INSTALLATION AND OPERATION MANUAL 2 Idle RPM adjustment 61 10 00 twin engine aircrafts Perform this adjustment only if difference in idle RPM is higher than 40 rpm generator idle speed difference is to 0 5 Check basic adjustment for both governors according to process in section 11 6 If the values don t correspond to that recorded in the governor documentation adjust it them If the basic adjustment for both governors is correct adjust engine idle according to the engine operational manual to decrease the difference under 40 rpm Verify idle speed at engine ground test according to aircraft flight manual at oil temperature 60 65 140 150 F Page 11 60 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER 11 9 ODSTRANOV N Z VAD Z vada Net snost reduk n ho ventilu po se izov n maxim ln ho tlaku Mo n p ina a Vadn t sn c krou ky b Nedota en ventil N prava a Postupujte dle kapitoly Postupy dr by b Postupujte dle kapitoly Postupy dr by Z vada Net snost t lesa zp tn ho ventilu s p pojkou a hrdla s tryskou Mo n p ina a Vadn t sn c krou ky N prava a Postupujte dle kapitoly Postupy dr by Z vada Net snost koaxi ln ch oup tek v t lese zp tn vazby Mo n p ina a Vadn t sn c krou ky N prava a Regul tor vym te Z vada Net snost mezi p rubou regul toru a p rubou redu
112. 0 04 13 2010 04 13 2010 04 13 2010 04 13 2015 05 12 2012 02 06 2012 02 06 2014 10 20 2012 02 06 2012 02 06 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2015 07 07 2010 04 13 2010 04 13 2010 04 13 INSTALLATION AND OPERATION MANUAL LIST OF EFFECTIVE PAGES Page Date of Rev Page 11 21 2010 04 13 11 49 11 22 2010 04 13 11 50 11 23 2010 04 13 11 51 11 24 2010 04 13 11 52 11 25 2010 04 13 11 53 11 26 2010 04 13 11 54 11 27 2012 02 06 11 55 11 28 2010 04 13 11 56 11 29 2012 02 06 11 57 11 30 2012 02 06 11 58 11 31 2012 02 06 11 59 11 32 2012 02 06 11 60 11 33 2010 04 13 11 61 11 34 2010 04 13 11 62 11 35 2012 02 06 11 63 11 36 2012 02 06 11 64 11 37 2012 02 06 11 65 11 38 2012 02 06 11 66 11 39 2012 02 06 11 67 11 40 2010 04 13 11 68 11 41 2012 02 06 11 69 11 42 2010 04 13 11 70 11 43 2010 04 13 11 71 11 44 2010 04 13 11 45 2012 02 06 11 46 2012 02 06 11 47 2010 04 13 11 48 2012 02 06 LIST OF EFFECTIVE PAGES Date of Rev 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2010 04 13 2012 02 06 2012 02 06 2010 04 13 2010 04 13 2012 02 06 2010 04 13 2010 04 13 2012 02 06 2010 04 13 2012 02 06 2012 02 06 2012 02 06 2010 04 13 2010 04 13 2010 04 13 2012 02 06 Page 111 1 2015 07 07 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Tato strana je z m rn
113. 1 Kontrola z kladn ho se zen a Ovl dac p ku vrtule nastavte do polohy max ot ek p ka Rn mus b t na dorazu max ot ek 15 b Ovl dac p ku vrtule nastavte do polohy prapor a zajist te p ka Rn mus b t na dorazu praporu 16 Ovl dac p ku vrtule p estavte zp t do polohy max ot ek Pokud nen prove te se zen podle provozn p ru ky letounu c Ovl dac p ku motoru nastavte na zar ku volnob hu ryska na p ce mus b t proti rysce minim ln ho letov ho hlu na stupnici regul toru obr zek 11 23A ep ovl dac p ky vn j ho koaxi ln ho oup tka mus b t na dorazu volnob hu d Ovl dac p ku motoru p estavte do polohy max reverz ryska na p ce mus b t proti rysce reverzu na stupnici regul toru obr zek 11 23B e Kontrolujte listov mi m rkami se zen prvku 32 dle postupu v kapitole 11 6 f Kontrolujte stranovou v li mezi beta krou kem a kameny nosi e dle postupu v kapitole 11 6 2 Zkou ka funkce vrtulov ho syst mu na zemi Prove te v pln m rozsahu po v m n motoru nebo regul toru ot ek vrtule Po v m n ostatn ch p stroj vrtulov ho syst mu prove te v rozsahu nezbytn m pro ov en funkce dan ho p stroje a Spus te motor podle letov p ru ky letounu b Proh ejte motor na teplotu vstupn ho oleje 60 65 140 150 F c Odvzdu n te vrtulov syst m INST
114. 10 00 TABLE OF CONTENT 2012 02 06 AVIA PROPELLER C slo zm ny Datum vyd n SEZNAM ZM N Zm n n strany E 1500 Stru n popis Rev No Issue Date INSTALLATION AND OPERATION MANUAL LIST OF REVISIONS Revised Page Short Description R 46 10 R 106 10 R 113 10 R 130 10 R 47 11 R 137 11 Strana 11 1 6 12 2011 13 dubna 2010 30 ervna 2010 20 ervence 2010 3 z 2010 11 dubna 2011 10 kv tna 2011 30 ervna 201 1 6 prosince 2011 v echny 1 1 11 1 111 1 5 4 6 1 a 6 12 11 1 11 1 6 2 11 1 111 1 5 6 11 1 1 1 6 5 1 1 Il 1 111 1 1 1 2 1 3 1 4 1 a2 4 3 4 7 5 1 a 5 17 6 4 9 1 11 1 1 1 1 1 2 1 2 2 11 1 1 2 1 1 6 2 6 3 6 15 6 17 a 6 20 9 1 11 48 2 ZM N 2 vyd n Kapitoly 4 5 6 7 9 11 byly zm n ny Zm na n zvu odd l v obsahu dle zm n v kapitole Prohl dky Dopln n typ vazel ny pou it do z vitu listu Kapitola Prohl dky byla kompletn p epracov na Zm na je ozna ena jen na za tku kapitoly P edletov prohl dka Kontrola funkce vrtule po spu t n motoru se nov odkazuje na letovou p ru ku letounu Dopln na mo nost pou it shodn ch komponent pro odmrazov n B a C Zru en utahovac moment v ka omezova e a stanoven nov postup pro uta en v ka Kapitola Omezen letov zp sobilosti
115. 2 60 2 61 2 62 2 63 2 64 2 65 2 66 2 67 Bushing Liner Screw Spinner flange Pin Pin Back bushing Liner Pin Pin Front bushing Pin Washer Screw Screw Castle nut Washer Cotter pin Screw Screw Lock washer Screw Selflocking nut Washer O ring O ring Sealing O ring O ring O ring O ring O ring O ring O ring Screw Bushing 2 68 2 69 2 70 2 71 2 72 2 73 2 74 2 75 7 15 7 16 7 17 7 18 Slide valve Support Washer Spring Spacer Retaining ring Reverse stop O ring Spinnerdome Spinner bulkhead Nutplate Nutplate Rivet Screw Washer Slip ring assy Spacer ring Cable assy Lead clip Screw Nut Washer Cable holder Screw Washer Screw Screw Nut Terminal plate Insert Spacer Brush block assy Screw Washer Table 4 2 Partlist reffering to Figure 4 2 DESIGN AND OPERATION INFORMATION Page 4 7 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL
116. 22 F a V 0 km h 5 Ovl dac p ku motoru p esu te pomalu a plynule p ed doraz volnob hu 5 kontrolujte zhasnut signalizace BETA zen Volnob n ot ky p ed a po reverzu mus b t shodn i Kontrola praporov n vrtulov ho syst mu i z stavba s praporovac m erpadlem 1 Kontrola funkce AUTOMATICK PRAPOROV N jen p i z stavb syst mu s automatickou funkc praporov n a Kontrolujte funkci AUTOMATICK PRAPOROV N podle Letov p ru ky letounu 2 Kontrola funkce RU N PRAPOROV N a Kontrolujte funkci RU N PRAPOROV N podle Letov p ru ky letounu b Na palubn ch stopk ch kontrolujte dobu od rozsv cen do zhasnut signalizace PRAPOROV ERPADLO mus b t 12 15 s DDD SYST M OVL D N VRTULE 61 10 00 6 2 2012 INSTALLATION AND OPERATION MANUAL Propeller control lever function check Engine control lever in maximum continuous power position Set with propeller control lever propeller RPM to 1900 rpm then reduce RPM with propeller control lever to 1700 rpm and back to previous position Propeller speed must be adequate to propeller control lever position IDE WARNING TORQUE MUST NOT EXCEED 100 Speed in reverse mode and reverse power check Set propeller control lever to maximum RPM position Place engine control lever to idle Move engine control lever over the stop move slowly and smoothly into maximum
117. 3 inch 11 15 0 1 mm 0 59 0 004 inch 2 2 mm 0 087 inch 10 15 0 1 mm 0 59 0 004 inch LUN7816 02 3 4 mm 0 134 inch 14 13 0 1 mm 0 512 0 004 inch 2 7 mm 0 106 inch 13 13 0 1 mm 0 512 0 004 inch 2 1 mm 0 083 inch 12 14 0 2 mm 0 551 0 008 inch 1 4 mm 0 055 inch 11 15 0 1 mm 0 59 0 004 inch 4 ROW1 0101 01 0 8 mm 0 0315 inch 10 15 0 1 mm 0 59 0 004 inch Tabulka 11 3 Nastaven min letov ho hlu vrtul ady V510 s regul torem LUN7816 f P i se izov n d lky t hla prvku 32 dbejte aby v le mezi beta krou kem a kameny f byla rovnom rn rozd lena na ob strany Celkov v le mezi beta krou kem a kameny je u nov ho nosi e kluzn ch kamen 0 15 0 18 mm 0 006 0 007 inch obr zek 11 16 Maxim ln dovolen v le v provozu je 0 4 mm P i mont i regul toru doporu ujeme tuto v li zm it n sleduj c m zp sobem p itla te lehce nosi kluzn ch kamen k jedn stran beta krou ku a celkovou v li zm te l stkov mi m rkami g Po se zen a zm en v le dot hn te ob matice t hla prvku 32 obr zek 11 24 g lev a prav z vit a pojist te v zac m dr tem Strana 11 37 6 2 2012 SYST M OVL D N VRTULE 61 10 00 Table 11 3 Minimum flight pitch adjustment of propellers V510 Type Series Axial clearance between the beta ring and carbon blocks is egually divided to both sides when the element 32 is ad
118. 7 14 Podlo ka 2 31 Bearing cage 2 70 Selflocking nut 7 14 Washer 2 32 Kuli ka 2 71 Podlo ka 7 15 Stahovac p ska 2 32 Ball 2 71 Washer 7 15 Cable tie 2 33 Klec lo iska 2 72 O krou ek 7 30 Sestava sb ra e 2 33 Bearing cage 2 72 O ring 7 30 Brush block assy 2 34 V le ek 2 73 O krou ek 2 34 Roller 2 73 O ring 2 35 Klec lo iska 2 74 O krou ek 2 35 Bearing cage 2 74 O ring Tabulka 4 4 Seznam d l k obr zku 4 4 Table 4 4 Partlist reffering to Figure 4 4 PUANA A T KONSTRUK N A PROVOZN INFORMACE 61 10 00 DESIGN AND OPERATION INFORMATION rage d 18 9 2014 bh 2014 09 18 Strana 5 1 20 10 2014 AVIA PROPELLER MONT ZN A PROVOZN INSTRUKCE OBECN UPOZORN N NIKDY NEOP REJTE VRTULI O BETA KROUZEK JINAK M ZE DOJ T K JEHO POSKOZEN A NESPR VN FUNKCI ZP TN VAZBY PREPRAVN Z TKU DEMONTUJTE Z P RUBY VRTULE A PO ZAV EN NA ZDVIHAC ZA ZEN P I MONT I NA MOTOR 1 K instalaci vrtule na motor pou ijte vhodn zdvihac za zen a z v sn popruhy VAROV N m m NOSNOST ZAR ZEN A POPRUH MUS BYT MINIM LN 200 KG 440 LBS UPOZORN N PRI ZVED N VRTULE DBEJTE ABY NEDO LO K POSKOZEN ODMRAZ T LES NA LISTECH POKUD JSOU INSTALOV NA OD POPRUH a Pokud instalujete na motor vrtuli bez instalovan ch list zav ste vrtuli na je b pomoc speci ln ho z v su za roubovan ho do jednoho z pouzder listu viz kapitola Speci ln n ad
119. 8 2015 07 07 2010 04 13 2012 02 06 2012 02 06 2014 01 17 2012 02 06 2012 02 06 2011 05 10 2014 01 17 2011 05 10 2011 05 10 2014 09 18 2014 01 17 2012 02 06 2014 01 17 2012 02 06 2014 01 17 Page 4 9 4 10 4 11 5 1 5 2 5 3 5 4 5 5 5 6 5 7 5 8 5 9 5 9 1 5 9 2 5 9 3 5 10 5 11 5 11 1 5 12 5 13 5 14 5 15 5 16 5 17 5 18 5 19 6 1 6 2 Date of Rev 2012 02 06 2014 01 17 2014 09 18 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2014 10 20 2012 02 06 2014 09 18 2015 07 07 2014 09 18 2012 02 06 2012 02 06 2011 05 10 2012 02 28 2012 02 06 2014 10 20 2014 10 20 2012 02 06 2012 02 06 P EHLED PLATN CH STRAN Page 6 3 6 4 6 5 6 7 6 8 6 9 6 10 6 11 6 12 6 13 6 14 6 15 6 16 7 1 7 2 7 3 7 5 7 6 7 7 7 8 7 9 7 10 7 11 8 1 8 3 8 4 1500 Date of Rev 2011 12 06 2012 02 06 2010 06 30 2012 02 06 2010 06 30 2012 02 06 2014 09 18 2012 02 06 2012 02 06 2012 02 06 2015 05 12 2012 02 06 2012 02 06 2010 04 13 2010 04 13 2010 04 13 2012 02 06 2015 07 07 2014 01 17 2012 02 28 2012 02 06 2014 01 17 2015 07 07 2015 07 07 2012 02 06 2010 04 13 2010 04 13 2010 04 13 Page 8 5 8 6 8 7 8 8 9 1 10 1 10 2 10 3 11 1 11 2 11 3 11 4 11 5 11 6 11 7 11 8 11 9 11 10 11 11 11 12 11 13 11 14 11 15 11 16 11 17 11 18 11 19 11 20 61 10 00 Date of Rev 201
120. 815 03 View from propeller UPOZORN N CAUTION NEINSTALUJTE REGULATOR S NASAZENYMI KLUZNYMI KAMENY POKUD JE DO NOT INSTALL THE GOVERNOR WITH THE CARBON BLOCK ASSEMBLY VRTULE INSTALOVANA NA MOTORU INSTALLED WHEN THE PROPELLER IS INSTALLED 14 Pou ijte spr vn a ist t sn n Ustavte regul tor na reduktor motoru ozuben 14 Use correct and clean packing Place the governor onto engine gear box Drive rod torzn ty inky mus zapadnout do n honu v reduktoru gearing must be correctly inserted into the gear box drive 15 P ipevn te regul tor ty mi rouby obr zek 11 7 p i pou it vhodn ho kl e Pru n 15 Fix the governor using four bolts figure 11 7 using suitable wrench A spring washer podlo ka je pod hlavou roubu a dal podlo ka je vlo ena do vybr n v p rub is at bolt head and the second washer is inserted into governor flange recess with regul toru sra en m dovnit Pojist te nejm n t i rouby nerezov m v zac m dr tem chamfer facing governor Secure at least three bolts using stainless steel lock wire obr zek 11 7 figure 11 7 Strana 11 18 EVA N Page 11 18 13 4 2010 SYSTEM OVLADANI VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 16 Pokud vrtule nen v praporov poloze nato te listy do praporu tak aby beta krou ek dosedl na p rubu vrtule UPOZORN N M VRTULOV LISTY UCHOPTE V KO ENOV STI NIKDY NE U PI KY
121. 89 onto the turning screw 78 and the feedback body 45 with ring 88 in position shown it is arrow up figure 11 36 and screw the turning screw into the governor body without final tightening The ball 92 shall be in socket 44 WARNING USE ONLY ALLOWED SEALING RINGS ALUMINUM Reinstall back both removed tubes 86 87 Tighten finally the turning screw 78 and the tubes 86 and 87 carefully with continuous tightening of all tube cap nuts and turning screws Tighten the tubes also on the second end Finally secure the turning screw 78 with the nut 59 and both tube cap nuts with lock wire using standard locking procedure Secure also the second end of the tubes Page 11 67 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER ed ER eo Wa MI PESSSSS 5 ww NA Obr zek 11 36 V m na t sn c ch krou k 6 V m na t sn c ch krou k t lesa zp tn ho ventilu V p pad net snosti t lesa zp tn ho ventilu vym te t sn n n sleduj c m zp sobem Sejm te v zac dr t z matice trubky 86 obr zek 11 37 nebo matice trubky 87 eventu ln z obou matic dle zji t n z vady Sejm te trubku 86 a 87 eventu ln ob POZN MKA Ne trubky sejmete mus te je t povolit na jejich druh m konci Po sejmut hrdla 46 nebo hrdla 44 z t lesa zp tn ho ventilu 45 vysu te t sn c krou ek 90 nebo t sn c krou ek 91 za nov UPOZORN N DEJTE POZOR
122. ALLATION AND OPERATION MANUAL B Propeller Governor LUN7816 1 Basic adjustment check a Propeller condition lever must be placed in maximum RPM position and then the lever Rn must be at maximum RPM stop 13 b Place the propeller condition lever into the feather position and fix the lever Rn must be located at its feather position 16 Place the propeller condition lever back to the maximum RPM position c Place the engine condition lever to the idle stop guideline on the cam lever must align with minimum flight pitch guideline on the governor scale figure 11 234 The pin of outer coaxial valve must touch the idle stop d Place the engine condition lever into maximum reverse position guideline on the cam lever must be aligned with BETA range on the governor scale figure 11 23B Verify element 32 setting using feeler gauge according to procedure in section 11 6 f Verify a side clearance between the beta ring and the carbon block assembly according to procedure in section 11 6 2 Propeller control system ground test Perform after engine or propeller governor exchange in full scope Perform in the sufficient appropriate scope to verify appropriate functionality after exchange of other propeller control system instruments a Start the engine according to the aircraft flight manual b Warm up engine lubricating oil to 60 65 140 150 F c Purge the propeller contro
123. CING TOWARD THE BOLT HEAD FIGURE 5 10 S Insert the mounting bolts through the engine flange and screw into mounting holes in the propeller flange CAUTION WHEN INSTALLING THE PROPELLER BY USING THE GUIDE PINS UNSCREW THEM FROM THE PROPELLER FLANGE THROUGH THE ENGINE FLANGE AFTER THE MINIMUM OF TWO MOUNTING BOLTS HAS BEEN INSTALLED Page 5 9 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL SRAZEN PODLOZKY CHAMFER OF WASHER Obr zek 5 10 Figure 5 10 c Momentovym kl em s n stavcem 19 mm 3 4 inch ut hn te mont n c Using the torque wrench and 19 mm 3 4 inch adaptor torque all mounting rouby podle postupu na obr zku 5 11 bolts using the procedure shown in Figure 5 11 d Pojist te v echny mont n rouby nerezov m v zac m dr tem 0 81 mm d Safety all mounting bolts with 0 81 mm 0 032 inch stainless steel safety 0 032 inch v dy dva rouby v i sob wire two bolts per safety UPOZORN N m uU CAUTION V ZAC DRAT NESM PRESAHOVAT PRES VNEJSI PR M R THE SAFETY WIRE MUST NOT PROTRUDE OVER THE OUTSIDE PRIRUBY VRTULE A MOTORU DIAMETER OF THE PROPELLER FLANGE AND ENGINE FLANGE 11 Pouze vrtule V508H 11 V508H propeller only Nainstalujte d ly beta syt mu zp t do vrtule obr zek 5 8 Reinstall the beta system parts back into the propeller Figure 5 8 a Ru n odt hn te beta krou
124. DU LETOUNU V PR PAD VIBRAC MUS B T NEPRODLEN ZJI T NA A ODSTRAN NA PR INA a Zji ov n p vodu vibrac za n v t inou kontrolou motoru Zdrojem vibrac mohou b t tak komponenty letounu jako jsou z v sy motoru nebo uvoln n kryty podvozku Prove te vy et en mo n ch zdroj vibrac dle p ru ky motoru a nebo letounu Pokud nebyla zji t na p ina vibrac postupujte dle dal ch bod ABNORMAL VIBRATION CAN INDICATE THE DAMAGE OF PROPELLER BLADE OR BLADE BEARING COMPONENT IT MAY LEAD TO IN FLIGHT BLADE SEPARATION AND CATASTROPHIC AIRCRAFT ACCIDENT THE SOURCE OF VIBRATION MUST BE IMMEDIATELY DETERMINED AND CORRECTED b Sejm te p edn kryt vrtule a prove te vizu ln kontrolu list a v ech viditeln ch d l vrtule na v skyt trhlin po kozen a jin ch neobvykl ch jev V p pad zji t n trhlinek nebo jak chkoliv pochybnost kontaktujte Avia Propeller c Zkontrolujte spr vnou polohu list v pouzdrech Ov te e pozi n ryska na ko eni listu se kryje s ryskou na ele pouzdra listu Max tolerance pro p esazen rysek na listu a pouzdru je 1 2 tlou ky rysky na listu V opa n m p pad prove te p einstalaci listu dle kapitoly Mont n a provozn instrukce v t to p ru ce d Zkontrolujte polohu obj mek se z va mi Spr vn poloha obj mek je pops na v kapitole Mont n a provozn instrukce tohoto manu lu e Zkontrolujt
125. E 1500 INSTALLATION AND OPERATION MANUAL 2 M stn oprava na n b zn a odtokov hran 2 Local repair of leading and trailing edge a List vrtule V508 a V508 propeller blade Hloubka po et a poloha m stn ch oprav je uvedena na obr zku 7 4 a Refer to figure 7 4 and table 7 1 for allowable depth number and location of v tabulce 7 1 Z zen ky max 1 mm 0 04 inch na n b n hran max 2 mm 0 08 inch na odtokov hran the local repairs Reduction in width max 1 mm 0 04 inch for leading edge max 2 mm 0 08 inch for trailing edge LEADING EDGE ODTOKOV HRANA TRAILING EDGE 4 0 mm 18 5 inch 470 mm 18 5 inch Obr zek 7 4 Oblasti listu V508 souvisej c s tabulkou 7 1 Figure 7 4 V508 blade areas referring to Table 7 1 Maxim ln po Maxi Oblast listu bs Maxim ln Max celkov Area of the blade ir esl akasi Maximum 195 rur prav of repairs max depth m eno od pi ky dle N b n Odtokov hloubka hloubka oprav measured from the tip sad Trail depth of ofobbosite obr zku 7 4 tokov jedn opravy proti sob acc to Figure 7 4 irang single repair edge repairs od pi ky do 70 mm 1 1 5mm 10 mm from tip to 70 mm 1 1 5 mm 10 mm od pi ky d
126. ELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 2 tolerance nelze dos hnout se zen m ot ek gener toru motoru c Po se zen dorazu b8 znovu kontrolujte volnob n ot ky vrtul p i motorov zkou ce p i teplot oleje 60 65 140 150 F d V atestu regul toru zjist te rozm ry B a e Zm te rozm ry B u regul tor podle obr zku 11 32 a porovnejte je s hodnotami e uveden mi v atestech P ed m en m kontrolujte polohy zar ek na ovl dac p ce mus b t na dorazech 58 Ovl dac p ka Doraz 58 ti Bezpe nostn doraz Obr zek 11 32 Kontrola rozm ru B f Nam te li hodnotu rozm ru B odli nou o v ce ne 0 1 mm oproti hodnot f uveden v osv d en upravte rozm r B dle osv d en se zen m dorazu 58 a kontrolujte ot ky obou vrtul p i motorov zkou ce podle letov p ru ky letounu g Jsou li oba rozm ry shodn s rozm ry udanymi v atestech provedte se zen doraz g 58 obou regul tor na z klad zji t n ch volnob n ch ot ek viz n e a to z jejich polovi n ho rozd lu Polovi n hodnotu rozd lu ot ek vyhledejte v tabulce 11 5 kde ode tete hodnotu pooto en dorazem 58 a sm r lana Hor SYST M OVL D N VRTULE 61 10 00 6 2 2012 INSTALLATION AND OPERATION MANUAL 2 Itis not possible keep this tolerance with idle power Verify a
127. ERATION 9 Verify functionality of the microswitch V figure 11 12 by moving lever Zv in the direction of arrow figure 11 13 Page 11 21 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL S X 32 Obr zek 11 14 Regul tor LUN7816 Pohled sm rem od vrtule 10 Kulov lo iska prvku 29 a 32 lehce nama te doporu en m plastick m mazivem 11 Kontrolujte dosedac plochu p ruby regul toru s centr a p rubu na reduktoru motoru Plochy mus b t ist bez po kozen povrchu Plochy o ist te ist m hadrem p padn namo en m do rozpou t dla 12 Zkuste ot et h del regul toru Jej pohyb mus b t voln 13 Pokud je instalov na vrtule sejm te nosi kluzn ch kamen z p ky Zv obr zek 11 6 UPOZORN N NEINSTALUJTE REGUL TOR S NASAZENYMI KLUZNYMI KAMENY POKUD VRTULE INSTALOV NA NA MOTORU Figure 11 14 Governor LUN7816 View from propeller 10 Grease bearings of elements pg and other appropriate surfaces 11 Verify governor flange and gear box flange Both surfaces must be clean and free from any damage Use a clean cloth eventually with cleaning solvent to wipe seating faces 12 Try to turn with drive rod The rod should rotate freely 13 If the propeller is installed remove carbon block assembly form lever Zv
128. ES 1 The hub arms and the blades are marked with position numbers in ascending 2 O ist te ko en listu a vnit ek pouzdra listu od ve ker ch ne istot 2 3 Ov te e na ko enu listu je instalov n o krou ek obr zek 5 2 3 UPOZORN N O KROU EK BR N VNIK N VLHKOSTI DO Z VITU KOROZE V Z VITU LISTU A NEBO POUZDRA LISTU M E V ST KE ZTR T LETOV ZP SOBILOSTI VRTULE 4 Lehce nama te z vit a konec ko ene listu vazel nou Aeroshell Grease 5 nebo 4 6 obr zek 5 2 UPOZORN N V LCOV ST KORENE LISTU OD Z VITU SM REM KE PI CE NESM B T NAMAZ NA PRED INSTALAC LISTU DO VRTULE SE UJIST TE E TATO ST KORENE JE SUCH Strana 5 3 MONT N A PROVOZN INSTRUKCE 61 10 00 20 10 2014 lt AZ sequence from number 1 Always install the blade into the arm with corresponding position number a Position number of the hub arm is stamped on the arm b Blade position number follows the blade set number on the shank face for example S 274 2 Older blades may have the position number at the propeller serial number New manufactured or overhauled blades also have the position number printed on the label CAUTION INSTALLATION OF THE BLADES IN THE HUB IN INCORRECT ORDER MAY LEAD TO EXCESSIVE VIBRATIONS IN OPERATION Clean the blade shank and inside of the blade bushing from all contaminants Make sure that o ring is installed in the groove in the blade shank Figure 5
129. ES RAPID TEMPERATURE DROP CAN CAUSE THE WATER IN THE BEARING MAY FREEZE THE ICE DEFORMED SEALS INSIDE THE BEARING IT LEADS TO HEAVY OIL LEAKAGE FROM THE HUB A CLEANING DO NOT USE PRESSURE WASHING EQUIPMENT TO CLEAN THE PROPELLER OR CONTROL COMPONENTS PRESSURE WASHING CAN FORCE WATER AND OR CLEANING SOLVENTS PAST SEALS AND CAN LEAD TO CORROSION OF INTERNAL PROPELLER COMPONENTS DO NOT USE AN CAUSTIC OR ACIDIC SOLUTIONS TO CLEAN ANY PROPELLER PART DO NOT USE ANY SOLVENT DURING CLEANING THAT COULD SOFTEN OR DESTROY THE BOND BETWEEN CHEMICALLY ATTACHED PARTS BEFORE USING OF SOME CLEANER OBSERVE THAT THE CLEANER HAS NOT ANY NEGATIVE EFFECTS FOR METAL SURFACES AND PAINTS B DYNAMIC BALANCE NOTE All manufactured or overhauled propellers are statically balanced Dynamic balance is recommended but not required unless specified by airframe or engine manufacturer Page 7 1 MAINTENANCE 2010 04 13 AVIA PROPELLER 1 Obecn Dynamick vyva ov n se prov d p esn m za zen m zji uj c m velikost a polohu dynamick nevyv enosti Po proveden m vyva ov n nesm b t zbytkov nevyv enost v t ne 0 2 ips Postupujte dle instrukc v robce vyva ovac ho za zen Pokud je dynamick nevyv enost v t ne 1 2 ips mus b t vrtule sta ena z provozu a vyv ena staticky 2 Kontroln postupy p ed vyva ov n m a Vizu ln zkontrolujte vrtuli instalovanou na letounu POZ
130. Figure 11 4 Governor LUN7815 02 View from engine 7 Secure with suitable manner the rod Sv 65 against moving NOTE Install the rod after governor basic adjustment see section 11 6 8 With lever Rn at maximum RPM stop 15 verify lever Bc travel from basic position up to reverse when the guideline on the lever with cam is against reverse range on the governor scale Then move the lever Bc further to safety stop CAUTION THE LEVER Bc SHOULD BE FREE THE LEVER HAS SOME DRAFT AT INITIALIZATION OF THE LOCKING MECHANISM NO 37 Page 11 10 2010 04 13 PROPELLER CONTROL SYSTEM AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 5223 UNI Obr zek 11 5 Regul tor LUN7815 02 Pohled sm rem od vrtule Figure 11 5 Governor LUN7815 02 View from propeller 9 Kontrolujte nosi kluznych kamen obr zek 11 6 na po kozen a kompletnost 9 Verify the carbon block assembly figure 11 6 for damage and completeness 10 epy nosi e kluzn ch kamen nama te vazel nou 10 Grease carbon block assembly pins with grease UPOZORN N VADN NOSI KLUZN CH KAMEN VY A TE Z PROVOZU WARNING REMOVE DAMAGED CARBON BLOCK ASSEMBLY FROM OPERATION 11 Pohybem p ky Zv ve sm ru ipky obr zek 11 4 se p esv d te poslechem 11 Verify function of the microswitch V figure 11 3 by moving lever Zv in the sepnut mikrosp na e V obr zek 11 3 direction of arrow fi
131. I LETOVE ZPUSOBILOSTI 61 10 00 AIRWORTHINESS LIMITATIONS 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 2 OBECN 2 GENERAL A Obsah A Statement of purpose Strana 2 1 17 1 2014 Tento dokument poskytuje informace o provozu instalaci a drzb vrtul Avia Propeller typov ch ad V508 3 list a V510 5 list s praporovou a reverza n polohou vrtulovych list Vrtule v t to p ru ce jsou ur eny pro provoz na turb novych motorech s mont n p rubou ARP880 Krom vrtulov jednotky jsou v t to p ru ce uvedeny i informace o syst mu ovl d n vrtule na motorech M601 s regul tory LUN7815 a LUN7816 Informace o instalaci demont i provozu a vyhled v n z vad jsou uvedeny v t to p ru ce Doporu uje se s touto p ru kou pou vat z rove provozn p ru ku letounu a motoru B Gener ln oprava Limity TBO v ech vrtul Avia jsou uvedeny v posledn m vyd n Servisn ho bulletinu Avia 1 kter je dostupn na webov ch str nk ch Avia Propeller na www aviapropeller cz Gener ln oprava je pravideln proces prov d n ve stanoven ch intervalech p i kter m je vrtule rozebr na a zkontrolov na Po kozen d ly jsou opraveny nebo vym n ny V echny t sn c prvky jsou vym n ny Protikorozn povrchov ochrany d l jsou obnoveny Vrtule je znovu smontov na nastavena a vyv ena Intervaly gener ln ch oprav se obvykle ozna
132. IL INLET PROPELLER REVERSE POSITION ENGINE CONDITION LEVER IN AIRCRAFT COCPIT TO ENGINE CONDITION LEVER Figure 11 2 1 Governor function in beta mode of operation Strana 11 7 13 4 2010 SYSTEM OVLADANI VRTULE 61 10 00 PROPELLER CONTROL SYSTEM Page 11 7 2010 04 13 AVIA PROPELLER b Automatick praporov n Postup je stejn jako p i manu ln m praporov n s t m rozd lem e sepnut praporovac ho erpadla prob hne automaticky na z klad vyhodnocov n krout c ho momentu vrtule Automatick syst m je obvykle omezen pro ur it rozsah ovl dac p ky motoru innost je signalizov na kontrolkou v kabin obvod Ize vypnout c Nouzov praporov n Pou v se v p pad e praporovac erpadlo nepracuje nebo nen instalov no Nouzov praporov n provede pilot p esunut m ovl dac p ky vrtule do polohy pro praporov n Listy vrtule jsou tla eny do praporu p soben m momentu od z va vrtule p padn tlakem oleje P echod vrtule do praporu je v tomto p pad asi t ikr t del ne p i manu ln m nebo automatick m praporov n Nouzov praporov n lze vyu t p i zastavov n motoru 11 4 MONT REGUL TORU NA MOTOR A Vrtulov regul tor LUN7815 02 1 Zkontrolujte stav regul toru nesm b t viditeln po kozen 2 Zkontrolujte zda je na p ce Rn ustavena ta n pru ina obr zek 11 3 3 Zkontrolujte zaji t n v ech element obr
133. KONTROLN PRAPOROV N 110 IQ IO 17 IV g h Ovl dac p ku motoru nastavte do polohy max trval ho v konu Ovl dac p ku vrtule nastavte ot ky vrtule na 1900 ot min Zapn te jisti e PRAPOROV N Stiskn te tla tko TEST PRAPOR Kontrolujte rozsv cen signalizace PRAPOR ERPADLO Ihned po rozsv cen signalizace PRAPOR ERPADLO tla tko uvoln te signalizace zhasne Ot ky vrtule vokam iku rozsv cen mus z stat konstantn Ovl dac p ku vrtule p estavte do polohy max ot ek vrtule Ovl dac p ku motoru nastavte na doraz volnob hu j Kontrola praporov n vrtulov ho syst mu Z stavba bez praporovac ho erpadla 1 Kontrola funkce NOUZOV PRAPOROV N IO Im Strana 11 47 13 4 2010 Ovl dac motoru nastavena doraz volnob hu Ovl dac p ku vrtule p esu te z polohy max ot ek do praporov polohy a zajist te Po zapraporov n vrtule jsou ot ky cca 350 ot min Ovl dac p ku vrtule odjist te a p esu te zp t do polohy max ot ek Ot ky p ed a po praporov n mus b t shodn prove te kontrolu t snosti spoj vrtule provedenou zkou ku zapi te do Z znamn ku vrtule SYST M OVL D N VRTULE E 1500 61 10 00 ID IQ IO ID 10 INSTALLATION AND OPERATION MANUAL 3 EMERGENCY FEATHERING check Switch off FEATHERING breaker Set engine control lever
134. LADE TIP NOTE It is recommended to move the lever Rn to feather stop 16 to facilitate servomechanism movement 17 Install the carbon block assembly figure 11 6 onto the lever Zv and the beta ring Install the washer and safety with cotter pin 1 6x10 NOTE Use new cotter pin each installation 18 Connect rod from RPM control system to the lever Rn figure 11 9 and secure 19 Connect the control rod from engine to the lever Bc in its basic position and secure 20 Connect plug to the beta switch and secure 21 Adjust the governor according to procedure in this section C Propeller Governor LUN7816 1 Verify governor condition for damage No damage acceptable 2 Verify installation of spring on the lever Rn figure 11 12 3 Verify locking devices of appropriate elements figures 11 12 11 13 11 14 NOTE Secure turning bolt tube cap nut sockets and closing nut figure 11 8 after tubing installation 4 Verify seals and securing figures 11 12 11 13 Page 11 19 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL gt Ryska T hlo 29 j reverzu P ka Bc Rod 29 Reverse guideline Lever Bc Ryska min oco MT GI Minimum flight pitch letov ho hlu 7 ALL uideline EN S i TA A A P ka Rn S Lever Rn Op my krou ek BETA ring l Doraz Feathering praporu 16 Doraz max Maximum ot
135. LIV D LY JAKO JE NAP EP 52 POJISTN KROU KY 81 NOSI KLUZN CH KAMEN 22 KLOUBOV LO ISKA T HEL ATD NESM B T P I MYT ZBAVENA VAZEL NY P PADN JE NUTN JE ZNOVU NAMAZAT 2 Kontrola se zen reduk n ho ventilu obr zek 11 34 POZN MKA U regul tor ady LUN7816 se jedn o kontrolu tlaku pod reduk n m ventilem 1 RV Odjist te a vy roubujte matici 59 s kuli kou 60 z dut ho roubu 78 Na dut roub 78 p ipojte tlakovou hadici 114 s manometrem a um st te ji tak aby stupnice manometru byla dob e iteln z kabiny letounu Hadici upevn te tak aby se nedot kala tepl ch st motoru Spus te motory dle letov p ru ky a proh t motorov olej na 60 65 140 150 F Ovl dac p ku vrtule nastavit do polohy maxim ln ch ot ek Ovl dac p ku motoru p esunout do polohy aby bylo dosa eno 1950 a 2080 ot min Ode t te daj manometru Ode ten pod reduk n m ventilem by pro regul tory ady LUN7816 m la b t v rozmez 2 6 a 2 85 MPa nen li pro danou aplikaci nastavena jin hodnota U regul toru LUN7815 02 jsou hodnoty tlak uvedeny v tabulce 11 6 Se zen tlaku pod reduk n m ventilem je pops no v n sleduj c kapitole Strana 11 63 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 11 10 MAINTENANCE PRACTICES There are described maintenance practices in this section together for all gove
136. LLATION AND OPERATION MANUAL Trouble Propeller rpm in flight does not reach maximum rpm Probably cause a Propeller condition lever does not reach maximum rpm stop b Incorrect adjustment of the propeller governor c Pressure in propeller control system is not sufficient Remegy a Verify control linkage place the lever into position of maximum rpm Follow instruction of engine manufacturer b Adjust the propeller governor per instruction of engine manufacturer C Perform relief valve pressure check and adjust if necessary Follow instruction of engine manufacturer Trouble Propeller rpm exceeds maximum rpm Probably cause a Incorrect adjustment of the propeller governor b Defective propeller governor Remegy a Adjust the propeller governor per instruction of engine manufacturer b Replace the propeller governor per instruction of engine manufacturer Trouble Fast rpm decrease Probably cause a Governor drive broken b Loss of oil pressure Remegy a Follow instruction of engine manufacturer b Follow instruction of engine manufacturer Page 8 3 2012 02 06 AVIA PROPELLER Z vada Vysok p ekmity vrtule p i akceleraci Mo n p ina a Nespr vn se zen minim ln letov hel vysunut beta krou ku b Vadn regul tor N prava a Zkontrolujte pop pad se i te nastaven minim ln ho letov ho hlu Verze V508H kapitola Mont n a provozn instr
137. LN s Da oU ROL P UU MMC uuu F ze SN A 2 8 0 6 Obr zek 11 1 Funkce regul toru ot ek SYST M OVL D N VRTULE 61 10 00 Figure 11 1 Propeller governor function PROPELLER CONTROL SYSTEM INSTALLATION AND OPERATION MANUAL Page 11 4 2010 04 13 AVIA PROPELLER C Beta zen Beta zen se pou v pro sn en tahu vrtule p i poj d n a pro dosa en z porn ho tahu po p ist n letounu Umo uje nastaven jak koliv polohy mezi minim ln m letov m hlem a maxim ln m reverzem za sou asn ho nastaven odpov daj c ho v konu motoru U vrtulov ch regul tor ot ek LUN7815 01 a 02 se v kon motoru v reverzu zvy uje a do max reverzn ho v konu v z vislosti na nastaven list podle typu vrtule U vrtulov ho regul toru LUN7815 03 z st v v kon motoru v reverzu na volnob n m re imu Beta zen prov d pilot ovl dac p kou motoru oup tko ot kov regulace je v re imu beta zen vy azeno z innosti Ovl d n vrtulov ch listu p eb r koaxi ln oup tko list je ovl d no p kou ovl d n motoru za zar kou volnob hu Vnit n oup tko je ot eno zp tnou vazbou od beta krou ku vrtule innost v oblasti beta zen je signalizov na kontrolkou v kabin letounu P i nastaven poloze vrtulov ch list je pr tok koaxi ln mi oup tky uzav en obr zek 11 2A
138. LO EN TOTO VEDE K SILN MU NIKU OLEJE Z VRTULE A I T N PRO IST N VRTULE A OVL DAC CH PRVK NEPOU VEJTE ZAR ZEN PRO TLAKOV MYT TLAKOV MYT M E ZP SOBIT ZATE EN VODY A NEBO MYC HO PR PRAVKU POD T SN N COZ M ZE V ST KE KOROZI VNITRN CH KOMPONENT VRTULE NEPOU VEJTE DN P PRAVKY NA B ZI RAVIN NEBO KYSELIN PRO MYT JAK KOLIV STI VRTULE NEPOU VEJTE DN MYC P PRAVEK KTER M E NARU IT NEBO ZNI IT LEPEN SPOJE P ED POU IT M KA D HO P PRAVKU SE UJIST TE E P PRAVEK NEM DN NEGATIVN INKY NA KOVOV POVRCHY A N T RY B DYNAMICK VYV EN POZN MKA V echny vyroben nebo opraven vrtule jsou staticky vyv eny Dynamick vyv en se doporu uje ale nen nezbytn nen li v robcem letounu nebo motoru stanoveno jinak Strana 7 1 13 4 2010 k E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 7 MAINTENANCE There are no freguent maintenance works reguired on the hub because all moving parts are inside the hub and not exposed to the environment Blade bearings and pitch change mechanism are filled with service oil during propeller operation A corrosion protection of the hub with thinned engine oil or anticorrosion spray is recommended CAUTION AVIA PROPELLER STRONGLY RECOMMENDS TO SUITABLE PROTECT THE BLADE BEARINGS AGAINST INTRUSION OF WATER INTO THE BEARING NO NEED FOR HANGARED AIRPLAN
139. N HRANY OTVORU PODLO KY MUS SM OVAT K HLAV ROUBU OBR ZEK 5 10 Skrz p rubu motoru za roubujte rouby do mont n ch otvor v p rub vrtule UPOZORN N POKUD INSTALUJETE VRTULI S POMOC VOD C CH EP PO ZA ROUBOV N NEJM N DVOU MONT N CH ROUB JE VY ROUBUJTE SKRZ P RUBU MOTORU Z P RUBY VRTULE MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 8 INSTALLATION AND OPERATION MANUAL CAUTION INSTALL THE PROPELLER ON ENGINE SLOWLY AND CAREFULLY TO AVOID DAMAGE OF PROPELLER AND ENGINE FLANGE OR DAMAGE OF THE O RINGS LEADING TO OIL LEAKAGE NOTE Two guide pins installed in two opposite mounting holes in propeller mounting flange may be used to support the propeller in proper position against the engine flange and make installation easier Refer to Special Tool chapter in this manual V508H propeller only Manually pull the beta ring toward the propeller mounting flange 9 Make sure the propeller seated correctly on engine flange and complete contact is established between the propeller flange and the engine flange 10 Attach the propeller to the engine flange with eight mounting bolts with washers NOTE The mounting bolts and washers may be reused when reinstalling the propeller between overhaul interval provided that they are not damaged or corroded a Place the washers on the screws CAUTION THE INSIDE CHAMFER OF THE WASHER MUST BE FA
140. N MKA Po prvn m b hu nov nebo opraven vrtule se na listech a vnit n m povrchu p edn ho krytu mohou objevit stopy oleje Je to norm ln a neznamen to e nik oleje se bude vyskytovat i nad le Pou ijte slab rozpou t dlo pro odstran n v ech stop oleje na listech a vnit n m povrchu p edn ho krytu b P ed dynamick m vyva ov n m poznamenejte po et a um st n vyva ovac ch z va ze statick ho vyv en c Pro vyva ov n se p ipou t pou it roub AN3 se samojistn mi maticemi d Poloha v ech otvor vyva ovac ch podlo ek mus b t pe liv zv ena Nesm doj t k jak mukoliv p ek en si s p ilehl m drakem letounu komponenty odmrazov n a motoru 3 Um st n vyva ovac ch podlo ek p i dynamick m vyva ov n a P i dynamick m vyva ov n se up ednost uje metoda p id v n z va na zadn kryt P padn pozd j sejmut t chto z va jsou li pou ita navr t vrtuli do stavu p vodn ho statick ho vyv en Sejmut z va statick ho vyv en se p ipou t pouze vyj me n b Pro dynamick vyva ov n pou vejte pouze nerezov nebo povrchov chr n n E 1500 INSTALLATION AND OPERATION MANUAL 1 Overview Dynamic balance is accomplished by using an accurate means of measuring the amount and location of the dynamic imbalance After such a undertake the remaining imbalance should be below 0 2 ips
141. NG check only when this function is involved 1 a Verify AUTOMATIC FEATHERING function according to aircraft flight manual 2 MANUAL FEATHERING check a Verify MANUAL FEATHERING according to aircraft flight manual b Verify time between switching on and off for FEATHERING PUMP lamp the time must be 12 15 s 3 EMERGENCY FEATHERING check a Switch off FEATHERING breaker b Setengine control lever to idle c Move propeller control lever from maximum RPM position to feather position Page 11 50 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER ID IQ Po zapraporov n vrtule jsou ot ky cca 350 ot min Ovl dac p ku vrtule p estavte zp t do polohy max ot ek Ot ky p ed a po praporov n mus b t shodn Kontrola funkce KONTROLN PRAPOROV N 10 IQ IO 17 10 g h Ovl dac p ku motoru nastavte do polohy max trval ho v konu Ovl dac p kou vrtule nastavte ot ky vrtule na 1900 ot min Zapn te jisti e PRAPOROVANI Stiskn te tla tko TEST PRAPOR Kontrolujte rozsv cen signalizace PRAPOR ERPADLO Ihned po rozsv cen signalizace PRAPOR ERPADLO tla tko uvoln te signalizace zhasne Ot ky vrtule vokam iku rozsv cen mus z stat konstantn V odli n m pr pad vyhledejte z vadu podle kapitoly 5 Ovl dac p ku vrtule p estavte do polohy max ot ek vrtule Ovl dac p ku motoru nastavte na doraz volnob hu j Kontrola pr
142. OPERATION AND INSTALLATION MANUAL REVERZOVATELN REVERSIBLE HYDRAULICKY OVL DAN HYDRAULICALLY CONTROLLED STAVITELN VRTULE VARIABLE PITCH PROPELLERS ST LYCH OT CEK CONSTANT SPEED V508 Type Series V510 Type Series Document number E 1500 ATA 61 10 00 2 Vyd n 13 dubna 2010 Technicky obsah tohoto dokumentu je schv len na Revize 7 ervence 2015 z klad opr vn n DOA EASA 21J 072 Issue 2 April 13 2010 The technical content of this document is approved Revision July 07 2015 under authority of DOA No EASA 21J 072 Avia Propeller s r o Beranov ch 65 666 199 00 Praha 9 Let any CZECH REPUBLIC Tel 420 296336511 Fax 420 296336519 sales Aaviapropeller cz www aviapropeller com AVIA PROPELLER UPOZORN N PRO MAJITELE U IVATELE A OBSLUHUJ C PERSON L Tato instala n a provozn p ru ka obsahuje popis technick informace a instrukce pro provoz a dr bu vrtul typov ady V508 a V510 Ve ker innosti souvisej c s provozem a dr bou vrtul mus b t prov d ny v souladu s touto p ru kou innosti p esahuj c sv m rozsahem r mec tohoto manu lu mohou b t prov d ny pouze v robcem nebo autorizovan m servisn m st ediskem VAROV N Ve ker innosti obsa en v tomto manu lu mohou prov d t pouze osoby s odpov daj c kvalifikac Nedodr en provozn ch instrukc a postup v tomto manu lu p ekro en stanoven ch
143. ORNY Xd ene dann S PH ES eN E valve lockin y C C P DR Feathering n pL stop 16 Maximum RPM stop Spring Microswitch V Connector Safety stop Figure 11 3 Governor LUN7815 02 View to engine Page 11 9 2010 04 13 PROPELLER CONTROL SYSTEM AVIA PROPELLER P ka s kulisou Sv Kulisa Sv DD ep T sn n M gre H U H del T hlo Sv 65 regul toru Torzn Op rny krouzek ty ka Nosi kluzn ch ESSE kamen o A RE T v ISS P ka Zv Obr zek 11 4 Regul tor LUN7815 02 Pohled sm rem od motoru 7 Uvoln n t hlo Sv 65 vhodn zajist te proti pohybu POZN MKA T hlo do kulisy zapojte a po z kladn m se zen regul toru viz kapitola 11 6 8 S p kou Rn na dorazu max ot ek p ekontrolujte chod p ky Bc ze z kladn polohy do reverzu kdy ryska na p ce s va kou je proti toleran n mu poli reverzu na stupnici regul toru Pot p estavte p ku Bc d le a na bezpe nostn doraz UPOZORN N CHOD P KY Bc NESM B T TUH P KA KLADE ODPOR POUZE P I P ECHODU PRVKU B7 BLOKOVAC HO MECHANISMU NA VRCHOLOVOU KRU NICI VA KY Strana 11 10 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Lever Bc Lever Sv with gate Gate Sv Pin Packing Governor Lever Sv 65 shaft BETA ring Carbon block Sto
144. Odd l Demont vrtule z motoru byl aktualizov n Strana 6 1 6 2 Odkaz na opravu listu nov na kapitolu Udr ba Strana 6 4 6 7 K hodnot m uveden m v milimetrech p id n p epo et na palce Strana 6 9 6 10 Desetinn rka u rozm ru v palc ch zm n na na te ku Strany 6 10 a 6 16 Odd l Oprava vrtulov ch list byl p esunut do kapitoly 7 Ostatn odd ly posunuty nahoru Strany 7 4 a 7 9 Postup opravy listu p esunut z kapitoly 6 a aktualizov n Strana 8 1 a 8 8 Kapitola Odstra ov n z vad byla aktualizov na Strana 9 1 Kapitola Doprava a skladov n byla aktualizov na Strany 10 1 10 2 Do kapitoly dopln n seznam n ad p vodn uveden v Servisn m dopisu SL 5 Strana 11 1 Nov pr zdn strana obsah kapitoly 11 byl p esunut do hlavn ho obsahu Strana 11 2 Odd l Obecn byl aktualizov n V cel kapitole 11 dopln ny k milimetr m a stup m celsia p epo ty na palce a stupn fahrenheita Page 5 4 Mentioned or similar in anti seize compounds changed to or equivalent Page 5 13 Information on installations with governor other than Jihostroj was updated Page 5 14 Section Propeller removal from engine was updated Page 6 1 6 2 Blade repair procedures newly referred to chapter Maintenance Page 6 4 6 7 Inch equivalents added to millimeter units Page 6 9 6 10 Decimal c
145. PELLER IS PACKED IN A SPECIAL FOIL IMPREGNATED WITH CORROSION INHIBITORS DO NOT REMOVE THE FOIL WITH NO INTENTION TO INSTALL THE PROPELLER ON ENGINE It is expected that the propeller will be put in service within 24 months since new or overhaul CAUTION IF THE PROPELLER IS NOT PUT IN SERVICE WITHIN 24 MONTHS FROM NEW OR OVERHAUL THEN THE CALENDAR TBO LIMIT MAY BE DECREASED REFER TO AVIA SERVICE BULLETIN NO 1 FOR COMPLETE INFORMATION ON TBO LIMITS CAUTION INSTALLING THE PROPELLER ON ENGINE LATER THAN 24 MONTHS FROM NEW OR OVERHAUL OR RETURNING THE PROPELLER TO SERVICE AFTER MORE THAN 24 MONTHS OF STORAGE WITHOUT THE INSPECTION AT AVIA PROPELLER OR AUTHORIZED SERVICE CENTER MAY LEAD TO OIL LEAKAGE AND OR INCORRECT FUNCTION REFER TO AVIA SERVICE BULLETIN NO 1 FOR MORE INFORMATION Page 9 1 SHIPPING AND STORAGE 2015 05 12 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 10 SPECI LN N RAD 10 SPECIAL TOOL Tabulka 10 1 obsahuje kompletn seznam n ad pot ebn ho pro mont vrtule na motor demont z motoru a p edepsanou dr bu M e obsahovat tak doporu en Refer to table 10 1 for complete list of necessary tool for installation of propeller on engine removal from engine and specified maintenance Also recommended tool n ad N zev Popis Vyobrazen Momentov kl Kl pro uta en mont n ch roub mimo verze V508H nebo mont n ch matic pouze verz
146. RAMEN PO DODATECN M DOTA EN KV LI POJI T N Z VLA KOU NEM VLIV NA PROVOZUSCHOPNOST VRTULE UPOZORN N 2 VV PRO UMOZN N POJIST N Z VLACKOU MATICI VZDY DOTAHUJTE NIKDY NEPOVOLUJTE PO UTAZEN NA PREDEPSANY MOMENT NESM DOJ T K DOTYKU KONC RAMEN OBJ MKY Obr zek 5 7 E 1500 MONT N A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION MANUAL CAUTION 1 IF THE SHOULDERS TOUCH EACH OTHER AFTER TORQUING REMOVE THE PROPELLER FROM SERVICE AND CONTACT THE AVIA PROPELLER TOUCHING OF THE SHOULDERS AFTER ADDITIONAL TIGHTENING OF THE CLAMP BOLT FOR SAFETY WITH COTTER PIN DOES NOT AFFECT SERVICEABILITY OF THE PROPELLER CAUTION 2 NEVER LOOSEN THE NUT TO UNCOVER THE HOLE FOR COTTER PIN ONLY TIGHTEN THE SHOULDERS OF THE CLAMP MUST NOT TOUCH EACH OTHER AFTER TIGHTENING TO SPECIFIED TORQUE Figure 5 7 Page 5 6 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL D INSTALACE VRTULE NA MOTOR D INSTALLING THE PROPELLER ON THE ENGINE Strana 5 7 20 10 2014 UPOZORN N mE VRTULE V508H S N 070031 VY ADUJE SPECI LN POSTUP P I INSTALACI NA MOTOR TENTO POSTUP JE UVEDEN A KONCI T TO KAPITOLY 1 Pouze vrtule V508H Pro umo n n instalace mont n ch roub je nutn zasunout beta krou ek k mont n p rub vrtule Sledujte obr zek 5 8 a Odstra te poji ovac dr t ze
147. ROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER d Zapojte t hlo ovl d n p ky Bc od motoru tak aby se nezm nila poloha p ky doraz a kontrolujte nastaven palivov ho regul toru kter m odpov dat provozn p ru ce motoru P estavte s pomocn kem v m st odpojen drakov ho ovl d n p ku na motoru do pln ho reverzu a kontrolujte 1 regul toru ot ek mus b t ryska na p ce proti rysce max reverzu na stupnici regul toru obr zek 11 26B IN Doraz na regul toru paliva mus b t na hlavn ovl dac p ce kontrolujte listovou m rkou 0 05 mm 0 002 inch na stisk Sou asn ode t te nastaven kter m odpov dat provozn p ru ce motoru Pokud se rysky p ky a stupnice v reverzn poloze nekryj se i te kinematiku motoru podle provozn p ru ky motoru POZN MKA Kone n se zen kontrolujte v cen sobn m p estaven m z polohy volnob h do polohy max reverz a znovu kontrolujte koncov dorazy Strana 11 41 6 2 2012 Ryska minim ln ho Ryska reverzu letov ho hlu Obr zek 11 26 Se zen max reverzn ho v konu rysky Po ukon en se zen zapojte op t drakov ovl d n na motor Pomal m p estaven m p ky ovl d n motoru z polohy volnob h do polohy max reverzn v kon a zp t kontrolujte dorazov polohy na regul toru paliva a regul toru ot ek vrtule Nen li mo no dos hnout max reverzn polohy na regul t
148. ROPELLER O RING PROPELLER O RING E ENGINE O RINGS SINGLE ACTING APPLICA TION DUAL ACTING APPLICATION Figure 5 9 7 Align dowel pin holes in the propeller flange with the dowel pins in the engine flange and carefully slide the propeller onto the engine flange Page 5 8 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER 8 UPOZORN N P I INSTALACI VRTULE NA MOTOR POSTUPUJTE POMALU A OPATRN ABY NEDO LO K PO KOZEN P RUBY VRTULE A MOTORU NEBO K PO KOZEN O KROU K VEDOUC K NIK M OLEJE POZN MKA Pro snadn j instalaci vrtule na motor mohou b t pou ity dva vod c epy instalovan v protilehl ch mont n ch otvorech v p rub vrtule kter podep raj vrtuli a udr uj j ve spr vn poloze v i p rub motoru viz kapitola Speci ln n ad v t to p ru ce Pouze vrtule V508H Ru n zasu te beta krou ek nadoraz sm rem k p rub vrtule 9 Ov te e vrtule je spr vn a pln p isazena k p rub motoru a p ruba vrtule kompletn dosed na p rubu motoru 10 P ipevn te vrtuli k p rub motoru osmi mont n mi rouby a podlo kami Strana 5 9 20 10 2014 POZN MKA Mont n rouby a podlo ky 12 pou vat opakovan b hem doby mezi gener ln mi opravami za p edpokladu e nejsou po kozeny nebo zkorodov ny a Na mont n rouby navle te podlo ky UPOZORN N SRA E
149. Strana 8 7 6 2 2012 ODSTRANOV N Z VAD E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL C DE ICING Trouble Radio communication is interfered at de icing switched on Probably cause a Damaged or excessive worn brushes b Dirty copper slip rings c Damaged or excessive worn copper slip rings d Bad contact in electrical circuit Remegy a Check the brushes per chapter Inspections Replace the brush block per chapter Installation and operation instructions as necessary b Clean the copper slip rings c Replacement of the slip ring by manufacturer or authorized repair center d Verify relevant contacts and tighten if necessary Trouble De icing is out of function Probably cause a Failed de icer b Failure in electrical circuit Remegy a Send the blade s with failed de icer to manufacturer or authorized service center for repair b Follow instruction of aircraft manufacturer D PROPELLER HUB BLADES Trouble Servomechanism leakage Probably cause a Defective cylinder sealing Remegy a Sendthe propeller to manufacturer or authorized repair centre Page 8 7 TROUBLESHOOTING 2012 02 06 AVIA PROPELLER Z vada Net snost v ulo en listu Mo n p ina a Po kozen t sn n v ulo en listu N prava a Vrtuli za lete k v robci nebo do autorizovan ho servisn ho st ediska Z vada Net snost v prostoru p ruby vrtule Mo n p ina
150. TE BL E KE KORENI NIKDY ZA PI KY c P esv d te se zda pri zp tn m pohybu do z kladn polohy po p eru en elektrick ho obvodu je vrchol kluzn ho epu vzd len od patn plochy va ky 27 minim ln 0 1 mm 0 004 inch Je li tato v le men se i te ji areta n m roubem obr zek 11 20 o jeho hlavu se p ka op r Areta n roub pak pojist te dota en m matice d Bod zapnut elektrick ho obvodu v z vislosti na vysunut op rn ho krou ku vrtule se i te n sleduj c m zp sobem 1 Ru n m p estaven m vrtulov ch list vysu te beta krou ek vrtule ovl dac p ku vrtule v kabin letounu p itom nastavte do polohy prapor Beta krou ek nastavte na vysunut na 9 5 94 mm 0 37 0 374 inch a v t to poloze vhodn zajist te 2 Okam ik zapnut elektrick ho okruhu se i te pouze nat en m va ky 27 po povolen zaji ovac ho roubku obr zek 11 20 UPOZORN N ZAJISTOVAC M SROUBKEM JSOU DV PODLOZKY Z NICHZ JEDNA JE P ROV UPOZORN N gt LISTY PRI PRET EN UCHOPTE BL E KE KORENI NIKDY ZA PI KY 3 Po se zen pojist te op t va ku 27 dota en m zaji ovac ho roubku POZN MKA Okam ik zapnut el obvodu mikrosp na em je t mo no zkou et p ipojen m vhodn ho slaboproud ho zdroje max 12 V se rovkou na kol ky 3 4 z str ky obr zek 11 20 e V echny r
151. TION AND OPERATION MANUAL L INSTRUCTION FOR INSTALLING THE PROPELLER V508H S N 070031 NOTE Install the propeller onto the engine as described below in this chapter respecting the information and procedures in this section 1 The special puller is reguired for propeller V508H S N 070031 to pull the beta ring toward the propeller mounting flange to allow installation of the mounting bolts Do not remove the cover caps unless stated otherwise see below a Fit the puller P N 900 0175 together Figure 5 18 b O 61 10 00 Lubricate an internal thread of the puller rod with sufficient amount of anti seize compound Loctite Moly 50 Loctite 8023 or eguivalent CAUTION USING THE PULLER WITH NOT LUBRICATED THREAD CAUSE SEIZING INSIDE THE PROPELLER REQUIRING THE REPAIR IN SERVICE CENTER Install the puller onto the propeller and connect to the piston rod inside the propeller through the opening in the cover Figure 5 19 Compress the beta system to pull the beta ring toward the propeller mounting flange POZN MKA Only if the beta ring is not pulled enough to allow installation remove the cover caps as described in this chapter and pull the beta ring by hand The propeller is attached to the engine flange with the nuts Torque the nuts in two steps as follows 1 Torque all nuts in sequence A in figure 5 11 to 40 50 Nm 30 40 Ib ft 2 Torque all nuts in sequence B in figure 5 11 to 95 110 Nm 70
152. TION INFORMATION The variable pitch propeller consists of the following main groups Propeller hub with blade bearings Pitch change mechanism Propeller blades Counterweights Propeller spinner De icing optional Propeller governor Oil NOTE See figures in this section for design of specific propeller type Propeller hub with blade bearings The one piece hub is made from steel with the outer surface cadmium plated Blade bearing of propeller V508 is turned by two race ball bearings Outer bearing races are part of the hub whereas the inner bearing races are located on the blade bushing Preload of the bearing is adjusted by thickness of the distance ring mounted under the clamp Blade bearing of propeller V510 is turned with two ball bearing races and one roller bearing race Outer bearing races are located on the outer ring pressed into the hub the inner ball races are parts of the blade bushing The bearing preload is adjusted by specific torque moment of the bearing ring All of propeller models except basic models V508 7 V508B and V508H are equipped with overspeed governor on the cylinder front face If the real propeller rpm increase the setting value the overspeed governor withdraws the oil from low pitch area in the hub into the drain till the rpm decrease to correspond with setting The pitch change mechanism All models except model V508H Dual acting servomechanism consists of piston hydraulic cy
153. TION MANUAL The repair should be maximum of 1 5 mm 0 06 inch deep but not more than 20 percent of total thickness of the blade in the place of repair Total area of all repairs must not exceed 40cm 6 2 square inch Distance between the repairs in the blade width must be min 40 mm 1 57 inch and its total width must not exceed one half of the blade width in the place of repair Diameter of repaired area must be 30 times greater than its depth b V510 propeller blade Nicks and scratches not deeper than 0 12 mm 0 005 inch located in area of 590 mm 23 2 inch airfoil beginning are acceptable and not required to be repaired Refer to figure 7 2 Nicks and scratches not deeper than 0 35 mm 0 014 inch are acceptable in area from 590 mm 23 2 inch to the tip and not required to be repaired Refer to figure 7 2 NICKS AND SCRATCHES NOT DEEPER NICKS SCRATCHES NOT DEEPER THAN 0 12 mm inch AR AN mm 0 014 inch ARE ACCEPTABLE IN THIS AREA AND NO ACCEPTABLE IN THIS AREA AND NOT 0 REPAIRED TO BE REPAIRED 23 2 inch Figure 7 2 Allowable damage on camber and face side of the V510 blade The repair should be maximum of 0 8 mm 0 032 inch deep but not more than 10 percent of total thickness of the blade in the place of repair Total area of all repairs must not exceed 30cm 4 65 square inch Distance between the repairs in the blade width must be min 40 mm 1 57 inch and its total width must n
154. UN7816 kapitola Syst m ovl d n vrtule v t to p ru ce Instalace s regul tory jin ch v robc p ru ka v robce motoru nebo regul toru b Nastavte pozemn volnob n v kon motoru dle instrukc v robce motoru Strana 8 1 6 2 2012 ODSTRANOV N Z VAD E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 8 TROUBLESHOOTING A NORMAL OPERATION Trouble Static propeller rpm at idle are higher Probably cause a Clearance between beta ring and carbon block is higher than 0 4 mm 0 016 inch b After return from beta mode of operation the beta lever on the governor did not returned to its basic position c Minimum flight pitch is set to a lower value d Engine has higher power at idle Remegy a Replace the carbon block assembly on the feedback lever per chapter Installation and Operation Instructions of this manual b Verify and adjust engine control per instruction of engine manufacturer c Adjust minimum flight angle Model V508H chapter Installation and Operation Instructions of this manual Installation with governor Jihostroj LUN7815 or LUN7816 chapter Propeller Control System of this manual Installation with other governors instruction of engine of governor manufacturer d Reduce engine idle per instruction of engine manufacturer Trouble Static propeller rpm at idle are lower Probably cause a Minimum flight pitch is set to a higher value
155. Uder blesku v t to kapitole POZN MKA Zn mkou deru blesku m e b t odli n zbarven m sto na povrchu d lu stopy op len nebo rozte en kovu rozt epen nebo chyb j c materi l v m st deru blesku 3 Zkontrolujte viditeln d ly vrtule na zn mky niku oleje z vrtule Postupujte dle odd lu Unik oleje nebo maziva v t to kapitole pro zji t n zdroje niku oleje Strana 6 2 6 2 2012 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL NOTE The blade play of models V508 is normal due to different design of the retention bearing 5 Check hardware for loose or missing 6 Inspect the de icers if installed for damage and unsticking Contact Avia Propeller if problem is noted 7 After engine start up check the propeller speed control and operation according to the procedure specified in the Pilot Operating Handbook POH for the aircraft 8 Check for any abnormal vibration If vibration occurs shut the engine down identify the source of vibration and correct it before further flight Refer to Vibration in this chapter and Troubleshooting in this manual WARNING ABNORMAL VIBRATION CAN INDICATE THE DAMAGE OF PROPELLER BLADE OR BLADE BEARING COMPONENT IT MAY LEAD TO IN FLIGHT BLADE SEPARATION AND CATASTROPHIC AIRCRAFT ACCIDENT B 300 HOUR ANNUAL INSPECTION NOTE Detailed inspection must be performed at 300 hour intervals of operation not to exceed 12 calendar months Fo
156. XAGON HEAD OF THE BOLT STOP MUST NOT BE RELEASED AND RE ADJUSTED IT IS ADJUSTED BY GOVERNOR MANUFACTURER NOTE Parts 15 18 29 B2 B7 58 and 65 are adjustable b With Bc lever figure 11 9 in basic position guideline on the lever with cam aligns with minimum flight pitch guideline on the governor scale and the control lever pin touches the stop verify Rn lever travel between stops and tel 6 With lever Rn at maximum RPM stop 15 verify lever Bc travel from basic position up to reverse when the guideline on the lever with cam is against reverse range on the governor scale Then move the lever Bc further to safety stop CAUTION Lever Be travel should be free Page 11 15 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Ryska min T hlo 29 pozem hlu P ka Bc d Ryska minim ln ho g AQ letov ho hlu AS Doraz max ot cek 15 Tazn pruzina Mikrosp na V Ta n pru ina Z str ka e J Doraz 58 Bezpe nostn doraz Obr zek 11 9 Regul tor LUN7815 03 Pohled sm rem k motoru 7 Kontrolujte nosi kluznych kamen obr zek 11 6 na po kozen a kompletnost 8 epy nosi e kluznych kamen nama te vazel nou UPOZORN N VADN NOSI KLUZN CH KAMEN VY A TE Z PROVOZU 9 Pohybem p ky Zv ve sm ru ipky obr zek 11 10 se p esv d te poslechem o sepnut mikrosp na e V obr
157. Z znamn ku vrtule s uveden m e do lo ke zm n polohy pozi n rysky Strana 7 11 7 7 2015 DR BA E 1500 61 10 00 Ino 4 If INSTALLATION AND OPERATION MANUAL Rotate the propeller to place another blade to the same position as the previous blade was measured Measure and note the angle Measure the angle of all blades by the same way the difference in angle of all blades is between 0 3 degrees the installation is correct When the difference in angle of all blades is above 0 3 degrees follow these steps 1 2 IB I 101 IN Remove the blade from the hub Using the sandpaper or needle file carefully remove the position mark from the edge of the blade bushing Do not remove more material than is necessary to remove the mark Thoroughly clean inside of the blade bushing Reinstall the blade into the hub Using the protractor set the blade so that the difference in angle of all blades is between 0 3 degrees Tighten the blade clamp with a specified torgue and check that the blade angle is still correct Using a sharp tip needle and a suitable flat block engrave the position mark on the blade bushing edge opposite to the position mark on the blade Treat the blade bushing edge with zinc coat or with clear lacquer Make an entry in the propeller logbook to document that an original position mark was changed Page 7 11 MAINTENANCE AVIA PROPELLER 8 ODSTRANOV N
158. a chodu motoru problik v nebo trvale sv t Mo n p ina a Ucpan proh vac tryska praporovac ho erpadla b Vadn tlakov sp na c Net sn zp tn ventil v regul toru vrtule N prava a Vym te praporovac erpadlo dle instrukc v robce letounu b Vym te tlakov sp na dle instrukc v robce letounu c Postupujte dle instrukc v robce motoru Strana 8 6 6 2 2012 ODSTRANOV N Z VAD E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Trouble Feathering too long longer than 8 seconds or not finished Probably cause a Feathering pump produces lower pressure b Failure in electrical circuit e g relay timer etc C Leakage in oil transfer system Remegy a Verify feathering pump voltage for feathering pump Follow instruction of aircraft manufacturer b Follow instruction of aircraft manufacturer c Follow instruction of aircraft manufacturer Trouble Manual feathering does not work Probably cause a Propeller condition lever is not at feathering stop Remegy a Adjust propeller speed control lever linkage so that it reaches the feathering stop Follow instructions of engine manufacturer Trouble Feathering lamp flashing or lightening at engine run Probably cause a Clogged heating orifice of the feathering pump b Defective pressure sensor c Leakage at check valve in the governor Remegy a Replace the feathering pump per ins
159. ance and angular location to the slip ring as shown in Figure 5 14 1 Page 5 11 INSTALLATION AND OPERATION INSTRUCTION 2014 09 18 AVIA PROPELLER c Ut hn te rouby p ipev uj c sb ra k mont n konzole utahovac m momentem 1 2 Nm 9 18 in Ib Po uta en ov te spr vnou vzd lenost a hel UPOZORN N NADM RN UTA EN ROUB M E ZP SOBIT DRHNUT NEBO ZABLOKOV N UHL K A NESPR VNOU FUNKCI ODMRAZOVAC HO SYSTEMU 4 Zkontrolujte radi ln zarovn n uhl k Ov te e ela uhl k dosedaj cel m povrchem na sb rac krou ky v cel m rozsahu 360 oto en p enosov ho kruhu jak je vyobrazeno na obr zku 5 14 2 b Zru eno POZN MKA Ostatn typy sb ra instalujte dle p ru ky letounu SM R ROTACE PRENOSOV CH KRUH PRENOSOV KRUHY _ 1 2 2 4 mm 0 047 0 095 inch P 7 p SB RAC Strana 5 11 1 7 7 2015 Obr zek 5 14 1 MONT ZN A PROVOZN INSTRUKCE E 1500 INSTALLATION AND OPERATION MANUAL c Torque the screws attaching the brush blocks to the mounting bracket to 1 2 Nm 9 18 in Ib Check correct distance and angle after tightening CAUTION OVERTIGHTENING THE SCREWS CAN CAUSE BIND OR HANG UP OF THE BRUSHES IN THEIR BLOCKS AND INCORRECT FUNCTION OF DE ICING SYSTEM 4 Check radial alignment of the brushes Make sure that the brushes are aligned so that the entir
160. aporov n vrtulov ho syst mu Z stavba bez praporovac ho erpadla 1 Strana 11 51 13 4 2010 Kontrola funkce NOUZOV PRAPOROV N IQ IO O 190 ma Ovl dac p ka motoru nastavena na doraz volnob hu Ovl dac p ku vrtule p esu te z polohy max ot ek do praporov polohy Po zapraporov n vrtule jsou ot ky cca 350 ot min Ovl dac p ku vrtule p esu te zp t do polohy max ot ek Ot ky p ed a po praporov n mus b t shodn prove te kontrolu t snosti spoj vrtule provedenou zkou ku zapi te do Z znamn ku vrtule SYST M OVL D N VRTULE E 1500 d e INSTALLATION AND OPERATION MANUAL Propeller speed is about 350 rpm in feather position Move propeller control lever back to maximum RPM position Propeller speed before and after should be the same 4 CONTROL FEATHERING function check 02 D 10 Place engine control lever to maximum continuous power position Set with propeller control lever propeller speed to 1900 rpm Switch on the FEATHERING breaker Press TEST FEATHERING button Observe FEATHERING PUMP switching on Immediately after energizing the FEATHERING PUMP lamp release the button lamp will extinguish Propeller speed must stand constant when the lamp is energized Move propeller control lever to maximum propeller RPM position Place engine control lever to idle stop j Check of feathering installa
161. at the reference station The reference station is marked with red line on the blade face side 1 Rotate the propeller to place one of the blades parallel to the ground Measure the angle of the blade Make note this angle Page 7 10 MAINTENANCE 2015 07 07 AVIA PROPELLER Ino Oto te vrtuli a nastavte dal list do stejn polohy v jak byl m en p edchoz list Zm te hel listu a poznamenejte si ho 3 Stejn m zp sobem zm te v echny listy c Pokud vz jemn hlov rozd l mezi v emi listy nen v t ne 0 3 instalace je v po dku d Pokud je vz jemn hlov rozd l mezi v emi listy v t ne 0 3 postupujte n sledovn 1 Vyjm te list z vrtulov hlavy 2 Smirkov m pap rem nebo jehlov m piln kem opatrn odstra te z hrany pouzdra listu pozi n rysku Neodeb rejte v ce materi lu ne je nezbytn pro odstran n rysky 3 D kladn vy ist te vnit ek pouzdra listu 4 Nainstalujte list zp t do vrtulov hlavy Pomoc hlom ru nastavte list tak aby hlov rozd l mezi v emi listy nebyl v t ne 0 3 Ut hn te obj mku listu p edepsan m utahovac m momentem a ov te e hel listu st le odpov d po adovan hodnot 5 Pomoc ostr jehly a vhodn ho rovn ho hranolu vyryjte na hranu pouzdra listu pozi n rysku proti pozi n rysce na listu 6 O et ete hranu pouzdra listu zinkov m n t rem nebo bezbarv m lakem 7 Prove te z znam do
162. ation and operation instruction in this manual if problem is noted Check correct installation of the clamps with counterweights Refer to Installation and operation instruction in this manual e Check the blade play per Loose blades in this chapter f Check the blade track per Blade track in this chapter Loose blades a Check the blade for looseness per figure 6 3 Blade play limits Blade end play Fore and aft play Radial play pitch change 4 mm 0 16 inch V508 type series only 4 mm 0 16 inch V508 type series only 1 measured at reference station difference between all blades must not be more than 0 5 In and out play 0 8 mm 0 032 inch V508 type series only Page 6 7 INSPECTIONS 2012 02 06 AVIA PROPELLER UPOZORN N U vrtule V510 se dn v le krom hlov v le nep ipou t P EDOZADN V LE lt PI KY LISTU r AXI LN V LE PI KY LISTU V ROVINE ROTACE RADI LN V LE Obr zek 6 3 V le list b Listy s v l v t ne jsou p pustn limity nebo listy kter se po uvoln n nevr t do p vodn polohy m ou b t zn mkou po kozen nebo z vady uvnit vrtule V takov ch p padech kontaktujte Avia Propeller 4 Dr ha listu POZN MKA Tato kontrola se prov d pouze v p pad podez en e by probl m v dr ze list mohl b t p inou nestandardn ho chov n vrtule nap vibrace POZN MKA Zastavit moto
163. aven na 5 8 Strana 5 16 Anglick text v tabulce 5 1 v lev m sloupci zm n n na esk Strana 7 5 V prav m sloupci opraveno slo obr zku 7 1 na 7 2 Strana 7 7 V prav m sloupci byl v odd lu 2 a odkaz na obr zek 7 2 opraven na 7 4 P id na informace o minim ln teplot oleje pro innost vrtule Strana 2 1 Informace o TBO p esunuta na za tek odd lu Gener ln oprava Strana 3 2 Aktualizov no zna en vrtul ady V510AG Strany 4 4 4 6 4 8 4 10 Aktualizov ny obr zky sestav vrtul Strana 5 1 P id na pozn mka o sestav krytu se roubovanou p edn v ztuhou P id na pozn mka nepou vat o krou ek z p epravn z tky Strana 5 2 Aktualizov no upozorn n na pou it vod c ch ep Strany 5 8 5 9 P id na kontrola obj mky listu po uta en na moment Strany 5 11 a 5 12 Aktualizov n postup mont e a nastaven el sb ra e Strana 6 10 Aktualizov n postup kontroly opot eben kart sb ra e LUN7850 7 Strany 7 6 7 9 7 10 Aktualizov n postup ochrany m stn opravy listu Strana 10 3 P id no speci ln n ad pro vrtule V508H R 31 12 February 28 2012 R 221 13 December 05 2013 R 8 14 January 17 2014 61 10 00 11 4 1 1 5 5 5 6 5 16 7 5 7 7 11 4 11 1 4 3 1 4 11 1 2 1 3 2 4 4 4 6 4 8 4 10 5 1 5 2 5 8 5 9 5 11 5 11 1 5 12 6 10 7 6 7 9 7 10 10 3 LIST OF REVISIONS Page 5 5 Czec
164. axim ln ch ot ek f P esu te pomalu p ku ovl d n motoru na ot ky gener toru odpov daj c po tku z sahu omezova e ot ek ot ky vrtule p estanou stoupat cca 1950 ot min N sledn zvy te ot ky gener toru o p ibli n 2 Tento kon opakujte p tkr t P ka ovl d n vrtule je v poloze maxim ln ch ot ek Strana 6 4 6 2 2012 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL b Corrosion marks in the blade bushing thread not exceed 1 5 of circumference for first and second thread from outside and 1 4 of circumference for other threads and bushing bottom Use special hand glass for inspection of threads backside NOTE Wipe the corrosion marks in the bushing thread with a clean cloth or slightly polish with fine emery cloth or ScotchBrite CAUTION In case of strong and or deep corrosion if it is not possible to remove the blade from the bushing or in case of any doubt remove the propeller from service and contact Avia Propeller 5 Install the blades per Blade installation in this manual 6 Perform function test of the overspeed governor as follows NOTE It is not applied to propeller models V508Z and V508H a Use a special wrench to remove the governor cover figure 6 1 NOTE Special wrench is no need for new designed overspeed governor P N 300 095 CAUTION The spring support must extend from governor body approx 1 5 mm 0 06 inch as displayed in figure
165. ccording to procedure in this section Maximum propeller RPM check 1 Propeller control lever in maximum RPM position 2 Move engine control lever to maximum take off power position 3 Maximum ground propeller speed should be 2080 120 rpm NOTE Specified value for RPM is only for information It depends on engine performance and atmospheric conditions Feathering pump heating leg pressure check only when the feathering pump is installed 1 Move engine control lever to maximum continuous power position 2 Feathering Pump is not lit Propeller control lever function check 1 Engine control lever at maximum continuous power position 2 Set with engine control lever propeller RPM to 1900 rpm then reduce propeller RPM to 1700 rpm using propeller control lever and back to previous position 3 Propeller speed must be adequate to position of propeller control lever WARNING TORQUE MUST NOT EXCEED 100 Speed in reverse mode reverse power check secondary pitch lock check 1 Set propeller control lever to maximum RPM position 2 Place engine control lever to idle 3 Move engine control lever over the stop move slowly and smoothly into maximum reverse position and observe operational values PROPELLER CONTROL SYSTEM rage Did 2010 04 13 AVIA PROPELLER lo 7 1500 Ot ky vrtule p i p esunu ovl dac p ky motoru se zvy uj a do ust len cca 1100 a 1200 ot min p esto e posun ovl dac
166. ch b Circuit failure Remegy a Follow instruction of engine manufacturer b Follow instruction of aircraft manufacturer Page 8 2 61 10 00 TROUBLESHOOTING AVIA PROPELLER Z vada Vrtule nedosahuje p i ust len m letu maxim ln ch ot ek Mo n p ina a P ka ot ek vrtule nen v poloze maxim ln ch ot ek b Spatn se zen regul tor ot ek vrtule c Nedostate n tlak oleje v hydraulick soustav vrtule N prava a Zkontrolujte kinematiku ovl d n p ku ustavte do polohy maxim ln ch ot ek Postupujte dle instrukc v robce motoru b Se i te regul tor ot ek dle instrukc v robce motoru c Zkontrolujte tlak oleje v regul toru vrtule pop pad tlak se i te Postupujte dle instrukc v robce motoru Z vada Ot ky vrtule p ekra uj maxim ln povolen ot ky Mo n p ina a Spatn se zen regul tor ot ek vrtule b Vadn regul tor ot ek vrtule N prava a Se i te regul tor ot ek vrtule dle instrukc v robce motoru b Vym te regul tor ot ek dle instrukc v robce motoru Z vada N hl pokles ot ek vrtule Mo n p ina a Praskl n hon regul toru b Ztr ta tlaku oleje v olejov soustav N prava a Postupujte dle instrukc v robce motoru b Postupujte dle instrukc v robce motoru Strana 8 3 6 2 2012 ODSTRANOV N Z VAD 61 10 00 TROUBLESHOOTING E 1500 INSTA
167. clamp Figure 5 4 lt CAUTION V508Z PROPELLER HAS THE CLAMP NOT LOCKED IN POSITION WITH THE PIN BEFORE TIGHTENING POSITION THE CLAMP SO THAT POSITION MARK ON THE CLAMP IS IN LINE WITH THE MARKS ON THE BLADE AND BLADE BUSHING FIGURE 5 5 BLADE CLAMP POSITION PIN V508Z PROPELLER ONLY Figure 5 4 Figure 5 5 Tighten the clamp Correctly position the bolt head Figure 5 6 and hold in place with the fingers of one hand while tightening the nut with other hand until snug Then still hold the bolt head use the torque wrench to torque the nut to 65 70 Nm 48 52 Ib ft Check correct position of the bolt head after torquing CAUTION INCORRECTLY TIGHTENED CLAMP BOLT WILL CAUSE AN UNDESIRABLE CHANGE OF BLADE ANGLE SETTING LEADING TO AERODYNAMIC IMBALANCE AND EXCESSIVE VIBRATIONS OF THE PROPELLER WHILE IN OPERATION Check correct position of the blade after torquing the clamp Make sure that the shoulders of the clamp do not touch each other after tightening the clamp bolt to specified torque Figure 5 7 and secure the nut with supplied cotter pin If the holes for cotter pin are covered after torquing tighten the nut additionally until nearest hole is open Page 5 5 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER Strana 5 6 20 10 2014 UPOZORN N 1 m V PR PAD DOTYKU RAMEN OBJ MKY PO UTAZEN NA PREDEPSANY MOMENT ST HN TE VRTULI Z PROVOZU A KONTAKTUJTE AVIA PROPELLER DOTYK
168. d Page Short Description R 137 14 18 z 2014 R 168 14 20 jna 2014 R 70 15 12 kv tna 2015 R 103 15 7 ervence 2015 Strana 11 5 7 7 2015 11 5 11 6 111 1 4 3 4 11 5 8 a 5 9 1 5 11 5 11 1 5 12 6 10 1 1 11 5 11 1 5 1 a 5 9 3 5 18 5 19 10 3 11 5 111 1 6 14 9 1 1 2 11 5 1 1 5 11 1 7 5 7 10 7 11 11 17 SEZNAM ZM N Strana 4 3 Dopln n chyb j c ch zm nov ch ar z minul ch zm n a zm na data str nky Strana 4 11 V tabulce 4 4 byla v angl verzi opravena polo ka 2 81 Strana 5 8 P id no upozorn n t kaj c se uta en obj mky listu Strany 5 11 6 10 P id n sb ra P N 066 5300 Strana 5 11 1 P id na kontrola sb ra e po instalaci Strana 5 12 P esunut obr zek 5 14 2 ze str 5 11 1 Strany 5 1 a 5 9 3 Aktualizov n postup mont e vrtule na motor Strany 5 18 5 19 Speci ln postup mont e vrtule S N 070031 na motor Strana 10 3 Aktualizov n seznam n ad P id ny postupy po tvrd m p ist n Aktualizov na Doprava a skladov n Aktualizov n postup mont e sb ra e P id n postup v m ny listu v provozu 7 5 11 17 Oprava textov ch chyb 61 10 00 R 137 14 September 18 2014 Il 5 II 6 111 1 4 3 4 11 5 8 to 5 9 1 5 11 5 11 1 5 12 6 10 R 168 14 October 20 2014 1 1 11 5 III 1 5 1 to 5 9 3 5 18 5 19 10 3 R 70 15 May 12 2015 11 5 111 1 6 14 9 1
169. d otherwise 5 Life limited parts of V508 series propellers Part Life limit Blade 15 000 hours 2 000 hours Hub 15 000 hours 2 000 hours Blade bushing 15 000 hours 2 000 hours Fork 15 000 hours 2 000 hours Cylinder 15 000 hours 2 000 hours 2000 hour life limit apply only to parts of V508E AG 106 A propeller assembly operated on Turbo Shark aircraft Sukhoi 26MX with Walter M601T engine Page 1 1 AIRWORTHINESS LIMITATIONS 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 6 D ly s omezenou ivotnost vrtul ady V510 6 Life limited parts of V510 series propellers D l ivotnost Part Life limit List 12 500 hodin 3 000 hodin Blade 12 500 hours 3 000 hours N boj 20 000 hodin 3 000 hodin Hub 20 000 hours 3 000 hours Pouzdro listu 20 000 hodin 3 000 hodin Blade bushing 20 000 hours 3 000 hours Vn j krou ek lo iska 20 000 hodin 000 hodin Outer bearing ring 20 000 hours 3 000 hours Un e 20 000 hodin 3 000 hodin Fork 20 000 hours 3 000 hours V lec 20 000 hodin 3 000 hodin Cylinder 20 000 hours 3 000 hours Limit ivotnosti 3000 hodin plat pouze pro d ly vrtule V510T 90A A 3000 hour life limit apply only to parts of V510T 90A A propeller assembly provozovan na letounu PZL 130 Orl k s motorem Walter M601T operated on PZL 130 Orlik aircraft with Walter M601T engine Strana 1 2 1 2 6 22012 OMEZEN
170. ding feathering Pressure oil for propeller working provide through the engine shaft and into the high and low pitch area in the hub is supplied by channels in the guide tube Some of the propeller models V508E V508E AG and all of V510 versions are eguipped with secondary low pitch stop installed inside the guide tube Secondary stop prevents the movement of blades into the low pitch not less than 89 if the feedback failure occurs All stops are internal and cannot be changed No adjustment is necessary because during manufacturing all pitch settings were made Model V508H only Sigle acting servomechanism consists of piston piston rod hydraulic cylinder and fork Pressure oil from the governor is supplied to the cylinder through the channel in the piston rod to control low pitch of the blades Oil pressure acts on the piston in the cylinder Through the piston rod the piston is joined with the fork in the hub All blade bushings are coupled with the fork through the pitch change blocks installed on the pins on the blade bushing faces Pitch change blocks transfer the linear motion of the piston with the fork to rotary motion of the blades High pitch of the blades is controlled by the compression spring inside the cylinder The spring force acts against the oil pressure force All stops are internal and cannot be changed However an adjustment of minimum flight angle is possible Refer to procedure in this manual Propeller blades
171. dlo ka je pod hlavou roubu a dal podlo ka je vlo ena do vybr n v p rub regul toru sra en m dovnit Pojist te nejm n t i rouby nerezov m v zac m dr tem obr zek 11 7 Upev ovac rouby Obr zek 11 7 Upev ovac rouby regul toru 19 Pokud vrtule nen v praporov poloze nato te listy do praporu tak aby beta krou ek dosedl na p rubu vrtule UPOZORN N VRTULOV LISTY UCHOPTE V KORENOV STI NIKDY NE U PI KY POZN MKA P ku Rn m ete p i p estavov n vrtulov ch list oto it k dorazu praporu 16 aby olej ze servomechanismu prot kal a nekladl odpor 20 Instalujte nosi kluznych kamen obr zek 11 6 na p ku Zv a na beta krou ek Na ep nosi e nasa te podlo ku a zajist te z vla kou 1 6x10 POZN MKA P i ka d instalaci pou ijte novou z vla ku 21 Pokud je instalov n elektrohydraulick ovlada LUN7880 a pomocn erpadlo E 1500 INSTALLATION AND OPERATION MANUAL 18 Fix the governor using four bolts figure 11 7 using suitable wrench A spring washer is at bolt head and the second washer is inserted into governor flange recess with chamfer facing governor Secure at least three bolts using stainless steel lock wire figure 11 7 Mounting 4 y ET bolts Lid Figure 11 7 Governor mounting bolts 19 If the propeller is not in feather move it to feather by turning blades to move the beta
172. e 1 2 De icer 2 33 Liner 3 2 Spinner bulkhead 1 3 O ring 2 34 Screw 3 3 Nutplate 2 35 Spinner flange 3 4 Nutplate 2 0 Hub 2 36 Pin 3 5 Rivet 2 1 Piston 2 37 Pin 3 6 Screw 2 2 Cylinder 2 38 Liner 3 7 Washer 2 3 Cylinder plate 2 39 Liner 2 4 Cylinder nut 2 40 Pin 7 1 Slip ring assy 2 5 Fork 2 41 Pin or Spacerring 2 6 Tube 2 42 Retaining ring 7 2 Cable assy 2 7 Insert 2 43 Pin 7 3 Lead clip 2 8 Overspeed governor 2 44 Washer 7 4 Screw 2 9 Clamp 2 45 Screw 7 5 Nut 2 10 Beta ring 2 46 Screw 7 6 Washer 2 11 Beta rod 2 47 Castle nut 7 7 Gable holder 2 12 Blade bushing 2 48 Washer 7 8 Screw 2 13 Pitch change block 2 49 Cotter pin 7 9 Washer 2 14 Washer 2 50 Screw 7 10 Screw 2 15 Retaining ring 2 51 Screw 7 11 Screw 2 16 Fork guide 2 52 Lock washer 7 12 Nut 2 17 Bearing ring 2 58 Screw 7 13 Terminal plate 2 18 Ball 2 54 Selflocking nut 7 14 Insert 2 19 Separator 2 55 Washer 7 15 Spacer 2 20 Nut 2 56 O ring 7 16 Brush block assy 2 24 Clamp bolt 2 57 O ring 7 17 Screw 2 22 Clamp nut 2 58 Sealing 7 18 Washer 2 23 Cotter pin 2 59 O ring 2 24 Flange bolt 2 60 O ring 2 25 Washer 2 61 O ring 2 26 Support 2 62 O ring 2 27 Snap ring 2 63 O ring 2 28 Spring 2 64 O ring 2 29 Lock piece 2 65 O ring 2 30 Lock washer 2 66 Reverse stop 2 31 Pin 2 67 O ring Table 4 1 Partlist reffering to Figure 4 1 61 10 00 DESIGN AND OPERATION INFORMATION Page 4 5 2012 02 06 AVIA PROPELLER INSTALLATION AND OPERATION MANUAL
173. e V508H utahovac m momentem N stavec 19 mm 3 4 inch N stavec pro uta en na moment a demont mont n ch roub matic N stavec pro uta en na moment a demont matice obj mky listu pouze verze V510 pou iteln s moment kl em a povolovac p kou N stavec 22 mm 7 8 inch N stavec pro uta en na moment a demont matice obj mky listu pouze verze V508 Nen t eba pro vrtule ady V510 pou iteln s moment kl em a povolovac p kou Povolovac p ka P ka pro povolen mont n ch roub matic a matic obj mek listu Strana 10 1 6 2 2012 Tabulka 10 1 Speci ln n ad SPECI LN N AD may be listed Designation Description Illustration Torque wrench Wrench to tighten and torque the mounting bolts except model V508H or mounting nuts only model V508H Socket 19 mm 3 4 inch compatible with torque wrench and breaker bar Socket to tighten torque and remove mounting bolts nuts Socket to tighten torque and remove blade clamp nuts models V510 only Socket 22 mm 7 8 inch compatible with torque wrench and breaker bar Socket to tighten torque and remove blade clamp nuts only models V508 No needed for V510 series propellers Breaker bar Bar to remove the mounting bolts nuts and blade clamp nuts 61 10 00 Table 10 1 Special tool SPECIAL
174. e face of each brush contacts the copper ring throughout full 360 degrees of slip ring rotation Refer to Figure 5 14 2 5 Cancelled NOTE Other types of brush assemblies should be installed according to aircraft manual SLIP RING ROTATION 2 SLIP RING ASSY 7 1 j 1 7 E 1 1 2 2 4 mm 0 047 0 095 inch DR RC E BRUSH BLOCK ASSY Figure 5 14 1 Page 5 11 1 INSTALLATION AND OPERATION INSTRUCTION 2015 07 07 61 10 00 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL PRENOSOV KRUH UHL K SLIP RING BRUSH PATN SPR VN PATN INCORRECT CORRECT INCORRECT Obr zek 5 14 2 Figure 5 14 2 A 4 DVA ROUBY P IPEV UJ C SB RA K MONT N KONZOLE Obr zek 5 15 G MONT KRYTU VRTULE Spr vn pozice p edn ho krytu v i zadn mu krytu je d na mont n mi zna kami na jedn v ztuze zadn ho krytu a jednom v ezu v p edn m krytu obvykle u listu 1 P ed mont p edn ho krytu pot ete gumov krou ek uvnit krytu vazel nou Pro p ipevn n p edn ho krytu pou ijte dodan rouby a podlo ky Po spr vn mont i krytu jsou sla vyra en na v ztuze zadn ho krytu a pobl v ezu p edn ho krytu proti sob H Z KLADN NASTAVEN PO INSTALACI Nastaven zar
175. e loosen NOTE It is recommended to dismount brush block if applied before propeller removal from engine or protect the brushes properly otherwise the brushes could be damaged Remove the beta block from the beta linkage and from the beta ring Remove the spinner dome Use a crane hoist with a sling for hanging the propeller or if the blades are removed use a special hanger installed to the blade bushing Page 5 14 INSTALLATION AND OPERATION INSTRUCTION 2012 02 06 AVIA PROPELLER POZN MKA Ujist te se e nosnost je bu a popruh je vy ne 200kg 440Lbs Demontujte dva p rubov rouby z p ruby motoru Instalujte dva vod c epy do uvoln n ch z vitov ch otvor v p rub vrtule POZN MKA Doporu uje se pou it vod c ch ep p i demont i vrtule jinak m e doj t k z va n mu po kozen p ruby motoru Sejm te vrtuli z motoru Vyjm te vod c z p ruby vrtule POZN MKA P rubovou st vrtule zakryjte p epravn z tkou pro zabr n n vyt k n oleje z vrtule a po kozen p ruby Na z tku navle te p rubov t sn c krou ek a p ipevn te ji k vrtuli p rubov mi rouby s podlo kami K SE ZEN MINIM LN HO LETOV HO HLU VERZE V508H Se zen minim ln ho letov ho hlu je mo n po demont i kryc ch v ek beta t hel Postupujte n sledovn obr zek 5 16 1 Odstra te poji ovac dr t ze roub kryc ho v ka
176. e of leakage NOTE A new or newly overhauled propeller may leak slightly during the first several hours of operation This leakage may be caused by the seating of seals and o rings and the slinging of lubricants used during assembly Such leakage should cease within the first ten hours of operation a Oil leakage is usually caused by damaged seal Inspect the propeller and identify source of leakage Potential sources of oil leakage are displayed in figure 6 2 VIEW FROM ENGINE FAULTY SEAL BETWEEN THE PROPELLER HUB AND THE ENGINE FAULTY SEAL OF THE HYDRAULIC CYLINDER FAULTY SEAL 1 m OF THE BETA ROD 7 FAULTY SEAL IN THE BLADE BEARING FAULTY SEAL OF a OVERSPEED GOVERNOR mM Figure 6 2 Potential sources of oil leakage model V508 displayed NOTE If cause of oil leakage is damaged seal between propeller hub flange and engine flange remove the propeller from engine and replace defective o ring by new from propeller spare parts In other cases contact Avia Propeller b If source of leakage as stated above is not determined inspect thoroughly entire surface of the hub for the crack Page 6 6 INSPECTIONS T AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 2 Vibrace 2 Vibration UPOZORN N WARNING NADM RN VIBRACE MOHOU B T P ZNAKEM VADY LISTU VRTULE NEBO KOMPONENTU ULO EN LISTU ZTR TA LISTU ZA LETU M E VY STIT V KATASTROFICKOU NEHO
177. e spinner bulkhead Strana 7 2 NE Page 7 2 13 4 2010 UDRZBA 61 10 00 MAINTENANGE 2010 04 13 AVIA PROPELLER C Nep ekra ujte maxim ln povolenou v hu 25g na jednom m st To se rovn p ibli n esti podlo k m AN970 3 d Pro p ipevn n z va pou vejte leteck rouby 10 32 inch Vyva ovac rouby p ipevn n na zadn m krytu mus vy n vat ze samojistn matice minim ln jedn m a maxim ln ty mi z vity e Ka d dynamicky vyv en vrtule mus b t opat ena t tkem na listu 1 Tento t tek upozor uje v robce nebo servisn st edisko e sou asn konfigurace z va nemus b t platn pro statick vyv en f Po et a um st n z va dynamick ho vyv en i statick ho vyv en pokud bylo zm n no mus b t zaznamen no do z znamn ku vrtule C USKLADN N PROVOZOVAN VRTULE V p pad demont e vrtule z motoru a jej ho del ho uskladn n demontujte vrtulov listy 2 pouzder Ot ete viditeln d ly vrtule a vrtulov listy tak aby byly such a ist UPOZORN N Dbejte aby se p i skladov n v dn m m st vrtule a list nedr ela vlhkost a nebo voda V nujte zvl tn pozornost ko en m list Vlhkost nebo voda v z vitu a nebo ve st edov m otvoru listu zp sob korozi a pozd j vy azen listu v r mci gener ln opravy Chra te kovov d ly vrtule tenkou vrstvou protikorozn ho oleje POZN MKA P
178. e v le list dle odd lu V le listu v t to kapitole f Zkontrolujte dr hu listu dle odd lu Dr ha listu v t to kapitole 3 V le listu 3 a Zkontrolujte v le list podle obr zku 6 3 Maxim ln p pustn v le V le na pi ce list 4 mm 0 16 inch pouze vrtule V508 P edozadn v le 4 mm 0 16 inch pouze vrtule V508 Radi ln hlov v le 1 m eno na kontroln m ezu rozd l mezi v emi listy nesm b t v t ne 0 5 Axi ln v le 0 8 mm 0 032 inch pouze vrtule V508 Strana 6 7 6 22012 PROHLIDKY 61 10 00 8 S Troubleshooting procedures typically begin with an investigation of the engine Aircraft components such as engine mounts or loose landing gear doors can be the source of vibration Perform evaluation of possible sources of vibration in accordance with engine and or aircraft manufacturer s instructions If no cause is found proceed according the following steps Remove the spinner dome and visually inspect the entire blades and visible hub components for cracks mechanical damage and other unusual condition If crack is found or in case of any doubt contact Avia Propeller Check correct installation of the blades in the bushings Verify that the position line on the blade shank coincide with the line on the blade bushing face Max tolerance for blade and bushing marks straightness is one half of blade mark thickness Reinstall the blade per Install
179. ebo gener ln oprav k v robci nebo do autorizovan ho servisn ho st ediska Pokud je jako n pravn opat en po adov no vy azen vrtule mus b t vrtule sta ena z provozu Takov vrtule je neopraviteln Strana 6 12 6 2 2012 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Overtorque E OVERHAUL rcent Pe NO ACTION NECESSARY Duration of Overtorque in Seconds Figure 6 8 Overtorque event For engine mounted accessories governors pumps propeller control units manufactured by Avia Propeller any overspeed at a severity level and or duration sufficient to require at minimum a search inspection for the propeller will require the accessory to be disassembled and inspected in accordance with the applicable maintenance manual Regardless of the degree of damage make a log book entry to document the overspeed event Corrective Action When no action is necessary no maintenance is necessary other than to verify that the overspeed was not caused by a mechanical problem When overspeed inspection or overhaul is required the propeller must be removed from service and be sended to manufacturer or authorized repair station for inspection or overhaul When the corrective action requires to scrap the propeller must be removed from service Such propeller is not repairable Page 6 12 INSPECTIONS 2012 02 06 AVIA PROPELLER 2 der blesku V p pad de
180. ected Damaged parts are repaired or replaced All sealing elements are replaced Corrosion preventive coatings of the parts are renewed Propeller is reassembled adjusted and balanced The overhaul interval is usually referred to as Time Between Overhaul TBO The TBO limit is based on operation limit expressed in hours of operation and on calendar limit expressed in calendar months The overhaul should be accomplished if one of this limit is acquired whichever occurs first The overhaul shall be accomplished only by Avia Propeller or authorized service station in accordance with latest revision of the Overhaul manual mentioned in section Related documents in this chapter Page 2 1 GENERAL 2014 01 17 AVIA PROPELLER C Souvisej c dokumenty 1 P ru ka Avia E 1461 61 10 61 P ru ka pro gener ln opravu P ru ka Avia EN 1370 61 10 70 P ru ka pro gener ln opravu kovov list Servisn bulletin Avia 1 Obsahuje intervaly gener ln ch oprav v ech vrtul Avia Bulletin je k dispozici na www aviapropeller cz P ru ka Avia E 1395 61 01 95 Standard Practices Manual 5 Dal servisn dokumenty Avia Servisn bulletiny Servisn dopisy Servisn doporu en kter mohou souviset s vrtulemi v t to p ru ce jsou k dispozici na www aviapropeller cz 2 B Rozm ry V echny rozm ry v t to p ru ce jsou uv d ny v milimetrech zkratka mm s p
181. edena do provozu b hem 24 m s c od data vyroben nebo gener ln opravy UPOZORN N NEUVEDEN VRTULE DO PROVOZU B HEM 24 M S C OD DATA VYROBEN NEBO GENER LN OPRAVY M ZE M T ZA N SLEDEK SN ZEN LIMITU KALEND N HO TBO PLN INFORMACE JSOU UVEDENY V SERVISN M BULLETINU 1 V ROBCE AVIA PROPELLER UPOZORN N INSTALACE VRTULE NA MOTOR POZD JI NE 24 M S C OD DATA VYROBEN NEBO GENER LN OPRAVY NEBO VR CEN VRTULE DO PROVOZU PO USKLADN N DEL M NE 24 M S C BEZ PROHL DKY V AVIA PROPELLER NEBO AUTORIZOVAN M SERVISN M ST EDISKU M E M T ZA N SLEDEK NIKY OLEJE A NESPR VNOU FUNKCI VRTULE V CE INFORMAC V SERVISN M BULLETINU 1 V ROBCE AVIA PROPELLER Strana 9 1 12 5 2015 DOPRAVA A SKLADOVANI E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 9 SHIPPING AND STORAGE Use an original shipping boxes and fixing elements for any shipment of the propeller and blades If it is not possible properly fix the hub and blades to avoid damage during the shipment Use an original hub flange protecting plug or protect the hub flange properly with soft material during the shipment or storage after removal of the propeller from engine The propeller and blades to be stored in a controlled environment under temperature of 20 to 35 5 to 95 F and relative humidity of 10 to 7596 Avoid extreme temperature and or humidity differences or cycles CAUTION THE PRO
182. eep this arrangement during adjustment Insert gage 1531 042 engine toolkit between stop and stop pin figure 11 15 When the clearance between the stop and the stop pin is smaller shorten rod BZ2 by turning CAUTION SHORTEN THE ROD ONLY INSTALLED ON THE GOVERNOR DO NOT REMOVE THE ROD AT ANY END f Moving with the tracking lever clamp the gage 1531 042 and adjust length of element 32 such way that carbon block assembly on the lever Zv is not pressed to the beta ring on one side when the beta ring is retracted and eliminated clearances The carbon block assembly must be free and axial clearance between the beta ring and carbon blocks is equally divided to both sides a Beta QSSeIT block ibly Figure 11 16 Beta ring clearance Figure 11 15 Adjustment with element 32 Page 11 26 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER UPOZORN N CELKOV V LE MEZI BETA KROU KEM VRTULE A KAMENY NA OBR ZKU 11 16 JE U NOV HO NOSI E KLUZN CH KAMEN 0 15 0 18 mm 0 006 0 007 inch NESM B T MEN V PROVOZU JE PR PUSTN CELKOV V LE MAX 0 4 mm 0 016 inch 9 Strana 11 27 6 2 2012 Hub model Typ vrtule All models except V echny verze mimo V508D AG with blades s listy 84 99A 99B Celkovou v li zm te p i mont i regul toru n sledovn P i vyjmut m rce 1531
183. el Verify propeller operation from reverse to feather This part is described in respective Flight Manual in a chapter describing the engine test Page 5 13 INSTALLATION AND OPERATION INSTRUCTION 2012 02 06 AVIA PROPELLER UPOZORN N PRI P ECHODU VRTULOVYCH LIST Z REVERZU JE NEZBYTN PONECHAT V KON MOTORU NA POZEMN M VOLNOB HU DOKUD NEZHASN BETA KONTROLKA V KABIN LETOUNU ZV EN V KONU P I ROZSV CEN SIGNALIZACI BETA M E ZP SOBIT P ETO EN VRTULE Prove te zastaven motoru dle Letov p ru ky Po pozemn m b hu zkontrolujte vrtuli na nik oleje v li vrtulov ch list a stav komponent odmrazovac ho syst mu Letov zkou ka Prove te letovou zkou ku v souladu s Letovou p ru kou UPOZORN N P KY OVL D N MOTORU A VRTULE PRESTAVUJTE V DY POMALU PRO ZABR NEN PRETO EN J DEMONT VRTULE Z MOTORU POZN MKA Pro pr stup k mont n m roub m matic m mus m t vrtule v dy beta krou ek pln zasunut do n boje U verze V508H mus b t pro zasunut beta krou ku pou it stahov k 900 0175 Pou ijte stahov k stejn m zp sobem jak je uvedeno v odd lu Mont vrtule V508H na motor v t to kapitole POZN MKA P ed vyjmut m list z pouzder odpojte kabely od odmrazovac ch t les a povolte obj mky list POZN MKA Doporu uje se sejmout elektrick sb ra je li pou it p ed demont vrtule z motoru p padn d kladn
184. ent 17 Install the carbon block assembly figure 11 6 onto the lever Zv and the beta ring Install the washer onto the pin and safety with cotter pin 1 6 x 10 CAUTION Use new cotter pin each installation 18 If hydraulic valve LUN7880 and auxiliary pump LUN7840 are installed follow this procedure a Remove locking wire on the turning screw figure 11 8 and loose it Loose tube at the valve LUN7880 and tube from the auxiliary pump LUN7840 at the engine wall b Connectthe tube from valve LUN7880 to the fitting with arrow and lightly tighten CAUTION Arrow on non return valve must point up as shown on the figure Keep tubes clean C Connectthe tube from the auxiliary pump LUN7840 to fitting marked with T with ball 5 16 inside and lightly tighten d Tighten the turning screw at synchronous tightening of tube connections CAUTION The turning screw must not get jammed thread in the governor could be damaged Page 11 23 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER e Ov te Ze je v uzav rac matici kuli ka 5 16 a matici dot hn te Cel spojen pojist te v zac m dr tem obr zek 11 12 19 Na p ku Rn zapojte t hlo od ovl dac p ky vrtule obr zek 11 12 a pojist te 20 Na p ku Bc v z kladn poloze ryska na p ce s va kou se kryje s ryskou min letov ho hlu na stupnici regul toru a ep ovl dac p ky se dot k dorazu obr zek 11 12 zapojte t hlo od ovl d
185. ent 37 with nut and safety washer 9g Lubricate the cam travel with a suitable grease Page 11 29 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Ovl dac p ku motoru v kabin letounu p esu te z reverzn polohy zp t do polohy h Move the engine condition lever in aircraft cockpit from reverse position back to minim ln ho letov ho hlu minimum flight pitch Ru n m p estaven m list vysu te beta krou ek z vrtulov hlavy a pomoc vhodn ho i Adjust the blades by hand so that the beta ring protruded from the propeller hub and fix p pravu zajist te ve vzd lenosti 4 5 mm 0 177 inch od n boje T hlo Sv 65 it by appropriate means at distance of 4 5 mm 0 177 inch from the hub flange Place zasu te vidlic na kulisu Sv a do vidlice vlo te ep tak aby proch zel otvorem the rod Sv 65 with yoke onto the gate Sv and insert pin into the yoke to go through kulisy the gate P esu te ovl dac p ku motoru a t m i p ku Bc z polohy minim ln letov hel Move the engine condition lever and thus also the lever Bc from position minimum sm rem k poloze reverz a do okam iku kdy uc t te odpor proti pohybu kdy ep flight pitch toward to reverse until you feel drag against movement when pin touches t hla Sv dosedne na koncovou dorazovou plochu kulisy Sv the gate Sv Kontrolujte kryje li se
186. ent of the stop 58 disturbs alignment of guideline on the cam lever with the governor scale Change lever 29 length figure 11 33 Remove lock wire from both nuts nuts with left and right thread the nut with left thread is marked with letter L from the rod 29 and adjust its length with turning such way that alignment is rearranged Press the lever Bc in direction of the arrow whole mechanism to the stop 58 Page 11 58 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER m Po korekci t hla 29 dot hn te jeho matice a zkontrolujte znovu kryt rysek Ob Strana 11 59 13 4 2010 matice zajist te v zac m dr tem T hlo 29 Ryska minim ln ho letov ho hlu Obr zek 11 33 Se zen na rysky t hlem 29 Stejn m zp sobem se i te druh regul tor V zac m dr tem a plombou zajist te dorazy 58 obou regul tor Se zen zapi te do atestu regul tor Vrtulov regul tor LUN7816 Se zen maxim ln ch regulovan ch ot ek vrtule Prov d se po prv m z letu letounu Prove te se zen max regulovan ch ot ek dle postupu v odd lu 11 8 UPOZORN N Maxim ln regulovan ot ky nesm p ekro it 2080 ot min SYST M OVL D N VRTULE E 1500 INSTALLATION AND OPERATION MANUAL m Then tighten the nuts and verify again the alignment of guidelines Safety both nuts 61 10 00 with w
187. epo tem na palce inch V echny teploty uveden v t to p ru ce jsou uvedeny ve stupn ch Celsia zkratka C s p epo tem na stupn Fahrenheita zkratka F Pro v echny metrick jednoky je jako desetinn odd lova pou ita rka pro v echny palcov jednotky je jako desetinn odd lova pou ita te ka Objedn v n d l P i v m n d l z d vodu jejich po kozen nebo ztr ty je nezbytn pou vat pouze origin ln d ly Kontaktujte v robce vrtule pro informace a nebo objedn n origin ln ho d lu POZN MKA Ne v echny d ly vrtule mohou b t m n ny v provozu Pouze n kter vn j d ly jako t sn c krou ek p ruby a spojovac materi l rouby matice kabely mohou b t v provozu vym n ny Strana 2 2 gt 6 2 2012 OBECNE 61 10 00 E 1500 INSTALLATION AND OPERATION MANUAL C Related documents 1 Avia Manual E 1461 61 10 61 Overhaul Manual 2 Avia Manual EN 1370 61 10 70 Overhaul Manual for Metal Blades 3 Avia Service Bulletin No 1 Includes an overhaul intervals of all Avia propellers Available on Avia website at www aviapropeller com 4 Avia Manual E 1395 61 01 95 Standard Practices Manual 5 Other Avia service documents Service Bulletins Service Letters Service Advisories which may relate to propellers in this manual are available on Avia website at www aviapropeller com Dimensions All measurements in this manual are p
188. er terminal board in line with holes in the clamp and connect cable to de icer Install the upper terminal board and sheet metal holder and attach all parts with fixing screws to the clamp Safety the screws with stainless steel wire 0 8 mm 0 032 inch j 4l lt Z C Figure 5 13 De icing type C F BRUSH BLOCK INSTALLATION Brush assemblies 068 5320 076 5300 and 066 5300 1 Check free movement of all brushes before installing Compress and release the brushes noticing any bind or hang up inside the block 2 Install the brush block assembly into its place on the engine gearbox Safety all mounting screws to each other with 0 81 mm 0 032 inch stainless steel wire 3 Check the brush block assembly for correct distance and angular location to the slip ring as shown in Figure 5 14 1 The distance between brush block and slip ring should be between 1 2 and 2 4 mm 0 047 to 0 095 inch and brush block should be angled of 2 degrees from perpendicular of the copper rings toward the direction of slip ring rotation As required reposition the brush assembly on the mounting bracket as follows a Loosen two screws attaching the brush block to the mounting bracket Refer to Figure 5 15 b Reposition the brush block to establish the correct dist
189. eta krou ku p i BETA lampy rozsv cen lampy 9 5 0 1 mm 0 374 0 004 inch Table 11 1 Min flight pitch adjustment of propellers V508 Type Series with governor LUN7815 61 10 00 Page 11 27 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER 2 Se zen axi ln v le blokovac ho oup tka regul toru prvkem sdru en vazby 65 plat pro regul tor LUN7815 02 E 1500 INSTALLATION AND OPERATION MANUAL 87 a se zen 2 Axial clearance of blocking valve adjustment with element 37 and coupled connection 65 for propeller governor LUN 7815 02 a Ovl dac p ku vrtule v kabin letounu p esu te do polohy maxim ln ch ot ek P ka a Move the propeller condition lever in cockpit to position of maximum RPM The Rn na regul toru se t m p esune na doraz max ot ek 15 governor lever Rn move then to maximum RPM stop 15 b Kontrolujte zda je vypojeno t hlo Sv 65 z kulisy Sv obr zek 11 17 Pokud nen b Verify whether rod Sv 65 is disconnected from the gate Sv figure 11 17 If not vy roubujte matici a vyjm te ep z vidlice t hla Potom t hlo vysu te mimo kulisu Sv remove its nut and pin from the rod yoke Then eject the rod out from the gate Sv C Uvoln n t hlo Sv 65 zafixujte tak aby jeho pohyb nebr nil p i dal pr ci c Loosen rod Sv 65 fix
190. ews remove the screws and cover cap CAUTION Remove the cover cap with care due to it is slightly preloaded by the spring inside 2 Remove the spring guide with the spring 3 Remove the other cover caps in the same way NOTE Take care not to loose any dismounted component 4 Slide the hollow wrench P N 900 0176 onto the beta rod and insert to the hub Adjustment of minimum flight angle is provided by turning the adjusting nut on the beta rod through the adapter installed over the nut Figure 5 16 Refer to v tabulce 5 1 table 5 1 to see how turning the nut affects the propeller RPM mU MONT ZN A PROVOZN INSTRUKCE 61 10 00 INSTALLATION AND OPERATION INSTRUCTION 2985 15 AVIA PROPELLER VAROV N V ECHNY T I SE IZOVAC MATICE MUS B T NASTAVENY SHODN OTO ENY O STEJNOU HODNOTU JINAK HROZ HOUP N BETA KROU KU A PO KOZEN STAV C HO MECHANISMU VRTULE Obr zek 5 16 Nastaven minim ln ho letov ho hlu vrtule V508H WARNING ALL THREE ADJUSTING NUTS MUST HAVE THE SAME SETTING TO EACH OTHER BE SAME ROTATED OTHERWISE THE PITCH CHANGE MECHANISM COULD BE DAMAGED BECAUSE OF THE WOBBLING OF THE BETA RING Se izovac matice TN P ibli n zm na Strana 5 16 28 2 2012 Pohled S AM vrtule 1 turn 100 2 turn 200 3 turn 300 1 turn 100 2 turn 200 3 turn 300 Tabulka 5 1 MONT N A PROVOZN INSTRUKCE
191. for damage e Inspect the brushes of the brush block for excessive wear as follows 1 lt 61 10 00 Brush block P N P3560 Remove the back cover Insert a 2 5 mm 0 1 inch diameter rod into each check hole in the brush block If the length of the rod inserted into any hole exceeds 33 5 mm 1 3 inch then all brushes must be replaced Brush blocks P N s 068 5320 076 5300 066 5300 Insert a 2 5 mm 0 1 inch diameter rod into each check hole in the brush block backside If the length of the rod inserted into any hole exceeds 9 mm 0 35 inch then all brushes must be replaced Brush block P N LUN7850 7 Insert a 0 8 mm 0 03 inch diameter wire into each check hole on side of the block with brushes If the length of the wire inserted into any hole exceeds 8 mm 0 315 then all brushes must be replaced Page 6 10 INSPECTIONS AE AVIA PROPELLER E SPECI LN PROHL DKY 1 P eto en vrtule P ekro en krout c ho momentu na h deli motoru P eto en vrtule nastane pokud ot ky vrtule p ekro maxim ln ot ky uveden v Typov m Certifik tu p slu n ho typu vrtule K p ekro en krout c ho momentu na h deli motoru dojde v p pad e zat en motoru p ekro limity stanoven v robci motoru vrtule a letounu N pravn opat en jsou z visl na m e a trv n p eto en vrtule nebo p ekro en krout c ho momentu motoru u ka d ho jednotliv ho p padu Pokud
192. gain propeller idle speed after stop 58 adjustment at engine ground test oil temperature 60 65 140 150 F Find value of dimension B in the governor documentation Measure dimension B for the governors according to figure 11 32 and compare with values in the governor documentation Before the measurement verify real contact at stop 58 Control lever Figure 11 32 Dimension B check If measured dimension B is different more than 0 1 mm compare to reported value adjust dimension B according to the reported one by adjustment of the stop 58 and verify speed of both propellers at engine ground test according to aircraft flight manual If both dimensions are equal to dimensions in the governor documentation perform adjustment of the stop 58 for both governors based on real idle RPM see below based on half of the difference Find speed difference half in the table 11 5 where read value for the stop 58 adjustment Page 11 57 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL n E sme ds rude counterclockwise turning clockwise turning Doraz 58 odinov ch ru i e odinov ch ru i e Stop 58 1 ot ka 0 5 ot ky 0 5 ot ky 1 ot ka 1 turn 0 5 turn 0 5 turn 1 turn O 40 20 20 40 40 20 20 40
193. gul toru Korigujte d lku t hla 29 obr zek 11 33 Sejm te v zac dr t z obou matic matice s lev m a prav m z vitem matice s lev m z vitem je ozna ena p smenem L t hla 29 a se i te ot en m jeho d lku tak aby nastalo op tn kryt rysek P kou Bc dotla ujte ve sm ru ipky cel soup na doraz 58 SYST M OVL D N VRTULE Adjusting the stop 58 based on propeller idle speed difference half reduce the speed at idle of propeller with higher RPM and increase the speed at idle of propeller with lower RPM This adjustment reduces difference to minimum 1 Remove securing of the stops 58 hold the screw with a wrench use another to loose the securing nut Turn the stop 58 on both governors according to value found in the table 11 5 ID Verify for both governors the dimension B which changes 0 35 mm 0 014 inch when half a turn is used and 0 7 mm 0 028 inch when 1 turn is used If you will find a deviation adjust the dimension B to the calculated value For fine adjustment use 1 3 or 1 4 turn of the stop 59 CAUTION TURNING WITH THE STOP 58 FOR MORE THAN t1 TURN IS NOT PERMITTED 61 10 00 Hold the screw in adjusted position with suitable wrench use the second wrench to tighten the securing nut and again verify the dimension B for both governors This adjustm
194. gure 11 4 12 Kulov lo iska prvk les a dal p slu n povrchy nama te vazel nou 12 Grease bearings of elements P9 and 65 and other appropriate surfaces 13 Stla en m p ky BI ve sm ru ipky obr zek 11 3 p i poloze p ky Rn v poloze 13 Verify function of the pilot valve locking by pressing the lever BI figure 11 3 when max ot ek kontrolujte chod blokovac ho oup tka po uvoln n se mus oup tko the lever Rn is at maximum RPM stop after releasing the pilot valve must return to vr tit samo zp t Prove te minim ln 3x its original position Perform min three times suena Lied SYST M OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM Page iT 13 4 2010 2010 04 13 AVIA PROPELLER Pojistn krou ky P ka Zv Kluzn Cep kameny Podlo ka 7 EXEC N Z vlacka kluznych kamen Obr zek 11 6 Nosi kluznych kamen 14 Kontrolujte dosedac plochu pr ruby regul toru s centr z a pr rubu na reduktoru motoru Plochy mus b t ist bez po kozen povrchu Plochy o ist te ist m hadrem p padn namo en m do rozpou t dla 15 Do h dele regul toru obr zek 11 4 vlo te torzn ty inku ty hranem dovnit Zkuste ot et torzn ty inkou jej pohyb mus b t voln UPOZORN N Ii TORZN TYCINKA MUS M T VYZNACENO C SLO MONTOVAN HO REGUL TORU 16 Pokud je instalov na vrtule sejm te nosi
195. h description of figures 5 6 and 5 7 in right column was changed to English Page 5 6 Reference to figure 5 9 at point 7 in right column was corrected to 5 8 Page 5 16 English text in table 5 1 in left column was changed to Czech Page 7 5 Figure number in right column was corrected from 7 1 to 7 2 Page 7 7 Reference to figure 7 2 in section 2 a in right column was corrected to 7 4 Adding information on minimum oil temperature for propeller operation Page 2 1 Information on TBO has been moved to the beginning of Overhaul chapter Page 3 2 Revised Designation of V510 series propellers Pages 4 4 4 6 4 8 4 10 Revised figures of the propeller assemblies Page 5 1 Added note about the spinner assembly with screwed front bulkhead Added note not to use the o ring installed on the shipping plug Page 5 2 Revised caution about using the guide pins Pages 5 8 5 9 Added inspection of the blade clamp after torquing Pages 5 11 to 5 12 Revised installing and positioning of the brush assembly Page 6 10 Revised wear inspection of brushes of LUN7850 7 brush assembly Pages 7 6 7 9 7 10 Revised treatment of local repair of the blade Page 10 3 Added special tools for propeller V508H Page 11 4 2014 01 17 AVIA PROPELLER C slo zm ny Datum vyd n SEZNAM ZM N Zm n n strany E 1500 Stru n popis INSTALLATION AND OPERATION MANUAL LIST OF REVISIONS Rev No Issue Date Revise
196. h kontrolujte dobu od rozsv cen do zhasnut signalizace PRAPOROV ERPADLO mus b t 12 15 s Kontrola funkce NOUZOV PRAPOROV N Vypn te jisti e PRAPOROV N Ovl dac p ku motoru nastavte na doraz volnob hu Ovl dac p ku vrtule p estavte z polohy max ot ek do praporov polohy IO IO 100 SYST M OVL D N VRTULE 61 10 00 INSTALLATION AND OPERATION MANUAL Propeller speed moving the engine control lever increases up to stabilization approx 1100 to 1200 rpm even engine control lever movement continues Energizing the BETA lamp fast increase follows to value approximately 1400 to1500 rpm Generator speed increases when BETA lamp is energized Io 192 IO 4 If described development corresponds to observed actions secondary pitch lock works correctly 5 Move engine control lever slowly and smoothly into maximum reverse position for period sufficient to read operational values Verify power in reverse mode of operation with engine operational manual Maximum reverse speed is 2030 rpm ID Move engine control lever slowly and smoothly back over idle stop Propeller speed follows engine control lever position continuously drops to idle Generator speed immediate drop to idle hold BETA lamp de energized at about 1100 rpm IO 17 100 7 Idle RPM must be the same like before Check of feathering installation with feathering pump AUTOMATIC FEATHERI
197. h other governors instruction of engine of governor manufacturer b Replace the propeller governor per instruction of engine manufacturer Trouble Increased resistance of engine condition lever movement into reverse Probably cause a Sediments at coaxial valve Remegy a Replace the propeller governor per instruction of engine manufacturer Trouble Rpm increase during normal operation without change of propeller lever position Probably cause a Governor failure Remegy a Replace the propeller governor per instruction of engine manufacturer Trouble Propeller rpm does not reach requested rpm during overspeed governor test Probably cause a Defective overspeed governor Remegy a Replace the overspeed governor per instruction of engine manufacturer Page 8 4 TROUBLESHOOTING 2012 02 06 AVIA PROPELLER Z vada Vibrace Mo n p ina a Vrtulov listy jsou nastaveny na rozd ln hly b Uvoln n ulo en listy c Trhlina na krytu d Nespr vn instalace vrtule na motoru e Spatn statick vyv en vrtule f Spatn dynamick vyv en vrtule N prava a Zkontrolujte zda jsou listy spr vn instalov ny v pouzdrech viz kapitola Mont n a provozn instrukce b Pokud je list uvoln n v ulo en vrtule mus b t sta ena z provozu a odesl na k v robci nebo do autorizovan ho servisn ho st ediska c Zkontrolujte kryt na v skyt trhlin d Zkontrolujte sp
198. horized repair centre Trouble Leakage in area of the overspeed governor Probably cause a Defective o ring under the overspeed governor Remegy a Send the propeller to manufacturer or authorized repair centre Trouble Blade shake Probably cause a Loose blade bearing Excessive play of the pitch change mechanism Remegy a Check the blade play according to procedure in section Inspections If any play exceeds the specified limits the propeller must be removed from service and be sended to manufacturer or authorized repair centre Page 8 8 TROUBLESHOOTING 2012 02 06 AVIA PROPELLER 9 DOPRAVA A SKLADOV N Pro p epravu vrtule a list pou vejte origin ln transportn obaly a fixa n elementy Pokud to nen mo n d kladn zafixujte hlavu a listy aby p i p eprav nedo lo k jejich po kozen Na mont n p rubu vrtule pou vejte origin ln ochrannou z tku nebo d sledn chra te p rubu m kk m materi lem b hem p epravy nebo uskladn n po demont i z motoru Vrtuli skladujte v zen m prost ed p i teplot 20 a 35 5 a 95 F a relativn vlhkosti 10 a 75 Zabra te prudk m zm n m nebo st d n teploty a vlhkosti v m st uskladn n vrtule UPOZORN N A VRTULE JE BALENA VE SPECI LN F LII OBSAHUJ C KOROZN INHIBITORY NEVYJ MEJTE VRTULI Z OBALU BEZ MYSLU INSTALOVAT JI NA MOTOR P edpokl d se e vrtule bude uv
199. i a dut roub V echna rouben a trubky pojist te v zac m dr tem Obr zek 11 37 V m na t sn c ch krou k zp tn ho ventilu 7 V m na nosi e kluzn ch kamen regul toru obr zek 11 38 V p pad opot eben kluzn ch kamen tyto vym te n sleduj c m zp sobem Sejm te z vla ku 55 a ep 52 s podlo kou 54 z p ky Zv 21 Sejm te opot ebovan nosi kluznych kamen 22 Nov nosi kluzn ch kamen 22 z n hradn ch d l pe liv prohl dn te zda m neporu eny kluzn kameny 79 a zda nejsou vypadl pojistn krou ky 80 UPOZORN N BEZ POJISTN HO KROU KU 80 NOSI KLUZNYCH KAMEN NESM TE NAMONTOVAT VADNOU Z VLA KU 55 VYM TE Namontujte nosi kluznych kamen dle kapitoly Mont regul toru Zkontrolujte z kladn se zen dle postupu v tomto manu lu Strana 11 69 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Connect tube 87 from the feathering valve LUN7880 0 if installed to the fitting 46 and tighten at both ends cap nut and the turning screw Secure all fittings and tubes with lock wire Figure 11 37 Replacement of non return valve sealing 7 Carbon block assembly exchange figure 11 38 In the case when carbon blocks are worn exchange them using following procedure Remove the cotter pin 55 and the pin 52 with washer 54 from the lever Zv 21 Remove the worn carbon block a
200. into the spinner dome see the marking CAUTION THE PROPELLER V508H S N 070031 HAS THE FRONT PLATE ATTACHED TO THE HUB THE SCREWS AT HALF OF THE SPINNER DOME MUST BE REMOVED OTHERWISE THE SPINNER DOME NOT TO BE REMOVED FROM THE PROPELLER Do not remove the screws attaching the cover plates to the rear bulkhead in the places of the blades if exist Figure 5 1 However if the cover plates have been removed reinstall them back into the rear bulkhead see the marking DO NOT REMOVE THESE SCREWS IF EXIST UNLESS STATED OTHERWISE gt REMOVE THESE M DO NOT REMOVE THESE SCREWS IF EXIST Figure 5 1 Page 5 2 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER C INSTALACE VRTULOVYCH LIST 1 Ramena vrtulov hlavy a vrtulov listy jsou ozna eny pozi n mi sly vzestupn od sla 1 pozi n m slem V dy instalujte list do ramene vrtule se shodn m a Pozi n slo ramene vrtule je vyra eno na ramenu b Pozi n slo listu je vyra eno za slem sady nap S 274 2 na ele ko ene Star listy mohou m t vyra eno pozi n slo za v robn m slem vrtule Nov vyroben nebo opraven listy maj pozi n slo uvedeno tak na nalepen m t tku UPOZORN N K INSTALACE LIST DO VRTULOV HLAVY V NESPR VN M PO AD M E V ST K NADM RN M VIBRAC M V PROVOZU E 1500 INSTALLATION AND OPERATION MANUAL C INSTALLING THE BLAD
201. ion and operation instruction ry M Z Nen t eba pro verzi V508H No needed for model V508H Z v s P N 059 8030 pro verze V508 Hanger P N 059 8030 for V508 series Z v s P N 068 8030 pro verze V510 Hanger P N 068 8030 for V510 series Pro mont vrtulov hlavy na motor s pou it m For hub installation on engine using a crane hoist je bu s popruhy viz Mont n a provozn with sling refer to Installation and operation instrukce instruction Tabulka 10 1 Speci ln n ad pokra ov n Table 10 1 Special tool cont d Strana 10 2 1 N N AN Page 10 2 6 2 2012 SPECIALNI 61 10 00 SPECIAL TOOLS 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL N zev Popis Vyobrazen Designation Description Illustration Stahov k beta P N 900 0175 f Beta puller P N 900 0175 f T k se pouze vrtule V508H S N 070031 Relate only to propeller V508H S N 070031 viz Mont n a provozn instrukce refer to Installation and operation instruction Kl P N 900 0176 pouze verze V508H Wrench P N 900 0176 model V508H only Adjustment of minimum flight angle of model V508H refer to Installation and operation instruction Se zen minim ln ho letov ho hlu verze V508H viz Mont n a provozn instrukce Tabulka 10 1 Speci ln n ad
202. ire Rod 29 Minimum flight pitch quideline Figure 11 33 Adjustment using rod 29 Use the same procedure for the second governor Secure the stops b8 for both governors Record works in governor documentations Propeller Governor LUN7816 Maximum RPM adjustment To be performed after control flight Perform maximum RPM adjustment according to procedure in section 11 8 CAUTION Maximum propeller RPM must not exceed 2080 rpm min Page 11 59 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 2 Ser zeni ot ek volnob hu Strana 11 60 6 2 2012 prov d se pouze v z stavb na dvoumotorovych letounech Toto se zen prove te pouze v p pad kdy rozd l volnob n ch ot ek vrtul je mimo p edepsanou toleranci 40 ot min a rozd l ot ek gener tor je max 0 5 Prove te kontrolu z kladn ho se zen obou regul tor podle postupu v kapitole 11 6 Neodpov daj li hodnoty se zen daj m podle atestu a postupu prove te nov se zen Je li z kladn se zen obou regul tor v po dku se i te volnob n ot ky gener tor podle Provozn p ru ky motoru tak aby rozd l ot ek byl max 40 ot min Po se zen zkontrolujte volnob n ot ky p i motorov zkou ce podle letov p ru ky letounu Teplota oleje mus b t dodr ena p i ode t n ot ek 60 65 C 140 150 F SYST M OVL D N VRTULE E 150
203. irecting oil to or from the propeller servomechanism Real propeller RPM corresponds with setting b Overspeed Refer to figure 11 1B The centrifugal force acting on the flyweights is greater than the speeder spring force The flyweights tilt outward and raise the pilot valve The pilot valve opens low pitch channel to drain blades moves to higher pitch and RPM goes down up to onspeed condition With governor LUN7816 high pitch side of the servomechanism is also pressurized at all the time by 0 6 MPa to help in pitch increasing c Underspeed Refer to figure 11 1C The centrifugal force acting on the flyweights is lower than the speeder spring force The flyweights tilt inward and lower the pilot valve The pilot valve opens low pitch channel to high pressure channel blades moves to lower pitch and RPM goes up to onspeed condition With governor LUN7816 the pressure at low pressure side of servomechanism must be high enough to exceed pressure of 0 6 MPa at high pitch side of the servomechanism and all other forces Page 11 3 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Strana 11 4 13 4 2010 E 1500 LUN 7815 LUN 7816 mem SSL SESS p d Tue M ne gt E SN nt bz STO ji TERA v T ae ii eaae EC EEE B iu p P o gt SSS Us MM Nin Bons YR BE E MPa 2 8 MPa A mm Hanf puc Een B Doma C
204. is not possible to reach maximum reverse position at the propeller governor or fuel control unit perform linkage adjustment according to aircraft engine operational manual Then recheck stops for idle and maximum reverse position Page 11 41 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER i Po se zen zasu te p ku Sv do p vodn polohy nasa te roub s pojistnou podlo kou ut hn te a zajist te POZN MKA P i ustaven p ky Sv do p vodn polohy dbejte aby otvor pro roub byl nastaven p esn proti dr ce v oup tku kterou proch z a z rove jist polohu p ky Sv j Dot hn te a zajist te p pojn m sta na p ce a regul toru paliva dle provozn p ru ky motoru 11 7 ZKOU EN A Vrtulov regul tor LUN7815 1 Kontrola z kladn ho se zen plat pro regul tor LUN7815 02 a Vypojte t hlo Sv 65 z kulisy Sv odjist te a vy roubujte matici a vyjm te ep z vidlice t hla Potom t hlo vysu te mimo kulisu Sv viz obr 11 17 b Uvoln n t hlo Sv 65 p iva te v zac m dr tem k pevn sti regul toru tak aby jeho pohyb v dal m pr b hu kontroly nebyl omezen c Ovl dac p ku vrtule nastavte do polohy max ot ek p ka Rn mus b t na dorazu max ot ek 15 d Ovl dac p ku vrtule nastavte do praporov polohy a zajist te p ka Rn mus b t na dorazu praporu 16 Ovl dac p ku vr
205. istov mi m rkami kontrolujte v li mezi va kou a se izovac m prvkem 37 na P edepsan v le je 0 1 0 3 mm 0 004 0 012 inch obr zek 11 18 f Nesouhlas li nam en v le s p edepsanou prove te jej se zen Odjist te matici na prvku 37 a povolte Prvek 87 p itom pridr te roubov kem P edepsanou axi ln v li se i te ot en m prvku B7 o cel z vity s jeho ustaven m do polohy dle obr zku 11 18 Po se zen zajist te prvek 37 matic a pojistnou podlo kou g Dr hu va ky nama te doporu en m plastick m mazivem Strana 11 29 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Range for reverse 0 1 0 3 mm Element 37 Figure 11 18 Adjustment of axial clearance of blocking valve IT IS FORBIDDEN TO MOVE PROPELLER CONDITION LEVER FROM MAXIMUM RPM POSITION INTO FEATHER WHEN ENGINE CONDITION LEVER IS IN REVERSE POSITION e Press fully the blocking valve with hand and measure clearance in between the cam and setting element B7 on the lever BI with feeler gauge Specified clearance is 0 1 0 3 mm 0 004 0 012 inch figure 11 18 f Ifthe clearance is not correct adjust it Loose the nut on element 37 Hold the Ed with a screwdriver Adjust the axial clearance by turning element 37 and set it into position according to figure 11 18 After adjustment secure the elem
206. itoly Mont krytu vrtule v t to p ru ce Prove te z znam o proveden prohl dce do z znamn ku vrtule C 900 HODINOV DVOULET PROHL DKA POZN MKA Podrobn prohl dka se prov d po ka d ch 900 hodin ch provozu nejpozd ji v ak po 24 kalend n ch m s c ch Pro mo nost efektivn ho pl nov n prohl dky se m e p edepsan hodinov interval pohybovat v rozmez 30 letov ch hodin UPOZORN N 900 hodinov prohl dka zahrnuje 300 hodinovou prohl dku 1 Sejm te p edn kryt vrtule 2 Odpojte kabely elektrick ho odmrazov n je li instalov no POZN MKA P ed vyjmut m list z pouzder ov te dostate nou viditelnost pozi n ch rysek na listu a pouzdru V p pad pot eby rysky obnovte ostrou jehlou 3 Odstra te z vla ky povolte rouby obj mek a vy roubujte listy z pouzder 4 D kladn zkontrolujte z vity list a vnit n z vity pouzder listu na v skyt koroze Pro dal provoz se p ipou t a Velmi mal stopy povrchov koroze v z vitu vrtulov ho listu UPOZORN N P padn stopy koroze v z vitu listu neodstra ujte Z dnym piln kem brouskem ani jin m n strojem Pou ijte pouze istou ut rku pro o ist n povrchu Strana 6 3 6 12 2011 PROHEIDISY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 4 Check the blades for play or movement per Loose blades in this chapter 5 Check de icing components if installed
207. jte dle instrukc v robce p pravku 3 Aplikujte vrchn n t r Schv len barvy ve spreji jsou uvedeny n e Tempo A 150 Epoxy Black Tempo A 151 Epoxy Gray Tempo A 152 Epoxy White UPOZORN N mer m OPRAVA LISTU M E ZM NIT VYV EN VRTULE CO MU E V ST K NADM RN M VIBRAC M VRTULE V PROVOZU V TAKOV M P PAD JE NEZBYTN PROV ST DYNAMICK VYV EN VRTULE POSTUPUJTE DLE ODD LU DYNAMICK VYV EN V T TO KAPITOLE E V M NA LISTU V PROVOZU 1 Vyjm te list z vrtulov hlavy 2 Nainstalujte do n boje nov list dle postupu v kapitole Mont n a provozn instrukce v t to p ru ce 3 Listy pro ka dou vrtuli jsou p esn sesadov ny Pozd j v m na jednoho nebo v ce list v provozu a nastaven nov ho listu do stejn pozice jako byl p vodn list m e zp sobit hlovou odchylku list v sad vedouc k aerodynamick mu rozv en Pro zaji t n shodn ho nastaven v ech list postupujte n sledovn a Praporovac m erpadlem p estavte vrtuli na mal hel Pokud praporovac erpadlo nen instalov no nastartujte motor a zastavte ho s vrtul na mal m hlu b Pomoc hlom ru zm te hel v ech list na rysce kontroln ho ezu Ryska kontroln ho ezu je erven ra na tlakov stran listu 1 Oto te vrtuli tak aby jeden z list byl rovnob n se zem Zm te hel listu a poznamenejte si ho Strana 7 10 7 7 2015 ds
208. justed Total clearance between the beta ring and carbon blocks is at least 0 15 0 18 mm 0 006 0 007 inch for the new assembly figure 11 16 Maximum clearance permitted is 0 4 mm Measure this clearance using following procedure press the carbon block assembly to one side of the beta ring and use feeler gauge to measure the total clearance After adjustment and clearance measurement tighten both nuts of the rod 32 figure 11 24 left and right thread and secure with recommended lock wire Page 11 37 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER UPOZORN N V robce vrtule nedovoluje nastaven minim ln ho letov ho hlu na jin hodnoty ne jsou uveden v tabulk ch 11 2 a 11 3 Obr zek 11 24 T hlo 32 se zen a zaji t n 2 Se zen mikrosp na e signalizace BET A p sma Prov d se po mont i regul toru ot ek vrtule po mont i motoru a Zapn te nap jen signalizace v kabin letounu POZN MKA B hem se izov n si zajist te pomocn ka pro sledov n v kabin letounu b Se izovac roub 38 na p ce kter ovl d mikrosp na se i te tak aby mikrosp na signalizace BETA p sma sepnul v poloze kluzn ho epu 0 8 mm 0 0315 inch nad patn plochou va ky obr zek 11 20 Toto se zen zaru uje spr vn sepnut mikrosp na e p i n b hu kluzn ho epu na vrcholovou plochu va ky UPOZORN N
209. k Nosi kluzn ch i kamen All B Obr zek 11 13 Regul tor LUN7815 03 Pohled sm rem od motoru 6 S p kou Rn na dorazu maxim ln ch ot ek 15 p ekontrolujte chod p ky Bc ze z kladn polohy do reverzn polohy kdy ryska na p ce se kryje s ryskou reverzu na stupnici regul toru Pot p estavte p ku Bc d le a na bezpe nostn doraz UPOZORN N Chod p ky Bc nesm b t tuh 7 Kontrolujte nosi kluzn ch kamen obr zek 11 6 na po kozen a kompletnost 8 epy nosi e kluzn ch kamen nama te vazel nou V STRAHA VADN NOSI KLUZNYCH KAMEN VYRADTE Z PROVOZU 9 Pohybem p ky Zv ve sm ru ipky obr zek 11 13 se p esv d te poslechem o sepnut mikrosp na e V obr zek 11 12 Strana 11 21 13 4 2010 SYSTEM OVL DAN VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Lever Be BETA ring 9 assembly Figure 11 13 Governor LUN7816 View from engine 6 With lever Rn at maximum RPM stop 15 verify lever Bc travel from basic position up to reverse when the guideline on the lever with cam is against reverse range on the governor scale Then move the lever Bc further to safety stop CAUTION Lever Bc travel should be free 7 Verify the carbon block assembly figure 11 6 for damage and completeness 8 Grease carbon block assembly pins WARNING REMOVE DAMAGED ASSEMBLY FROM OP
210. ktoru Mo n p ina a Nedota en upev uj c rouby b Vadn t sn n na p rub regul toru N prava a Dot hn te upev uj c rouby b Vym te t sn n Strana 11 61 13 4 2010 SYST M OVL D N VRTULE E 1500 11 9 TROUBLESHOOTING Trouble Relief valve leakage after pressure adjustment Probably cause a Defective sealing b Loosen valve Remegy a See section Maintenance practices b See section Maintenance practices Trouble Non return valve with fitting leakage Probably cause a Defective sealing Remegy a See section Maintenance practices Trouble Coaxial valves leakage at feedback body Probably cause a Defective sealing Remegy a Replace the governor Trouble Leakage between governor and gear box flange Probably cause 8 Loosen mounting bolts b Defective sealing between the flanges Remegy a Tighten mounting bolts b Replace the sealing 61 10 00 PROPELLER CONTROL SYSTEM INSTALLATION AND OPERATION MANUAL Page 11 61 2010 04 13 AVIA PROPELLER Z vada Net snost na dut m roubu t lesa zp tn ho ventilu Mo n p ina a Vadn t sn c krou ky N prava a Vym te t sn n Z vada Zv t en p edepsan axi ln v le blokovac ho oup tka na zadn m v ku regul toru v poloze revers Mo n p ina a P i poloze ovl dac p ky vrtule na dorazu praporov polohy byla p estavena ovl
211. l system 1 Ovl dac p ku motoru nastavte na volnob n ot ky gener toru 1 Place the engine condition lever into idle position 2 Ovl dac p ku vrtule p estavte do polohy prapor ot ky vrtule se sn na 2 Move the propeller condition lever into feather position propeller RPM reduces to 350 ot min 350 rpm 3 S prodlevou 215 s vra te ovl dac p ku vrtule do polohy max ot ek a vy kejte 3 Move back the propeller condition lever after about 15 s delay to maximum RPM az ot cky vrtule dos hnou vychoz hodnoty position and wait to previous RPM Strana 11 48 KTN NI Page 11 48 6 2 2012 SYSTEM OVL D N VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER Strana 11 49 13 4 2010 4 Uveden cyklus 3x opakujte mezi cykly prodleva na volnob n ch ot k ch 40 s Kontrola volnob n ch ot ek vrtul jen u dvoumotorov ho letounu Ovl dac p ku motoru nastavte na doraz volnob hu Ovl dac p ku vrtule p estavte do polohy max ot ek Rozd l volnob n ch ot ek max 40 ot min V odli n m p pad prove te se zen podle t to kapitoly IWIN I Kontrola maxim ln ch ot ek vrtule Ovl dac p ka vrtule v poloze max ot ek Ovl dac p ku motoru p estavte do polohy max vzletov ho v konu Maxim ln ot ky na zemi maj b t 2080 120 ot min IWIN POZN MKA Uveden hodnota ot ek je informativn je z visl na v konu motoru a
212. letectv sportovn ch a akrobatick ch letounech T Jsme dr iteli licence pro v robu vrtulov ch list a kryt vyr b n sv tov zn mou americkou firmou Hamilton Standard LTd pro historick v le n letouny jako jsou P 51 Mustang T 6 Texan a dal D Na e v robky vysok kvality jsou certifikov ny v esk republice USA a mnoha dal ch zem ch Evropy Asie Austr lie St edn a Ji n Ameriky D Obchodn a servisn centra v USA Kanad Venezuele N mecku PRO V CE INFORMAC NAV TIVTE NA E WEBOV STR NKY www aviapropeller com E 1500 INSTALLATION AND OPERATION MANUAL Avia Propeller Ltd since 1919 Highly experienced engineering and manufacturing company Our specialization is in research and development manufacturing repairs overhauls service and sales of aircraft all metal variable pitch propellers and their parts Our R amp D team has long term experiences with aircraft propeller design One of the latest R amp D targets is to enlarge the new propeller AV product line lighter aluminium hub and blades Operations department is using up to date machinery incl devices accompanied with traditional craftsmanship of staff manufacturing products of the best quality D Quality department guarantees the highest quality level of the goods being delivered to our customers Our quality system fulfilled requirements of the European Aviati
213. linder and the fork The cylinder is mounted on the hub The piston in the cylinder is connected with the fork in the hub to do linear motion All blade bushings are coupled with the fork through Page 4 1 DESIGN AND OPERATION INFORMATION 2011 05 10 AVIA PROPELLER jsou spojena s un e em p es stav c kameny na epech na elech pouzder list P es stav c kameny je line rn pohyb p stu s un e em p ev d n na ot iv pohyb list Dvou inn servomechanismus je pln ovl d n tlakem oleje od regul toru vrtule v etn praporov n Tlakov olej pro innost vrtule je veden p es h del motoru a do prostoru mal ho a velk ho hlu vrtule je p iv d n kan ly ve vod c trubce N kter verze vrtul V508E V508E AG a v echny verze V510 jsou vybaveny sekund rn zar kou instalovanou uvnit vod c trubky Sekund rn zar ka zamezuje p estaven vrtulov ch list do mal ho hlu ne m n ne 8 v p pad poruchy zp tn vazby V echny zar ky jsou uvnit vrtule a nemohou b t m n ny dn nastaven nen nutn v echny hly jsou nastaveny p i mont i vrtule Pouze verze V508H Jedno inn stav c mechanismus se skl d z p stu p stnice v lce a un e e Tlakov olej od regul toru pro stav n list na mal hel je p iv d n do v lce kan lem v p stnici Tlakov olej p sob na p st um st n ve v lci P st je pevn spojen s un e e
214. listu tak aby pozi n ep byl uprost ed v ezu obr zek 5 4 Strana 5 5 20 10 2014 UPOZORN N U VERZE V508Z NEN OBJ MKA POLOHOV NA POZI N M EPEM P ED UTA EN M MUS B T OBJ MKA NASTAVENA TAK ABY RYSKA NA OBJ MCE BYLA PROTI RYSK M NA LISTU A POUZDRU OBR ZEK 5 5 POZI N EP OBJ MKY LISTU POUZE VRTULE V508Z Obr zek 5 4 Obr zek 5 5 Ut hn te obj mku listu Ustavte hlavu roubu obj mky do spr vn polohy obr zek 5 6 a dr te prsty jedn ruky a druhou rukou za roubujte matici nadoraz Pot za st l kontroly polohy hlavy roubu jednou rukou ut hn te matici momentov m kl em utahovac m momentem 65 70 Nm 48 52 Ib ft Po kone n m uta en ov te spr vnou polohu hlavy roubu UPOZORN N m NESPR VN UTA EN SROUBU OBJ MKY ZP SOB NEZ DOUC ZM NU NASTAVEN HLU LISTU VEDOUC AERODYNAMICK NEVYV ENOSTI VRTULE A NADM RN M VIBRAC M B HEM PROVOZU Po uta en utahovac m momentem ov te spr vnou polohu listu v pouzdru Ov te e konce ramen obj mky se vz jemn nedot kaj obr zek 5 7 a pojist te roub s matic dodanou z vla kou Pokud jsou otvory pro poji t n z vla kou po uta en na moment zakryty dot hn te matici na nejbli pozici umo uj c poji t n MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 6 Center the position pin in the slot of the
215. lte ho Povolte trubku u ovlada e LUN7880 a trubku od pomocn ho erpadla LUN7840 u p ep ky motoru b Na hrdlo se ipkou p ipojte trubku od ovlada e LUN7880 a lehce dot hn te UPOZORN N Sipka na zp tn m ventilu mus sm ovat vzh ru viz obr zek Trubky mus b t ist c Na hrdlo ozna en T s kuli kou 5 16 uvnit p ipojte trubku od pomocn ho erpadla LUN7840 a lehce dot hn te d Dot hn te dut roub postupn m dotahov n m matic a rouben na konc ch trubek UPOZORN N Dut roub se p i dotahov n nesm p it mohl by b t po kozen z vit v regul toru Strana 11 23 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 14 Use correct and clean packing Place the governor onto engine gear box Drive rod gearing must be correctly inserted into the gear box drive 15 Fix the governor using four bolts figure 11 7 using suitable wrench A spring washer is at bolt head and the second washer is inserted into governor flange recess with chamfer facing governor Secure at least three bolts using stainless steel lock wire figure 11 7 16 If the propeller is not in feather move it to feather by turning blades to move the beta ring that it seats at the propeller hub CAUTION CATCH THE BLADES AT ITS SHANK NEVER AT BLADE TIP NOTE It is recommended to move the lever Rn to feather stop 16 to facilitate servomechanism movem
216. m v prostoru n boje p es p stnici V echna pouzdra listu jsou spojena s un e em p es stav c kameny na epech na elech pouzder list P es stav c kameny je line rn pohyb p stu s un e em p ev d n na ot iv pohyb list Stav n list na velk hel zaji uje tla n pru ina um st n ve v lci a p sob c na p st proti tlakov mu oleji V echny krajn dorazy jsou uvnit vrtule a nemohou b t m n ny nicm n zm na minim ln ho letov ho hlu je mo n podle postupu v t to p ru ce Vrtulov listy Vrtulov listy jsou vyrobeny ze slitiny hlin ku Jsou za roubov ny do pouzder listu a zaji t ny sta en m obj mky Spojen se servomechanismem je provedeno p es stav c kameny instalovan na epech na elech pouzder list Z va Vrtule jsou vybaveny z va mi konstruovan mi jako sou st obj mek S la od z va pom h p estavovat vrtulov listy do velk ho hlu a dojde li k p eru en dod vky oleje od regul toru p estav vrtulov listy do praporov polohy Strana 4 2 10 5 2011 KONSTRUK N A PROVOZN INFORMACE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL the pitch change blocks installed on the pins on the blade bushing faces Pitch change blocks transfer the linear motion of the piston with the fork to rotary motion of the blades Dual acting system is fully controlled by using of oil pressure from propeller governor inclu
217. ment scale Strana 11 30 2 KTN NI Page 11 30 6 2 2012 SYSTEM OVL DAN VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 3 Se zen mikrosp na e signalizace BETA p sma plat pro regul tory LUN 7815 02 LUN7815 03 a Zapn te nap jen signalizace v kabin letounu POZN MKA B hem se izov n si zajist te pomocn ka pro sledov n v kabin letounu b Se izovac roub 38 na p ce kter ovl d mikrosp na se i te tak aby mikrosp na signalizace BETA p sma sepnul v poloze kluzn ho epu 0 8 mm 0 0315 inch nad patn plochou va ky 27 obr zek 11 20 Toto se zen zaru uje spr vn sepnut mikrosp na e p i n b hu kluzn ho epu na vrcholovou plochu va ky UPOZORN N V POLOZE KDY EP KLOU E NA VRCHOLOV PLO E VA KY P EZKOU EJTE LEHCE PRSTEM RUKY ZDA LZE JE T P KOU SE SERIZOVAC M SROUBEM B8 ZATLA IT VE SM RU IPKY TLA TKO MIKROSP NA E D LE DO MECHANICK HO DORAZU VOPA N M P PAD BY DO LO KPO KOZEN MIKROSP NA E SE IZOVAC ROUB 38 ZAJIST TE MATIC A B Zaji ovac Mikrosp na Va ka 27 eajstovaci roub 38 Z str ka Obr zek 11 20 Se zen mikrosp na e signalizace BETA A elektrick okruh vypnut B elektrick okruh zapnut Strana 11 31 6 2 2012 3 BETA range microswitch adjustment for governors LUN7815 02 LUN7815 03 a
218. miovan m vn j m povrchem Ulo en listu vrtule V508 se ot v lo isku se dv ma adami kuli ek Vn j lo iskov dr hy jsou sou st vrtulov ho n boje zat mco vnit n lo iskov dr hy jsou sou st pouzdra listu P edp t ulo en je nastaveno vymezovac m krou kem instalovan m pod obj mkou Ulo en listu vrtule V510 se ot v lo isku se dv ma adami kuli ek a jednou adou v le k Vn j lo iskov dr hy jsou sou st vn j ho krou ku nalisovan ho do n boje vnit n lo iskov dr hy jsou sou st pouzdra listu P edp t ulo en je nastaveno p edepsan m utahovac m momentem krou ku lo iska V echny modely krom V508 7 V508B a V508H jsou vybaveny omezova em ot ek vrtule na eln plo e v lce Pokud jsou skute n ot ky vy ne ot ky nastaven omezova p epou t olej z prostoru mal ho hlu ve vrtuli do odpadu dokud ot ky vrtule neklesnou na ot ky nastaven Stav c mechanismus list V echny verze mimo V508H Dvoj inn stav c mechanismus se skl d z p stu hydraulick ho v lce a un e e V lec je namontov n na n boji P st ve v lci je pevn spojen s un e em v prostoru n boje a spolu konaj line rn pohyb na st edov vod c trubce V echna pouzdra listu Strana 4 1 10 5 2011 KONSTRUK N A PROVOZN INFORMACE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 4 DESIGN AND OPERA
219. mm 0 425 0 004 inch Tabulka 11 2 Nastaven min letov ho hlu vrtul ady V508 s regul torem LUN7816 Table 11 2 Min flight pitch adjustment of propellers V508 Type Series with governor LUN7816 e Prvek 32 d lku t hla se i te tak aby v le mezi epem ovl dac p ky a p kou Sv e Adjust the element B2 rod length that the clearance between control lever pin and the odpov dala rozm ru Y V li kontrolujte listovymi m rkami lever Sv corresponds to the dimension Y Check the clearance with feeler gauge UPOZORN N CAUTION NEN DOVOLENO SNIMAT TAHLO PRVEK B2 KTERE JE NAMONTOVANO SHORTEN THE ROD ONLY INSTALLED ON THE GOVERNOR DO NOT REMOVE JEDNIM KONCEM NA SLEDOVACI PAKU A DRUHYM NA PAKU Zv THE ROD AT ANY END ana 11 36 11 36 6 2 2012 SYSTEM OVLADANI VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL PRO VRTULI V510 FOR PROPELLER V510 Constant Z Nc M a ngo a BeTA ampon pv Typ regul toru Typ p ky Sv Konstanta Z Nastaven n TE gt pro v po et rozm ru Y min letov ho hlu Letov hel p i rozsv cen BETA lampy T ro LUN7816 0 4 mm 0 016 inch 14 13 0 1 mm 0 512 0 004 inch LUN7816 01 0 3 mm 0 012 inch 13 13 0 1 mm 0 512 0 004 inch 0 9 mm 0 035 inch 12 14 0 2 mm 0 551 0 008 inch 1 6 mm 0 06
220. mont i vrtule po mont i regul toru ot ek vrtule po mont i motoru Se zen minim ln ho letov ho hlu se izovac m prvkem 32 regul toru ot ek po mont i na motor a p i v m n vrtule a P ed se izov n m kontrolujte 1 Beta krou ek je na dorazu vrtulov ho n boje vrtule v praporov poloze ID P ka Bc je na dorazu volnob hu obr zek 11 22 Ico Ryska na p ce se kryje s ryskou minim ln ho letov ho hlu na stupnici regul toru obr zek 11 23 POZN MKA Nen li vrtule v praporov poloze p estavte ji do t to polohy 3 gt LAM 17 MS nL O OR Doraz volnob hu Cep ovl dac p ky T hlo 32 Obr zek 11 22 Se zen rozm ru Y Strana 11 34 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL B Propeller Governor LUN7816 1 Governor adjustment with element 32 Perform when the propeller is installed the propeller governor is installed the engine is installed Adjustment of minimum flight pitch using the governor element 32 after installation on the engine and at propeller reinstallation a Verify before adjustment The beta ring seats at the hub the propeller blades are in feather position IN The lever Bc is at idle stop figure 11 22 Guideline on the lever aligns with mini
221. mum flight pitch guideline on the governor scale figure 11 23 Ico NOTE If the propeller is not in feather position feather it Figure 11 22 Dimension Y adjustment Page 11 34 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER K bw co 1 SR K a gt 7 gt Obr zek 11 23 Z kladn poloha p ky b Na obou konc ch t hla prvku B2 sejm te v zac dr t kter m jsou ji t ny kontramatice t hla s lev m a prav m z vitem Matice kl em lehce povolte c V atestu regul toru zjist te rozm r X na stran 5 horn tabulka d Krozm ru X p i t te podle zastav n verze regul toru konstantu Z tabulky 11 2 nebo 11 3 tak e kone n rozm r bude Y X Z mm UPOZORN N U regul tor LUN7816 a LUN7816 01 s p kou 1535 002 nesm b t hodnoty Y men ne 1 9 mm 0 075 inch POZN MKA S p kou Sv 1535 002 nen mo n nastaven minim ln ho letov ho hlu v cel m rozsahu hl dle tabulek 11 2 a 11 3 proto e hodnota Y nesm b t men ne 1 9 mm 0 075 inch Z toho d vodu je mo n prov st v m nu p ky Sv 1535 002 za p ku 4 ROW1 0101 01 V m nu m e prov st pouze pracovn k opr vn n v robcem vrtule motoru nebo regul toru Po vym n mus b t na identifika n t tek uveden nov verze regul toru LUN7816 02 UPOZORN N Po v m n p ky Sv mus b t provedeno se
222. nt is described in the following section Page 11 63 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Po zastaven motoru demontovat hadici s manometrem a namontovat zp t matici 59 After engine stop remove the hose and reinstall the nut 59 with the ball 60 and secure If S kuli kou 60 a pojistit Regul tor v p pad pot eby ot t ist m hadrem necessary clean the governor Obr zek 11 34 P ipojen manometru Figure 11 34 Manometer connection Ot ky vrtule Tlak MPa Propeller rpm Pressure MPa 2080 2 30 2 45 2080 2 30 2 45 2060 2 28 2 43 2060 2 28 2 43 2040 2 27 2 42 2040 2 27 2 42 2020 2 25 2 40 2020 2 25 2 40 2000 2 23 2 38 2000 2 23 2 38 Tabulka 11 6 Nastaven tlaku pro LUN7815 02 Table 11 6 Pressure for LUN7815 02 3 Se zen max tlaku regul toru prvkem 73 a 76 reduk n ho ventilu obr zek 11 35 3 Pressure adjustment using element 73 and 76 of the relief valve figure 11 35 V p pad zji t n ho nespr vn ho se zen tlaku pod reduk n m ventilem se reduk n In the case that the pressure adjustment of the relief valve was found to be incorrect ventil se izuje n sleduj c m zp sobem adjust it following way Strana 11 64 2 11 64 13 4 2010 SYSTEM OVLADANI VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER POZN MKA U
223. nto postup s ostatn mi c Rotate the propeller manually in the direction of normal rotation and repeat this pi kami list procedure with another blade tips d Nakreslen rysky pi ek v ech list od sebe nesm b t vzd leny v ce ne 3 mm d The marked lines of all blade tips should be separated by not more than 3 mm 0 12 inch 0 12 inch UPOZORN N CAUTION Rozd l v t ne 3 mm 0 12 inch m e b t zn mkou ohnut ch list nebo po kozen Difference greater than 3 mm 0 12 inch may be an indication of bent blades or servomechanismu uvnit vrtule V p pad zji t n probl mu s dr hou list damage of propeller servo inside the hub Indicated blade track problem should be kontaktujte Avia Propeller referred to Avia Propeller Obr zek 6 4 Kontrola dr hy list Figure 6 4 Blade track check 5 Elektrick odmrazovac syst m 5 Electric de icing system a Zkontrolujte sb rac kruh na nadm rn opot eben a po kozen Povrch m d n ch a Inspect the slip ring for excessive wear and damage Surface of copper rings must krou k mus b t hladk ist a such be smooth clean and dry b Zkontrolujte dota en v ech roubov ch spoj uchycen kabel k zadn mu b Check all screw connections for looseness attaching of cables to the spinner krytu a na obj mk ch list a p ipojen kabel ke kontakt m sb rac ho krou ku a bulkhead and to the blade clamps connection of cables to
224. o 2 76 inch 0 2 inch 0 395 inch from tip to 2 76 inch 0 2 inch 0 395 inch od 70 mm do 470 mm 2 2 6mm 9 mm 70 mm to 470 mm 2 2 6 mm 9 mm od 2 76 inch do 18 5 inch 0 24 inch 0 35 inch 2 76 inch to 18 5 inch 0 24 inch 0 35 inch od 470 mm do 770 mm 4 4 3mm 5mm 470 mm to 770 mm 1 1 3 mm o mm od 18 5 inch do 30 3 inch 0 12 inch 0 2 inch 18 5 inch to 30 3 inch 0 12 inch 0 2 inch od 770 mm do konce profilu 0 1 1 5 mm 770 mm to airfoil end 0 4 1 5 mm od 30 3 inch do konce profilu 0 06 inch 30 3 inch to airfoil end 0 06 inch Tabulka 7 1 P pustn m stn opravy na n b n a odtokov hran listu V508 Table 7 1 Local repair allowable limits on the leading and trailing edge of V508 blade Strana 7 7 IRADI Page 7 7 28 2 2012 UDRZBA 61 10 00 MAINTENANCE 2012 02 28 AVIA PROPELLER b List vrtule V510 P pustn hloubka po et a poloha m stn ch oprav je uvedena na obr zku 7 5 av tabulce 7 2 Z en ky max 1 mm 0 04 inch na n b n hran max 2 mm 0 08 inch na odtokov hran Obr zek 7 5 Oblasti listu V510 souvisej c s tabulkou 7 2 INSTALLATION AND OPERATION MANUAL b V510 propeller blade Refer to tigure 7 5 and table 7 2 for allowable depth number and location of the local repairs Reduction in width max 1 mm 0 04 inch for leading edge max 1 5 mm 0 06 inch for trailing edge
225. oma in inch dimension changed to dot Pages 6 10 to 6 16 Section Blade repair transferred to chapter 7 Other sections moved above Page 7 4 to 7 9 Blade repair procedures transferred from chapter 6 and updated Page 8 1 to 8 8 Chapter Troubleshooting was updated Page 9 1 Chapter Shipping and storage was updated Pages 10 1 10 2 Added list of special tool transferred from Service letter SL 5 Page 11 1 Newly blank table of content of chapter 11 was transferred to main table of content Page 11 2 Section General was updated Inch and fahrenheit equivalents added to millimeter and celsius units throughout chapter 11 Strana 11 3 6 2 2012 SEZNAM ZM N 61 10 00 LIST OF REVISIONS Page 18 2012 02 06 AVIA PROPELLER C slo zm ny Datum vyd n SEZNAM ZM N Zm n n strany E 1500 Stru n popis Rev No Issue Date INSTALLATION AND OPERATION MANUAL LIST OF REVISIONS Revised Page Short Description R 31 12 28 nora 2012 R 221 13 5 prosince 2013 R 8 14 Strana 11 4 17 1 2014 17 ledna 2014 11 4 111 1 5 5 5 6 5 16 7 5 7 7 11 4 111 1 4 3 11 4 111 1 2 1 3 2 4 4 4 6 4 8 4 10 5 1 5 2 5 8 5 9 5 11 5 11 1 5 12 6 10 7 6 7 9 7 10 10 3 SEZNAM ZM N Strana 5 5 Cesky popis u obr zk 5 6 a 5 7 v prav m sloupci zm n n na anglick Strana 5 6 Odkaz na obr zek 5 9 v bodu 7 v prav m sloupci opr
226. on Safety Agency EASA D Our commercial department co operate with customers from about 50 countries of the world We consider each and every customer to be of great importance for us Our products and activities All metal aircraft propellers for piston and turboprop engines up to 1200 HP used on regional airline airplanes agricultural general aviation sport and aerobatic airplanes D Licensed blade and spinner manufacturing for propellers made by world famous U S company Hamilton Standard Ltd for Warbirds like the P 51 Mustang T 6 Texan etc 5 High quality products certified the Czech Republic USA and many European Asian Australian Central and South American countries 5 Sales and Service Centers the USA Canada Venezuela Germany FOR MORE INFORMATION VISIT OUR WEBSITE www aviapropeller com
227. oru ot ek ani paliva prove te se zen drakov ho ovl d n dle provozn p ru ky letounu N sledn znovu kontrolujte dorazov polohy volnob h a max reverz SYST M OVL D N VRTULE E 1500 d INSTALLATION AND OPERATION MANUAL Connect linkage to the lever Bc such way that lever position stop will not be changed and verify fuel control unit setting according to the engine operational manual Move with assistant engine power lever at engine disconnected from linkage to full reverse position and check 1 Guideline on the governor lever should align with maximum reverse guideline figure 11 26B at the governor scale IN Movement limitation on the fuel control unit must be ensured on the main control lever verify with feeler gauge 0 05 mm 0 002 inch at compression Setting should correspond with engine operational manual If the guidelines of the lever and on the scale are not aligned adjust according to the engine operational manual NOTE Verify final adjustment with multiple setting from idle to maximum reverse position and recheck stops 9 61 10 00 Minimum flight Guideline for reverse ZA Figure 11 26 Maximum reverse output adjustment setting on scale Reinstall engine linkage after the adjustment Move slowly engine control lever from idle to maximum reverse power position check the stops on the fuel control unit and the propeller governor If it
228. ose it and remove the cover 72 NOTE The relief valve spring is pressed be careful at removing the cover Figure 11 35 Relief valve In the case that pressure will be adjusted with adding removing shims element 73 under the spring 75 inside the relief valve then adding removing shims will increase decrease the pressure Shim thickness 1 mm 0 04 inch means pressure change 0 07 MPa for governor series LUN 7815 and 0 10 MPa for governor series LUN 7816 WARNING TOTAL THICKNESS OF ALL SHIMS SHALL BE MAXIMUM 4 mm 0 16 inch THE PIN 74 MUST REMAIN IN THE SPRING 75 Page 11 65 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER POZN MKA K se izov n pou vejte p edepsan podlo ky o tlou ce 1 a 1 5 mm 0 04 and 0 06 inch V p pad Ze budete tlak se izovat t sn c mi podlo kami prvek 76 pod v kem 72 pak p id n m odebr n m podlo ky se tlak sn zv Tlou ka podlo ky 1 mm 0 04 inch znamen zm nu tlaku jako u prvku 73 viz v e POZN MKA Pou vejte podlo ek t chto p edepsan ch tlou t k 1 mm 1 5 mm a 2 mm 0 04 0 06 a 0 08 inch Pod v kem jsou povoleny maxim ln dv podlo ky V ko 72 p i stla en pru iny s op rkou lehce ru n na roubujte na t leso reduk n ho ventilu 71 Pak t leso 71 pridr te kl em a dot hn te kl em v ko 72 UPOZORN N T LESO REDUK N HO VENTILU NESM TE P LI DOTAHOVAT DO T LESA
229. ot exceed one half of the blade width in the place of repair Diameter of repaired area must be 30 times greater than its depth Page 7 5 MAINTENANCE di 0107 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL c Postup opravy c Repair procedure 1 Pou ijte malou ru n rota n brusku s brusn m kotou kem nebo smirkovy 1 Use a small hand held rotary grinder with grinding wheel or 80 grit pap r o hrubosti 80 Odstra te po kozen z povrchu listu tak jak je sandpaper to remove damage from blade surface as displayed in figure zn zorn no na obr zku 7 3 7 3 2 10X zv t ovac lupou se ujist te e po kozen je pln odstran no 2 Use 10X magnifying glass to verify that the damage was totally removed Polish the repaired area with red ScotchBrite or 280 grit sandpaper 0 P ele t te opravenou plochu erven m ScotchBrite nebo smirkov m pap rem o hrubosti 280 99 4 Paint the repair area Refer to Painting After Repair in this chapter 14 Provedte opraven plochy dle postupu v t to kapitole REPAIR du Pos up Ne d DEPTH OF REPAIR TRICETIN SOBEK HLOUBKY Pad K THIRTY TIMES THE DEPTH OPRAVY EA OF REPAIR PO KOZEN POVRCHU 9 0 4 TUE ANY SURFACE DAMAGE Ag Ld X Obr zek 7 3 M stn oprava povrchu listu Figure 7 3 Blade surface local repair Page 7 6 Strana 7 6 gt UDRZBA 61 10 00 MAINTENANCE 2014 01 17 17 1 2014 AVIA PROPELLER
230. otoru dle Letov p ru ky P kou ovl d n motoru nastavte ot ky p ibli n 17000t min P ka ovl d n vrtule je nastavena na maxim ln ot ky Sni te ot ky vrtule p kou ovl d n vrtule o 200 a 4000t min Vra te p ku ovl d n vrtule do polohy maxim ln ch ot ek a pozorujte vzestup ot ek kter by se m ly ust lit na p vodn hodnot Opakujte tento postup min t ikr t pro odvzdu n n hydraulick ho syst mu a pro dod vku oh t ho oleje do v lce Zvy te ot ky p id n m v konu na p ibli n 19500t min P kou ovl d n vrtule sni te ot ky vrtule asi o 1000t min a zvy te v kon motoru o p ibli n 5 10 ot ek gener toru Pozorujte funkci regul toru ot ky by se m ly ust lit na sn en rovni Ov te funkci vrtule v cel m rozsahu od reverzu do praporu Postupujte dle instrukc pro motorovou zkou ku uveden v Letov p ru ce Strana 5 13 6 2 2012 MONT N A PROVOZN INSTRUKCE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Refer to section Propeller control system in this manual for complete information on basic adjustment for installations with governor Jihostroj LUN7815 and LUN7816 This section provides further information on additional adjustment testing and troubleshooting of the propeller governing system For propeller control system with Avia governor refer to Avia Operation and Installation Manual E 1707 For propeller
231. ouby kter mi se prov d lo se izov n pojist te poji ovac m lakem Strana 11 32 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL NOTE Switching on off of the electric circuit by the microswitch V should be tested either by the lever Zv after removing the carrier of the slide blocks or with help of two mechanics by manual adjustment of the propeller blades Set the propeller control lever in the cockpit to position feather carbon block assembly on the lever Zv is connected CAUTION HOLD BLADES NEAR BLADE SHANK NEVER AT BLADE TIP c Make sure that during the reverse motion to the initial position after breaking the electric circuit the top of the journal is spaced from the base position minimum 0 1 mm 0 004 inch If this clearance is less adjust it by adjusting element figure 11 20 and this screw is then locked by tightening the nut d Adjust when the electric circuit is energized based on the beta ring position using following procedure 1 Setthe cockpit propeller condition lever into feather position protrude beta ring by turning propeller blades by hand to position 9 5 9 mm 0 37 0 374 inch and fix this position using the appropriate means Moment when the electric circuit is energized shall be adjusted only by turning the cam 27 figure 11 20 ID CAUTION TWO WASHERS ARE PLACED UNDER THE SECURING SCREW ONE OF THEM IS SPRING
232. output adjustment BETA range microswitch adjustment Page 5 12 INSTALLATION AND OPERATION INSTRUCTION 2014 09 18 AVIA PROPELLER Kompletn informace o z kladn m nastaven pro instalace s regul tory Jihostroj LUN 7815 a LUN7816 jsou uvedeny v kapitole Syst m ovl d n vrtule Tato kapitola obsahuje dal informace pro roz en se izov n zkou en a vyhled v n z vad ovl dac ho syst mu vrtule Informace o ovl d n vrtule s regul torem Avia jsou uvedeny v Provozn a mont n p ru ce Avia E 1707 Informace o ovl d n nastaven a dal informace o instalac ch s regul tory jin ch v robc jsou uvedeny v p ru ce v robce motoru I ZKOU EN V robce motoru a vrtule nedoporu uj zbyte n pou vat vysok ot ky motoru b hem pozemn zkou ky P ed zkou kou ukli te plochu aby nedo lo k po kozen list a odmrazovac ch t les nap klad z seky od kam nk Kontrola funkce odmrazovac ho syst mu Pozemn zkou ka vrtule s elektrick m odmrazov n m mus b t prov d na v dy s instalovan m p edn m krytem vrtule jinak dojde k po kozen spojovac ch kabel Doba trv n zkou ky zapnut ho odmrazovac ho syst mu p i b hu vrtule nen omezena P i zastaven m motoru je trv n zkou ky omezeno pouze na 2 cykly jinak dojde k p eh t odmrazovac ch t les Pozemn zkou ka Kontrola funkce vrtule Prove te spu t n a proh t m
233. overnor flange using packing and appropriate cap 11 Reinstall the carbon block assembly onto the lever Zv 12 Cover governor fittings with appropriate caps 13 Clean the governor preserve it and place into a suitable box 11 6 BASIC ADJUSTMENT AFTER INSTALLATION ON ENGINE CAUTION ALL REMOVAL INSTALLATION AND REPAIR WORKS PUBLISHED IN THIS MANUAL MUST BE PERFORMED BY PERSONNEL WITH APPROPRIATE QUALIFICATION A Propeller Governor LUN 7815 1 Governor adjustment with element 32 for governors LUN7815 02 LUN7815 03 NOTE Perform this adjustment with propeller installed NOTE For basic adjustment of minimum flight angle of propeller V508 with governor LUN7815 refer to table 11 1 a Check whether the propeller is in feather position and the beta ring is not protruded and it seats at propeller hub b If the propeller is not in feather position move it to feather position by turning the blades to seat the beta ring on the propeller hub WARNING CATCH THE BLADES AT ITS SHANK NEVER AT BLADE TIP Page 11 25 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER C obou konc ch prvku 332 sejm te v zac dr t kter m jsou zaji t ny ob matice lev a prav k t hlu a lehce je kl em povolte POZN MKA Lev z vit je ozna en na t hlu p smenem L d Povyt hn te vrtuli ru n za ko enovou partii list sm rem od motoru aby se vymezila axi ln v le v lo
234. p ky vrtule v kabin tak aby mezi n m a ovl dac p kou vrtule byla v le 2 3 mm 0 08 0 12 inch Doraz 15 zajist te dota en m matice a doporu en m v zac m dr tem s plombou Ov en se zen maxim ln ch ot ek prove te v n sleduj c m letu Se zen a zji t n hodnoty ot ek zapi te do atestu regul toru SYST M OVL D N VRTULE E 1500 INSTALLATION AND OPERATION MANUAL 11 8 FURTHER ADJUSTMENT A 1 61 10 00 Propeller Governor LUN7815 Maximum RPM adjustment for governors LUN7815 02 LUN7815 03 To be performed after control flight Move propeller control lever in cockpit such way that governor lever Rn is not touching maximum RPM stop Loose stop 153 figure 11 29 Loose the nut and adjust max RPM by turning the stop screw 15 Screw in decreasing of RPM Screw out increasing of RPM One turn 360 of the stop screw change the RPM approx about 20 RPM NOTE For max controlled propeller RPM refer to table 11 4 Move propeller control lever to maximum RPM position governor lever Rn must be touching the stop 15 If clearance is found adjust propeller control lever stop in the cockpit to distance 2 3 mm 0 08 0 12 inch from propeller control lever Secure the stop 15 by nut tightening and using lock wire Verify this adjustment at next flight Make a record in the logbook
235. p and connect cable to de icer Install the sheet metal holder with rubber insert and attach all parts with fixing screws to the clamp Insert the spacer between the clamp and holder prior to attachment Fixing screws are different in length use shorter screw with spacer Safety the screws with stainless steel wire 0 8 mm 0 032 inch 1 Om 1 l mm W SV S IN Z e L older Insert Figure 5 12 De icing type BI De icing system type B2 Connect the cable to the de icer with screws and toothed washers Safety the screws with paint De icing system type B Connect the cable to the de icer with screws and toothed washers Safety the screws with paint NOTE From September 2010 the same components as for de icing type C may be altenatively used In this case refer to mounting procedure on the next page Page 5 10 INSTALLATION AND OPERATION INSTRUCTION 2012 02 06 AVIA PROPELLER Odmrazovac syst m typ C obr zek 5 13 Um st te spodn d l svorkovnice na obj mku tak aby otvory ve svorkovnici a obj mce byly proti sob a p ipojte kabel k odmrazovac mu t lesu Prilo te vrchn d l svorkovnice a plechov dr k a p ipevn te v echny komponenty pomoc roub s podlo kami k obj mce Pojist te rouby nerezov m dr tem 0 8 mm 0 032 inch
236. pou ijte novou z vla ku h Kontrolujte se zen sdru en vazby ovl dac p ku motoru p esu te na doraz epu t hla Sv 65 v kulise Sv ryska na p ce s va kou se m kr t s ryskou Sv na stupnici regul toru obr zek 11 27C Povolen odchylka 0 5 mm 0 04 inch i Kontrolujte v li mezi epem sledovac p ky a zar kou dle postupu v kapitole 11 6 j Kontrolujte v li mezi blokovac m a hlavn m oup tkem dle postupu v kapitole 11 6 k Kontrolujte v li mezi beta krou kem a kameny nosi e dle postupu v kapitole 11 6 Strana 11 43 13 4 2010 SYSTEM OVL DAN VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Range for reverse Figure 11 27 Governor LUN7815 02 Basic adjustment check f Place the engine condition lever into maximum reverse position guideline on the cam lever must be aligned with BETA range on the governor scale figure 11 27B If not adjust according to the engine operational manual g Connectthe rod Sv 65 screw the nut and secure with cotter pin WARNING Use new cotter pin each installation h Check adjustment of the coupled connection move the engine condition lever to touch rod Sv 65 pin in the gate Sv the guideline on the cam lever should align with Sv guideline on the governor scale figure 11 27C Max difference is 0 5 mm 0 04 inch i Check clearance between tracking lever pin and stop acc to
237. ppropriately certificated maintenance entity Refer to section Maintenance in this manual 2 Inspect the blades and spinner for the traces of lightning strike Refer to Lightning strike in this chapter if lightning strike is confirmed or suspected NOTE Lightning strike can be indicated as discolored area inside the painted surface signs of burning or melting chipped or missing material in the place of lightning strike 3 Inspect the blades for evidence of oil leakage from the hub Perform inspection per Grease or oil leakage in this chapter to identify the source of leakage NOTE A new or newly overhauled propeller may leak slightly during the first several hours of operation This leakage may be caused by the seating of seals and o rings and the slinging of lubricants used during assembly Such leakage should cease within the first ten hours of operation 4 Models V510 only Manually by hand check the blades for the play in the retention bearing Any blade play except angle play is not acceptable If blade play is suspected inspect the blade play per Loose blades in this chapter where the blade play limits are stated Page 6 1 INSPECTIONS 2012 02 06 AVIA PROPELLER POZN MKA V le list u verz V508 je norm ln z d vodu odli n ho konstruk n ho e en ulo en listu 5 Ov te e v echny upev ovac a poji ovac prvky jsou uta en a dn nechyb 6 Zkontrolujte odmrazovac t lesa j
238. pushing appropriate cockpit button the feathering pump and feathering valve Now oil from the feathering is connected directly to the high pitch channel and propeller moves to feather This action is indicated by feathering lamp in the cockpit After engine restart and idle setting the propeller moves out from feather position Page 11 5 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 Kan l velk ho hlu nastaven list A Un e 2222222242 PZN une Ad k S AN za SSS V aa 7 M vzo Hop ZZ 1 A N Ah rh P st Op rn krou ek Y Kluzny k men P ka zp tn vazby Zv Obr zek 11 2 innost regul toru v re imu beta zen Strana 11 6 13 4 2010 SYST M OVL D N VRTULE 61 10 00 odpadu oleje INSTALLATION AND OPERATION MANUAL Kan l mal ho hlu nastaveni list Vstup tlakov ho olej P smo re imu ru n ho zen vrtule Reverzn poloha vrtule P ka ovl d n motoru v kabin letounu Koaxi ln oup tka Kan l K p ce ovl d n motoru Vnit n koax oup tko Page 11 6 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 LOW PITCH CHANNEL HIGH PITCH YOKE CHANNEL N Mah uc RNA SEE ETV V a X T AN N X B HN PISTON BETA RING D 0 COAXIAL VALVE CARBON BLOCK ASSY FEEDBACK LEVER o INSTALLATION AND OPERATION MANUAL PRESSURIZED O
239. r cover was specified no torque required Chapter Airworthiness limitations was updated Model V508H was added chapters 3 4 5 6 was updated Information on start of calendar TBO was updated Chapter Airworthiness limitations was updated Added reference to Service Bulletin No 1 Page 6 2 6 3 Added tolerance of required hour interval of inspection Page 6 15 Added note that in case of overspeed overtorque event the report Page 11 1 2011 12 06 AVIA PROPELLER SEZNAM ZM N C slo zm ny Datum vyd n Zm n n strany E 1500 Stru n popis Rev No Issue Date INSTALLATION AND OPERATION MANUAL LIST OF REVISIONS Revised Page Short Description R 137 11 pokra 6 nora 2012 11 71 Strana 11 2 6 2 2012 1 2 a 1 4 11 2 a 11 4 1 1 1 1 2 2 1 a 2 3 4 3 a 4 11 5 2 a 5 4 5 6 5 10 5 11 9 13 9 14 5 17 6 1 6 2 6 4 6 7 6 9 a 6 16 7 4 a 7 9 8 1 a 8 8 9 1 10 1 10 2 11 1 11 2 11 27 11 29 a 11 32 11 35 a 11 39 11 41 11 45 11 46 11 48 11 56 11 57 11 60 11 63 11 65 a 11 67 SEZNAM ZM N momentu mus b t vypln n protokol Strana 6 17 Dopln no e kontakt vrtule s ciz m objektem znamen gener ln opravu Strana 6 18 Dopln ny informace pro p pady vystaven vrtule ohni a kontaminaci motorov ho oleje Strany 6 19 6 20 P id ny protokoly pro p pad p eto en vrtule a p ekro en krout
240. r vnost instalace vrtule na motor viz kapitola Mont n a provozn instrukce e Vrtule mus b t znovu staticky vyv ena f Vrtule mus b t znovu dynamicky vyv ena B PRAPOROV N Z vada Po inicializaci automatick ho praporov n se vrtule nezapraporovala Mo n p ina a Vadn hydraulick obvod nap LUN7880 praporovac erpadlo apod b Vadn elektrick instalace c N zk pracovn tlak N prava a Vadn prvek hydraulick ho obvodu vym te Postupujte dle instrukc v robce letounu b Postupujte dle instrukc v robce letounu c Zkontrolujte tlak v syst mu Postupujte dle v robce motoru Strana 8 5 6 2 2012 ODSTRANOV N Z VAD E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Trouble Vibration Probably cause a Blades are set to different angles b Loose blade bearing Cracks at spinner dome surface Incorrect propeller installation Incorrect static balance Incorrect dynamic balance Remedy a Check the correct installation of the blades in the bushings see section Installation and operation instruction b If loose blade bearing the propeller must be removed from service and be sended to manufacturer or authorized repair centre C Check the spinner dome for cracks occurrence d Check the correct installation of the propeller on the engine see section Installation and operation instruction e Propeller m
241. r exchange in full extent 61 10 00 Page 11 44 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Strana 11 45 6 2 2012 Po v m n ostatn ch p stroj vrtulov ho syst mu prove te v rozsahu nezbytn m pro ov en funkce dan ho p stroje Spus te motor podle Letov p ru ky letounu Proh ejte motor na teplotu vstupn ho oleje 60 65 140 150 F Odvzdu n te vrtulov syst m Ovl dac p ku motoru nastavte na volnob n ot ky gener toru Ovl dac p ku vrtule p estavte do polohy prapor ot ky vrtule se sn na 350 ot min S prodlevou 15 s vra te ovl dac p ku vrtule do polohy max ot ek a vy kejte a ot ky vrtule dos hnou v choz hodnoty Uveden cyklus 3x opakujte mezi cykly prodleva na volnob n ch ot k ch 40 s IN 1 Ico Kontrola volnob n ch ot ek vrtul jen u dvoumotorov ho letounu Ovl dac p ku motoru nastavte na doraz volnob hu Ovl dac p ku vrtule p estavte do polohy max ot ek Rozd l volnob n ch ot ek max 40 ot min Jsou li vy postupujte dle kapitoly Odstra ov n z vad v tomto manu lu IW IN Kontrola maxim ln ch ot ek vrtule Ovl dac p ka vrtule v poloze max ot ek Ovl dac p ku motoru p estavte do polohy max vzletov ho v konu Maxim ln ot ky na zemi maj b t 2080 120 ot min IWINI POZN MKA Uveden hodnota ot ek je informativn je z
242. r possibility of flexible inspection schedule the required hour interval may vary plus minus 30 flight hours 1 Remove the spinner dome and visually inspect the entire blades spinner and visible hub components for nicks gouges erosion cracks corrosion Refer to section Maintenance in this manual for blade repair procedures Damage of other propeller part should be referred to Avia Propeller 2 Inspect the blades and spinner for the traces of lightning strike Refer to Lightning strike in this chapter if lightning strike is confirmed or suspected NOTE Lightning strike can be indicated as discolored area inside the painted surface signs of burning or melting chipped or missing material in the place of lightning strike 3 Inspect visible propeller parts for evidence of oil leakage from the hub Perform inspection per Grease or oil leakage in this chapter to identify the source of leakage Page 6 2 INSPECTIONS 2012 02 06 AVIA PROPELLER 4 Zkontrolujte v le list dle odd lu V le listu v t to kapitole 5 Zkontrolujte komponenty odmrazovac ho syst mu je li pou it dle odd lu Elektrick odmrazovac syst m v t to kapitole O Zkontrolujte poji t n p rubov ch roub Pokud je poji ovac dr t uvoln n p eru en nebo pokud chyb ov te uta en roub p edepsan m momentem pojist te dr tem dle kapitoly Mont na motor v t to p ru ce a Instalujte kryt dle kap
243. r s listy nastaven mi na minim ln letov hel Zkontrolujte dr hu list n sleduj c m zp sobem obr zek 6 4 a Za palkujte kola letounu b Um st te rovnou pevnou podlo ku s p ipevn n m listem pap ru pod pi ku nejni ho listu Tu kou nakreslete ru pod l cel ky pi ky listu Strana 6 8 30 6 2010 PROHLIDKY E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL CAUTION Any blade play except radial play is not acceptable for propeller model V510 lt FORE AND AFT PLAY V IN AND OUT PLAY END PLAY Figure 6 3 Blade play RADIAL PLAY b Blades with movement greater than allowable limits or that do not return to their original position when released may indicate internal wear or damage that should be referred to Avia Propeller 4 Blade track NOTE This inspection procedure only be performed if blade track problem is suspected as potential source of abnormal propeller operation e g vibration NOTE Shut down the engine with propeller in minimum flight angle Check the blade track as follows figure 6 4 a Chock the aircraft wheels securely b Place a flat fixed board with attached sheet of paper under the tip of the lower blade Use a pencil to draw a line along the full width of the blade tip Page 6 8 INSPECTIONS r 06 30 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL c Ru n ot ejte vrtul ve sm ru skute n rotace a opakujte te
244. ring that it seats at the propeller hub CAUTION CATCH THE BLADES AT ITS SHANK NEVER AT BLADE TIP NOTE It is recommended to move the lever Rn to feather stop ha to facilitate servomechanism movement 20 Install the carbon block assembly figure 11 6 onto the lever Zv and the beta ring Install the washer onto the pin and safety with cotter pin 1 6x10 NOTE Use new cotter pin each installation 21 If hydraulic valve LUN7880 and auxiliary pump LUN7840 are installed follow this LUN7840 postupujte n sledovn procedure Strana 11 13 TT Page 11 13 13 4 2010 SYSTEM OVLADANI VRTULE 61 10 00 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER E 1500 a Odjist te dut roub obr zek 11 8 a povolte ho Povolte trubku u ovlada e LUN7880 a trubku od pomocn ho erpadla LUN7840 u p ep ky motoru b Na hrdlo se ipkou p ipojte trubku od ovlada e LUN7880 a lehce dot hn te UPOZORN N Sipka na zp tn m ventilu mus sm ovat vzh ru viz obr zek Trubky mus b t ist c Na hrdlo ozna en T s kuli kou 5 16 uvnit p ipojte trubku od pomocn ho erpadla LUN7840 a lehce dot hn te d Dot hn te dut roub postupn m dotahov n m matic a rouben na konc ch trubek UPOZORN N Dut roub se p i dotahov n nesm p it mohl by b t po kozen z vit v regul toru e Ov te e je v uzav rac matici kuli ka 5 16 a matici dot hn te Cel spojen pojist te v
245. rnor models LUN7815 and LUN7816 if no other note applied 1 Cleaning DO NOT USE PRESSURE WASHING EQUIPMENT PRESSURE WASHING CAN FORCE WATER AND OR CLEANING SOLVENTS TO GOVERNOR WHICH CAN LEAD TO CORROSION OF INTERNAL COMPONENTS AND OR INCORRECT FUNCTION DO NOT USE AN CAUSTIC OR ACIDIC SOLUTIONS TO CLEAN ANY PROPELLER PART BEFORE USING OF SOME CLEANER OBSERVE THAT THE CLEANER HAS NOT ANY NEGATIVE EFFECTS FOR METAL SURFACES AND PAINTS MOVING PARTS AS THE PIN 52 SAFETY RINGS 81 CARBON BLOCK ASSEMBLY 22 ROD BEARINGS ETC MUST NOT BE DEGREASED DURING WASHING OR IT IS NECESSARY TO THEY BE RE LUBRICATED 2 Relief valve adjustment check see figure 11 34 NOTE For governor LUN7816 it concerns check of relief valve pressure for the valve No 1 RV Loose and unscrew the nut 59 with ball 60 from the turning screw 78 Connect measuring hose 114 with manometer to the turning screw 78 and place it such way that manometer sale is legible Fix the hose to don t touch hot parts Start the engine according to the flight manual and warm up oil to 60 65 140 150 F Place propeller control lever to maximum RPM position Move engine control lever to position where propeller speed is 1950 to 2080 rpm Read pressure Pressure for governor series LUN7816 should be in range 2 6 to 2 85 MPa if no other adjustment is used for appropriate application For the governor LUN7815 02 the pressures are in table 11 6 Pressure adjustme
246. rovided in millimeters abbreviated as mm with equivalent in inch units All temperature units in this manual are provided in Celsius grades abbreaviated as C with equivalent in Fahrenheit grades abbreviated as F The coma is used as decimal point for all metric units for all inch units the dot is used as decimal point Parts ordering Only original part is necessary to use if any is needs to replace due to its damage or loss Contact propeller manufacturer to original part information and or delivery NOTE Not all propeller parts can be replaced in the field Only some outside mounted parts as the flange o ring and the connecting hardware screws nuts cables etc can be replaced in the field Page 2 2 SEN 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL N kter dal d ly mohou b t m n ny v provozu pouze pracovn ky vy kolen mi a Some other parts can be replaced in the field only by persons trained and pov en mi v robcem vrtule approved by propeller manufacturer Kontaktujte v robce vrtule pro v ce informac Contact propeller manufacturer for more information Strana 2 3 2 3 6 2 2012 SISERNE 61 10 00 2012 02 06 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL 3 TYPOV ZNACEN 3 MODEL DESIGNATION Vrtule typov rady V508 Propeller V508 Type series V508 E 99 B B1 V508 E 99 B B1 1 2 3 4 5 1 2 3 4 5 1 Typ vrtulov hlavy 1 H
247. ru blesku do vrtule mus b t p ed dal m provozem provedena kontrola Pokud v ak nen vrtule o ividn po kozen m e b t do asn provozov na dal ch 10 hodin p ed proveden m kontroly Pro dodate n ch 10 hodin provozu mus b t vrtule prohl dnuta dle n sleduj c ho postupu a Sejm te p edn kryt vrtule a vizu ln zkontrolujte vrtuli kryt a komponenty odmrazov n na v skyt po kozen kter je nutn p ed dal m letem odstranit nap p etr en kabely nebo op len vrtulov hlavy b Zkontrolujte vrtulov listy na v skyt po kozen zp soben ch derem blesku c Ov te funkci elektrick ho odmrazovac ho syst mu d Bez ohledu na rozsah po kozen mus b t der blesku zaznamen n do z znamn ku vrtule UPOZORN N Bez ohledu na v sledek prohl dky mus b t vrtule po 10 hodin ch provozu odesl na k v robci nebo do autorizovan ho servisn ho st ediska na proveden d kladn kontroly 3 Kontakt s ciz m objektem Kontakt s ciz m objektem je jak koliv ud lost za chodu nebo za klidu motoru kdy p i kontaktu vrtule s mkoliv jin m ne je vzduch dojde k viditeln mu po kozen vrtulov ch list Pouze mal po kozen od kam nk vznikl b hem norm ln ho provozu vrtule se nepova uj za kontakt s ciz m objektem Kontakt vrtule s ciz m objektem m e zp sobit irok spektrum po kozen Bez kompletn demont e vrtule nen mo n zjistit rozsah po
248. ryska na p ce s va kou s ryskou Sv na stupnici regul toru Check whether guideline on the lever with cam aligns with guideline Sv onto the obr zek 11 19 Pokud se rysky nekryj uvoln te pojistnou matici t hla kter je na governor scale figure 11 19 If the guidelines are not aligned loose rod safety nut stran vidlice kl em Sv 1532 924 z n ad pro motor T hlo vysu te mimo kulisu which is at yoke side with wrench Sv 1532 924 from engine toolkit Place the rod p ky Sv obr zek 11 17 a vidlic ot ejte v pot ebn m sm ru v dy o n sobky out of the gate Sv figure 11 17 and turn the yoke in respective direction always at 180 Opakujte kontrolu p i zasunut vidlici s epem a se zen d lky t hla a do multiple of 180 Repeat the check yoke is inserted and pin is installed and rod dosa en nejni ho mo n ho rozd lu rysek length adjustment until the guidelines lowest difference Dot hn te pojistnou matici t hla kl em Sv a zajist te ji v zac m dr tem j Tighten the rod nut with wrench Sv and secure with lock wire Po skon en m se izov n na roubujte na vlo en ep matici k After adjustment install nut onto the inserted pin Poji t n prove te a po kontrole z kladn ho se zen podle t to kapitoly Secure after basic adjustment check according this section Ryska Sv Guideline Sv Obr zek 11 19 Se zen t hla Sv Figure 11 19 Rod Sv adjust
249. s 1 mm 1 5 mm and 2 mm 0 04 0 06 and 0 08 inch Maximum two washers can be under the cover Screw the cover 72 with pressing the spring manually to the relief valve body 71 Then hold the body 71 with a suitable wrench and tighten with other wrench the cover 72 CAUTION DO NOT TIGHTEN THE RELIEF VALVE BODY TOO MUCH IT COULD PUT ACROSS AND IT COULD CAUSE SLEEVE VALVE 77 STICKING IT IS GUIDED WITH PRESSURE UNSTEADINESS AND OSCILLATION ALSO THE BODY CANNOT BE LOOSEN BECAUSE OF LEAKAGE Secure the relief valve with lock wire Purge air from the system at engine ground test 4 Remedy for relief valve leakage Relief valve leakage can be caused by loosen relief valve cover or defective sealing Tighten the cover such way that lock wire will be removed hold the relief valve body 71 to fix it at tightening and tighten the cover 72 Secure the relief valve with lock wire use standard procedure If defective sealing is the cause remove lock wire hold the relief valve body 71 to fix it and remove the cover 72 NOTE Be careful when removing the cover to don t loose washers 73 and to keep pin 74 on the spring 75 Page 11 66 PROPELLER CONTROL SYSTEM 2012 02 06 AVIA PROPELLER Vadnou t sn c podlo ku y prvek 76 sejm te a zm te celkovou tlou ku P ipravte si nov t sn c krou ky o stejn celkov tlou ce Je dovoleno pou t maxim ln dvou podlo ek Nov t sn c podlo ky nasu
250. sou st vrtule zat mco sb ra je montovan na motoru Kabely spojuj sb rac krou ek s odmrazovac mi t lesy Odmrazov n je zeno asova em kter p iv d energii do syst mu a oh v odmrazovac t lesa v ur en ch asov ch intervalech Olej Pracovn kapalinou pro innost vrtule je olej odeb ran z mazac soustavy motoru Dal informace jsou uvedeny v provozn p ru ce motoru Minim ln teplota oleje pro innost vrtule je 40 C 40 F Strana 4 3 5 12 2013 KONSTRUKCNI A PROVOZNI INFORMACE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Counterweights Propellers are equipped with counterweights designed as part of the clamps Force from counterweights assist to move the blades into the high pitch position and if oil supply lost from governor move the blades into the feather position Propeller spinner The spinner dome and spinner bulkhead are made from aluminum alloy Filler plates on the spinner bulkhead increase the stiffness of the spinner dome on the cutouts for the blades On the bulkhead are located balancing weights De icing The propeller has electrical de icing system optionally installed The de icers installed on the blades heat the blades and combined with the centrifugal force and airstream blast remove accumulated ice from blades surface A slip ring and brush assembly conduct power to the de icers through the cables Slip ring is part of the propeller
251. sou li instalov na na po kozen a odlepen V p pad n lezu kontaktujte v robce vrtule 7 Po spu t n motoru ov te ovl d n ot ek a funkci vrtule dle postupu uveden ho v letov p ru ce letounu 8 Sledujte v skyt nezvykl ch vibrac Jestli e doch z k vibrac m vypn te motor zjist te p inu a p ed dal m letem ji odstra te Postupujte dle odd lu Vibrace v t to kapitole a dle kapitoly Odstra ov n z vad v t to p ru ce UPOZORN N NADM RN VIBRACE MOHOU B T P ZNAKEM VADY LISTU VRTULE NEBO KOMPONENTU ULO EN LISTU ZTR TA LISTU ZA LETU M E VY STIT V KATASTROFICKOU NEHODU LETOUNU B 300 HODINOV RO N PROHL DKA POZN MKA Podrobn prohl dka se prov d po ka d ch 300 hodin ch provozu nejpozd ji v ak po 12 kalend n ch m s c ch Pro mo nost efektivn ho pl nov n prohl dky se m e p edepsan hodinov interval pohybovat v rozmez 30 letov ch hodin 1 Sejm te p edn kryt vrtule a zkontrolujte vrtulov listy kryt a ve ker viditeln d ly vrtule na v skyt vrub z sek mechanick ho opot eben trhlin a koroze Opravu vrtulov ch list prove te dle kapitoly Udr ba v t to p ru ce V p pad zji t n po kozen jin ho d lu vrtule kontaktujte Avia Propeller 2 Zkontrolujte povrch list krytu a viditeln d ly vrtule na zn mky deru blesku V p pad n lezu nebo podez en postupujte dle odd lu
252. ssembly 22 Inspect the new carbon block assembly 22 from spare parts whether the carbon blocks 79 are not defective and whether safety rings 80 are in place CAUTION DON T INSTALL THE CARBON BLOCK ASSEMBLY WITHOUT THE SAFETY RING 80 REPLACE THE COTTER PIN Install the carbon block assembly see section Governor installation Verify basic adjustment according to procedure in this manual Page 11 69 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER Obr zek 11 38 Nosi kluzn ch kamen 11 11 SKLADOV N A KONZERVACE 1 Konzervace regul toru demontovan ho z motoru Regul tor sejmut z motoru je nutno nakonzervovat Konzervaci prove te n sleduj c m zp sobem Nejd ve ot ete vn j plochy ist m t tcem lehce namo en m do vhodn ho istidla UPOZORN N P I OT R N POVRCHU DBEJTE NA TO ABY IST C PROSTREDEK NEVNIKL DOVNITR REGUL TORU PR RUBOU KOLEM KOAXI LN CH SOUP TEK 18 19 BLOKOVAC HO OUP TKA 35 A DO SK KY 5 MIKROSP NA EM 23 NEODMAST TE KLOUBOV LO ISKA T HLA 29 32 A 65 DR HU KULISY P KY Sv 66 A VA KY P KY 34 A TAK EPY NOSI E KLUZN CH KAMEN 22 Vn j plochy mimo barven ch pot ete lehce t tcem s konzerva n m olejem O konzervaci prove te z pis do dokumentace regul toru Strana 11 70 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Figure 11 38 Carbon block assembly
253. tahov n m v ech matic trubek a dut ho roubu Neopome te dot hnout trubky i na jejich druh m konci Nakonec pojist te dut roub 78 s matic 59 a ob matice trubek 85 86 v zac m dr tem standardn m zp sobem Neopome te pojistit trubky i na jejich druh m konci Strana 11 67 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Defective sealing washer element 76 remove and measure total thickness Prepare new sealing with the same thickness Use maximum two washers Split the new sealing washers onto the cover 72 Verify that the pin 74 is at the spring 75 and original washers 73 are installed Hold the relief valve body 71 with a suitable wrench and screw the cover 72 with the washers 76 and tighten with other suitable wrench see above Secure the relief valve with lock wire b Remedy for turning screw leakage Remove lock wire from the turning screw 78 figure 11 36 and from the both tube cap nuts Remove the tube 86 to the feathering pump LUN7840 8 Remove the tube 87 to the feathering valve LUN7880 8 NOTE Before the tube will be removed it is necessary to loose also the second end of the tube If itis not necessary don t remove the nut 59 with the ball 60 from the turning screw 78 Remove the turning screw 78 together with parts 45 46 44 59 60 88 and remove defective sealing rings 89 Be careful for the ball 92 Install new sealing rings
254. te ep z vidlice t hla Sv 65 Potom t hlo vysu te mimo kulisu Sv viz obr zek 11 4 Toleran n pole a T hlo 29 reverzu P ka Bc Ryska dorazu Sv Ryska min letov ho hlu Prvek 37 P ka s va kou P ka BI P ka Rn M n Op rn krou ek I Blokovac V oup tko 2041 Doraz Cor S praporu 16 P u Doraz max ot ek 15 Ta n pru ina Bezpe nostn doraz Z str ka Obr zek 11 3 Regul tor LUN7815 02 Pohled sm rem k motoru Strana 11 9 13 4 2010 SYSTEM OVLADANI VRTULE E 1500 INSTALLATION AND OPERATION MANUAL 5 With Bc lever figure 11 3 in basic position guideline on the lever with cam aligns with minimum flight pitch guideline on the governor scale and the control lever pin touches the stop 58 verify Rn lever travel between stops 15 and 16 CAUTION IF THE LEVER Rn IS NOT TOUCHING THE STOP DON T MOVE THE LEVER Bc FROM ITS BASIC POSITION MIN FLIGHT ANGLE GUIDELINE TO REVERSE LOCKING MECHANISM COULD BE DAMAGED 61 10 00 6 Remove cotter pin nut and remove pin from rod Sv les Then place the rod out from slotted piece Sv see figure 11 4 Range for Lever 29 reverse Lever Bc Sv sto m s Minimum flight pitch A RRS Element 37 Koo Lever with cam kk LX a ke qa Lever BI Uf s Lever Rn lever X FLE ie p HA 11 k BETA ing S m KL T
255. te malou ru n rota n brusku s brusn m kotou kem p lkulat 1 Use a small hand held rotary grinder with grinding wheel half round mill piln k nebo smirkovy pap r o hrubosti 80 Odstra te po kozen z hrany file or 80 grit sandpaper to remove damage from blade edge as listu tak jak je zn zorn no na obr zku 7 6 displayed in figure 7 6 I 10X zv t ovac lupou se ujist te e po kozen je pln odstran no Use 10X magnifying glass to verify that the damage was totally removed P ele t te opravenou plochu erven m ScotchBrite nebo smirkov m pap rem o hrubosti 280 0 Polish the repaired area with red ScotchBrite or 280 grit sandpaper 4 Paint the repair area Refer to Painting After Repair in this chapter 14 Provedte n t r opraven plochy dle postupu v t to kapitole EDGE REPAIR d DEPTH OF REPAIR D TEN TIMES THE DEPTH OPRAVA HRANY d HLOUBK D DESET OPRAV FOU JE Jo Ton OF REPAIR Obr zek 7 6 M stn oprava hrany listu Figure 7 6 Blade edge local repair Strana 7 9 TEN Page 7 9 17 15014 DRZBA 61 10 00 MAINTENANCE 2014 01 17 AVIA PROPELLER 3 N t r po oprav Chra te opravenou plochu proti korozi Aplikujte chemick povlak a vrchn n t r dle n sleduj c ho postupu 1 O ist te povrch pomoc acetonu nebo MEK 2 Alikujte protikorozn povlak Alodine 1200 nebo Alodine 1132 Touch N Prep na hol povrch Postupu
256. te na v ko 72 P esv d te se zda na pru in ventilu 75 je ep 74 a uvnit v ka p vodn podlo ky 73 stejn tlou ky a stejn ho po tu Podr te kl em t leso reduk n ho ventilu 71 aby se nedotahovalo za roubujte do n j v ko 72 s podlo kami 76 a dot hn te kl em viz v e uveden upozorn n Reduk n ventil pojist te v zac m dr tem b Odstran n net snosti dut ho roubu Sejm te v zac dr t z hlavy dut ho roubu 78 obr zek 11 36 a z matice trubky 84 na hrdle s tryskou 44 a z matice trubky 85 na hrdle 46 Sejm te trubku 86 k pomocn mu erpadlu LUN7840 8 Sejm te trubku 87 k ovlada i LUN7880 8 POZN MKA Ne trubku sejmete mus te je povolit na jejich druh m konci Matici 59 s kuli kou 60 pokud to nen nutn nedemontujte z dut ho roubu 78 Vy roubujte dut roub 78 spole n s d ly 45 46 44 59 60 88 a odstra te vadn t sn c krou ky 89 Pozor na kuli ku 92 Nasa te na dut roub 78 nov t sn c krou ky 89 a t leso zp tn ho ventilu 45 s mezikrou kem 88 v nazna en poloze tj ipkou nahoru obr zek 11 36 a dut roub zat m jen lehce za roubujte do t lesa regul toru V hrdle 44 mus b t kuli ka 92 UPOZORN N POU IJTE JEN P EDEPSAN T SN C KROU KY HLIN KOV Namontujte zp t ob sejmut trubky 86 87 Kone n dota en dut ho roubu 78 a trubek 86 a 87 prove te opatrn postupn m do
257. ther position adjustment for governor LUN7815 03 a Perform when feathering time is higher than 15s adjusting is possible by using the stop 16 b Remove seal and lock wire from the stop 16 figure 11 30 c Move propeller control lever in cockpit to maximum RPM position the lever Rn is at maximum RPM stop 15 d Loose propeller control lever stop in the cockpit by about 3 mm 0 12 inch e Loose the stop nut 16 and turns it 2 to 2 5 clockwise lever Rn travel to feather position will increase f Move propeller control lever easy up to the stop 16 CAUTION IF THE LEVER Rn DOESN T REACH THE STOP 16 OT MEANS THAT LEVER MOVEMENT COULD BE OBSTRUCTED INSIDE THE GOVERNOR KEEP THE LEVER Rn IN THIS POSITION AND RETURN THE STOP 16 BACK UNTIL IT TOUCH THE LEVER Rn PIN AND ANOTHER HALF OF TURN BACK WITH THE SCREW g Adjust clearance of the feather stop in the cockpit to 2 mm and secure h Secure the stop 16 with lock wire i Verify functionality according to procedure in section 11 7 j Make a record in the governor documentation 4 19 RPM adjustment for governor LUN7815 02 LUN7815 03 twin engine aircrafts a Minimum flight angle and thus idle RPM is adjustable with the stop 58 b Perform this adjustment only if 1 Difference in idle RPM is higher than 40 rpm Page 11 56 PROP
258. tion without feathering pump 1 EMERGENCY FEATHERING function check IQ IO 17 190 ma 61 10 00 Engine control lever set to idle stop Move propeller control lever from maximum RPM position to feather position Propeller speed should be about 350 rpm Loose propeller control lever and move back to maximum propeller rpm position Propeller speed before and after should be the same Verify propeller for leakage Record the test into the propeller logbook Page 11 51 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER 11 8 DALS NASTAVEN A 1 Strana 11 52 13 4 2010 Vrtulovy regul tor LUN7815 Se zen maxim ln ch regulovan ch ot ek vrtule plat pro regul tory LUN 7815 02 LUN7815 03 Prov d se po prv m z letu letounu Ovl dac p ku vrtule v kabin pilota p estavte tak aby p ka Rn na regul toru byla vzd lena od dorazu max ot ek Odjist te doraz 15 obr zek 11 29 Povolte matici a prove te se zen max ot ek ot en m dorazov ho roubu 15 Za roubov n sn en ot ek Vy roubov n zv en ot ek Jedno oto en roubu 360 znamen zm nu max ot ek p ibli n o 20 ot min POZN MKA Maxim ln regulovan ot ky vrtule jsou uvedeny v tabulce 11 4 Ovl dac p ku vrtule p estavte do polohy max ot ek p ka Rn mus b t na dorazu 15 Pokud zjist te v li se i te doraz ovl dac
259. to be established between the carbon block and the beta ring when initially installing a new or overhauled propeller Figure 5 11 1 Maximum permitted side clearance is 0 4 mm 0 016 inch b For propeller models using U Type beta ring the side clearance of 0 025 to 0 05 mm 0 001 to 0 002 inch to be established between the carbon block and the beta ring when initially installing a new or overhauled propeller Figure 5 11 2 Maximum permitted side clearance is 0 25 mm 0 01 inch Page 5 9 2 INSTALLATION AND OPERATION INSTRUCTION 2014 10 20 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL UPOZORN N CAUTION UJIST TE SE ZE BETA KAMEN CHOD VOLN VBETA KROUZKU MAKE SURE THE SIDE CLEARANCE EXIST THROUGHOUT FULL 360 V CEL M ROZSAHU 360 OTOCEN BETA KROUZKU DEGREES OF THE BETA RING ROTATION POZN MKA NOTE Pro dodr en stranov v le lze strany beta kamene zbrousit jemn m Sand the sides of the carbon block with fine sandpaper as needed to establish smirkov m pap rem the side clearance 13 Vlo te beta k men na beta krou ek a na p ku zp tn vazby P ipevn te beta 13 Install the carbon block assembly into the beta ring and on the beta feedback k men k t hlu zp tn vazby dle instrukc v robce letounu nebo regul toru lever Attach the carbon block to the beta feedback lever per the airframe or governor manufacturer s instructions KROUZEK BETA RING j
260. to idle Move propeller control lever from maximum RPM position to feather position Propeller speed is about 350 rpm in feather position Move propeller control lever back to maximum RPM position Propeller speed before and after should be the same CONTROL FEATHERING function check 110 IQ IO 17 100 I2 ro IO 190 Place engine control lever to maximum continuous power position Set with propeller control lever propeller speed to 1900 rpm Switch on the FEATHERING breaker Press TEST FEATHERING button Observe FEATHERING PUMP switching on Immediately after energizing the FEATHERING PUMP lamp release the button lamp will extinguish Propeller speed must stand constant when the lamp is energized Move propeller control lever to maximum propeller RPM position Place engine control lever to idle stop Check of feathering installation without feathering pump 1 EMERGENCY FEATHERING function check Engine control lever set to idle stop Move propeller control lever from maximum RPM position to feather stop and fix it Propeller speed should be about 350 rpm Loose propeller control lever and move back to maximum propeller rpm position Propeller speed before and after should be the same Verify propeller for leakage Record the test into the propeller logbook Page 11 47 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER B Vrtulov regul tor LUN7816
261. tr t pera c Na regul toru ot ek kde dosud nen p ipojeno ovl d n p ky Bc od motoru kontrolujte 1 Doraz p ky Sv na dorazov roub volnob hu kontrolujte listovou m rkou 0 05 mm 0 002 inch na stisk obr zek 11 25 E 1500 INSTALLATION AND OPERATION MANUAL 3 Maximum reverse output adjustment Perform when the propeller governor installation the engine installation a Disconnect linkage from engine power lever at engine b Loose and remove nut and screw from the lever Sv figure 11 25 pull carefully the lever such way that it passes stop pin at turning NOTE Don t remove the lever Sv from inner coaxial valve to avoid spring loose C Verify at the governor where linkage to the lever Bc is not connected following items 1 Lever Sv touching the idle stop verify with feeler gauge 0 05 mm 0 002 inch for compression figure 11 25 2 Sou asn ryska na p ce mus b t proti rysce minim ln ho letov ho hlu na 2 Atthe same time guideline on the lever must align minimum flight pitch guideline stupnici regul toru obr zek 11 264 on the governor scale figure 11 264 Stahovac roub P ka Sv D Inob hu ep oraz ovl dac p ky Obr zek 11 25 Se zen max reverzn ho v konu p ka Sv Figure 11 25 Maximum reverse output adjustment lever Sv Strana 11 40 2 11 40 13 4 2010 SYSTEM OVLADANI VRTULE 61 10 00 P
262. truction of aircraft manufacturer b Replace the pressure switch per instruction of aircraft manufacturer c Follow instruction of engine manufacturer Page 8 6 TROUBLESHOOTING 2012 02 06 AVIA PROPELLER C ODMRAZOV N Z vada P i zapnut m odmrazov n vrtule je ru eno radiov spojen Mo n p ina a Po kozen nebo nadm rn opot eben uhl k b Zne i t n m d n sb rac krou ky c Po kozen nebo nadm rn opot eben m d n sb rac krou ky d Nedokonal kontakt v elektrick cest N prava a P ekontrolujte uhl ky dle kapitoly Prohl dky Je li pot eba vym te sb ra podle kapitoly Mont n a provozn instrukce b O ist te m d n sb rac krou ky c V m na p enosov ch kruh u v robce nebo v autorizovan m servisn m st edisku d Systematicky prohl dn te p slu n spoje p padn dot hn te Z vada P i zapnut odmrazov n je odmrazov n nefunk n Mo n p ina a Vadn odmrazovac t leso b Z vada v elektrick cest N prava a List y s vadn m t lesem zaslat do opravy k v robci nebo do autorizovan ho servisn ho st ediska b Postupujte dle instrukc v robce letounu D VRTULE HLAVA LISTY Z vada Vn j net snost servomechanismu Mo n p ina a Po kozen t sn n v lce N prava a Vrtuli za lete k v robci nebo do autorizovan ho servisn ho st ediska
263. tu pouzdra nepresahuj c 1 5 obvodu prvn ho a druh ho z vitu zvenku a 1 4 obvodu u ostatn ch z vit a dna pouzdra Pro kontrolu zadn ch ploch z vit pouzder pou ijte speci ln zrc tko POZN MKA P padn stopy koroze v z vitu pouzdra ot ete istou ut rku p padn lehce p ele t te jemn m smirkov m pl tnem nebo ScotchBritem UPOZORN N V p pad zji t n siln a nebo hloubkov koroze nelze li list vyjmout z pouzdra nebo v p pad jak chkoliv pochybnost st hn te vrtuli z provozu a kontaktujte Avia Propeller 5 Instalujte listy dle kapitoly Instalace list v t to p ru ce 6 Prove te kontrolu funkce omezova e ot ek dle n sleduj c ho postupu POZN MKA Nevztahuje se na vrtuli V508Z a V508H a Demontujte v ko omezova e obr zek 6 1 speci ln m kl em POZN MKA Speci ln kl nen nutn pro nov proveden omezova e ot ek P N 300 095 UPOZORN N Op rka pru iny mus vy n vat z t la omezova e p ibli n 1 5 mm 0 06 inch as displayed in figure 6 1 V opa n m p pad op rku n kolikr t stla te a uvoln te b Namontujte p edn kryt vrtule c Spus te a proh ejte motor dle postupu v Letov p ru ce d Prove te odvzdu n n hydraulick ho syst mu vrtule p esunut m p ky ovl d n vrtule z minim ln ho letov ho hlu do praporu a zp t minim ln t ikr t e P esu te p ku ovl d n vrtule do polohy m
264. tule p estavte zp t do polohy max ot ek e Ovl dac p ku motoru nastavte na zar ku volnob hu ryska na p ce s va kou mus b t proti rysce minim ln ho letov ho hlu na stupnici regul toru obr zek 11 27A Pokud nen prove te se zen podle Provozn p ru ky motoru ep ovl dac p ky vn j ho koaxi ln ho oup tka mus b t na dorazu 58 UPOZORN N POKUD JE OVL DAC P KA MOTORU PRESTAVENA ZA ZAR KU VOLNOB HU DO P SMA MAL CH KLADN CH A Z PORN CH HL NESM B T OVL DAC P KA VRTULE PRESTAVOV NA DO PRAPOROV POLOHY A NAOPAK Strana 11 42 13 4 2010 SYSTEM OVL DAN VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL i Slip the lever Sv to its original position after adjustment and reinstall the screw with securing washer tighten and secure NOTE Attend to setting the hole for the screw against groove in the sleeve valve at lever Sv installation into original position j Tighten and secure connecting points on the lever Bc and the fuel control unit according to the engine operational manual 11 7 TESTING A Propeller Governor LUN7815 1 Basic adjustment check only for governor LUN7815 02 a Disconnect the rod Sv 65 from the gate Sv loose and remove nut and remove the pin from the rod fork Then move the rod out of the gate Sv figure 11 17 b Fix the loosen rod
265. ub type 2 Verze vrtulov hlavy 2 Hub modification 7 and B z kladn verze v roba ukon ena 7 and B basic version production closed D standardn verze D standard version D 2 reverzn hel 8 D 2 reverse angle 8 D AG AGRO verze min letovy hel 10 D AG agricultural version min flight angle 10 Z AGRO verze reverzn hel 3 Z agricultural version reverse angle 3 E se sekund rn zar kou E with secondary stop E AG se sekund rn zar kou bez odmrazov n E AG with secondary stop without de icing H jedno inn H single acting 3 Pr m r vrtule v palc ch 3 Propeller diameter in inches 4 listu podle certifikovan kombinace hlava listy 4 Blade type according to certified hub blade combination 5 Odmrazov n 5 De icing A bez odmrazov n A notinstalled B1 elektrick 28V DC 1 vyh van sekce B1 electrical 28V DC single heating element B2 elektrick 28V DC 2 vyh van sekce B2 electrical 28V DC dual heating elements Strana 3 1 2 Xp Page 3 1 10 5 2011 TYPOVE ZNACENI 61 10 00 MODEL DESIGNATION 2011 05 10 Strana 3 2 17 1 2014 AVIA PROPELLER Vrtule typov rady V510 510 T 90 A A 1 2 34 5 1 Typ vrtulov hlavy 2 Verze vrtulov hlavy bez ozn z kladn verze AG AGRO verze T akrobatick verze 3 Pr m r vrtule v palc ch 4 Typ listu podle certifikovan kombinace hlava listy 5 Odmrazov n A bez odmrazov n
266. ue of 8 s when feathering pump is installed INDIE Page 11 53 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER b Kontrolu prove te p i motorov zkou ce c Sejm te plombu a v zac dr t z dorazu 16 obr zek 11 30 P ka Rn Obr zek 11 30 Se zen dorazu praporu d Ovl dac p ku vrtule v kabin pilota p estavte do polohy max ot ek p ka Rn je na dorazu max ot ek 16 UPOZORN N ZEN QE P ED PRESTAVEN M OVL DAC P KY VRTULE KONTROLUJTE OVL DAC P KU MOTORU MUS B T NA ZAR ZCE VOLNOB HU KONTROLUJTE JISTI E BATERIE MUS B T VYPNUTY Povolte matici dorazu 16 a oto te j m o 2 a 2 5 ot ky ve sm ru hodinov ch ru i ek krok p ky Rn do praporov polohy se zv t f Presu te ovl dac p ku vrtule lehce a na doraz kter m nebude doraz 16 ale blokovac oup tko na kter naraz hlavn oup tko uvnit regul toru p esouvan p kou Rn g V t to poloze ovl dac p ku vrtule zajist te Strana 11 54 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL b Perform the verification at engine ground test c Remove seal and lock wire from the stop 16 figure 11 30 Lever Rn Feathering Figure 11 30 Feather stop adjustment d Move propeller control lever in cockpit to maximum RPM position the lever Rn is
267. uj jako Time Between Overhaul TBO Limit TBO je ur en provozn m limitem vyj d en m hodinami provozu a kalend n m limitem uv d n m v kalend n ch m s c ch Gener ln oprava m b t provedena po dosa en n kter ho z t chto limit podle toho co nastane d ve Gener ln opravu m e prov st pouze Avia Propeller nebo schv len servisn st edisko a to v souladu s platn mi revizemi p ru ek pro gener ln opravu uveden mi v odd lu Souvisej c dokumenty v t to kapitole OBECN 61 10 00 This publication provides operation installation and line maintenance information on the Avia feathering and reversing propellers V508 3 blade and V510 5 blade Type Series Propellers in this manual are used on turbine engines with ARP880 mounting flange In addition to the propeller assembly the propeller governing system of M601 engines operated with governors LUN7815 and LUN7816 is addressed in this manual Installation removal operation and trouble shooting data is included in this publication However the airplane and engine manufacturers manuals should be used in addition to this information Overhaul For the list of TBO limits of all Avia propellers refer to latest issue of Avia Service Bulletin No 1 available at Avia Propeller website at www aviapropeller com The overhaul is periodic process performed at specific intervals in which the propeller is disassembled and insp
268. ukce v t to p ru ce Instalace s regul torem Jihostroj LUN7815 nebo LUN7816 kapitola Syst m ovl d n vrtule v t to p ru ce Instalace s regul tory jin ch v robc p ru ka v robce motoru nebo regul toru b Vym te regul tor ot ek vrtule dle instrukc v robce motoru Z vada Zv en odpor p i p estaven p ky do reversu Mo n p ina a Usady v koaxi ln m oup tku N prava a Vym te regul tor ot ek vrtule dle instrukc v robce motoru Z vada Samovoln zv en ot ek vrtule Mo n p ina a Z vada na regul toru vrtule N prava a Vym te regul tor vrtule dle instrukc v robce motoru Z vada P i kontrole omezova e nedosahuje vrtule p edepsan ch ot ek Mo n p ina a Vadn omezova ot ek vrtule N prava a Vym te omezova ot ek dle instrukc v robce motoru Strana 8 4 6 2 2012 ODSTRANOV N Z VAD E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL Trouble High propeller overspeed at acceleration Probably cause a Incorrect adjustment of minimum flight pitch beta ring position b Defective governor Remegy a Verify and adjust the minimum flight pitch Model V508H chapter Installation and Operation Instructions of this manual Installation with governor Jihostroj LUN7815 or LUN7816 chapter Propeller Control System of this manual Installation wit
269. ulace ot ek je zn zorn n na obr zku 11 1 Ovl dac p ka ot ek na regul toru je spojena p es t hla s p kou ovl d n vrtule v kabin letounu Poloha ovl dac p ky ur uje stla en d c pru iny Toto stla en p edstavuje po adovan ot ky H del regul toru je poh n na od reduktoru motoru a jej ot ky jsou pom rn k ot k m vrtule H del je propojena se z va mi se kter mi se spole n ot Strana 11 2 6 2 2012 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL 11 PROPELLER CONTROL SYSTEM 11 1 INTRODUCTION A General This chapter is addressed only to installation with governor Jihostroj P N LUN7815 or LUN7816 For propeller control system with Avia governor refer to Avia Operation and Installation Manual E 1707 For propeller control system with other governors refer to engine manufacturer s manual 11 2 Cancelled 11 3 PROPELLER CONTROL A Oil supply The propeller governor consists of a oil pump and control subassemblies The oil pump ensures pressurized oil to propeller control It consists of a gear pump and a relief valve which holds pump outlet at required level B RPM control RPM control it is control of the propeller to constant speed is provided by propeller governor which compares real RPM with requested RPM and accordingly turns the blades There are principles of RPM control on figure 11 1 Speed
270. ust be statically rebalanced f Propeller must be dynamically rebalanced B FEATHERING Trouble Propeller did not move into feather after automatic feathering initialization Probably cause a Failure in hydraulic circuit e g LUN7880 feathering pump etc b Failure in electrical circuit c Low working pressure Remegy a Replace defective hydraulic element in the system Follow instruction of aircraft manufacturer b Follow instruction of aircraft manufacturer Check pressure in the system Follow instruction of engine manufacturer Page 8 5 TROUBLESHOOTING 2012 02 06 AVIA PROPELLER Z vada Praporovac cyklus prodlou en d le ne 8 sekund nebo neukon en Mo n p ina a N zk tlak od praporovac ho erpadla b Vadn elektrick instalace nap styka asovac rel apod c Net snost v olejov m syst mu N prava a Zkontrolujte praporovac erpadlo nap t pro praporovac erpadlo Postupujte dle instrukc v robce letounu b Postupujte dle instrukc v robce letounu c Postupujte dle instrukc v robce letounu Z vada Vrtuli nelze ru n zapraporovat Mo n p ina a P ka ovl d n ot ek vrtule na regul toru nen na dorazu pro praporov n N prava a Se i te ovl d n p ky ot ek vrtule tak aby p ka Rn byla na dorazu pro praporovou polohu Postupujte dle instrukc v robce motoru Z vada Kontrolka praporov n z
271. ve te a po kontrole z kladn ho se zen podle t to kapitoly Toleran n pole reverzu Obr zek 11 21 Se zen reverzn ho v konu rysky SYST M OVL D N VRTULE E 1500 INSTALLATION AND OPERATION MANUAL 4 Maximum reverse output adjustment a 61 10 00 only for propeller governor LUN7815 02 Verify that rod Sv 65 is disconnected from the gate Sv If not loose and remove nut and remove the pin Then disconnect the rod from its gate figure 11 17 Fix the loosen rod Sv 65 using lock wire to the governor such way that it will not be reduced in its movement later during adjustment Adjust maximum reverse power according to engine operational manual Place the engine condition lever to maximum reverse position after reverse power adjustment Guideline on the cam lever should align with reverse range zone figure 11 21 If not adjust according to the engine operational manual Connect the rod Sv 65 tighten the nut on the pin and verify adjustment of the joint linkage on the scale according to this section After basic adjustment verification according to this section secure the nut with a cotter pin Range for reverse Figure 11 21 Reverse output adjustment scale Page 11 33 PROPELLER CONTROL SYSTEM 2010 04 13 AVIA PROPELLER B Vrtulov regul tor LUN7816 1 Se zen regul toru prvkem B2 Prov d se po
272. vent whether or not the engine is operating when the propeller comes into contact with anything other than air resulting in visible damage of the propeller blades Only minor damage from stones during normal propeller operation may not be considered as foreign object stike A foreign object strike can cause a broad spectrum of damage It is no possible to detect the extent of damage inside the hub without its disassembly Any foreign object strike event resulting in visible damage of the blades except minor stone nicks requires overhaul at manufacturer or authorized service centre Page 6 13 INSPECTIONS 2012 02 06 AVIA PROPELLER 4 Vystaven ohni nebo z ru Vystaven ohni nebo nadm rn mu ru vy aduje kontrolu vrtule a za zen montovan ch na motoru vyr b n ch Avia u v robce nebo autorizovan m servisn m st edisku 5 Kontaminace motorov ho oleje Kontaminace motorov ho oleje vy aduje kontrolu vrtule a za zen montovan ch na motoru vyr b n ch Avia u v robce nebo autorizovan m servisn m st edisku 6 Tvrd p ist n Za tvrd p ist n se pova uje takov p ist n kdy letoun dosedne na zem s v t rychlost a silou ne je obvykl p i em nedojde ke kontaktu vrtule se zem a Pokud p i tvrd m p ist n nebyly p ekro eny limitn n sobky zat en letounu nejsou na vrtuli vy adov ny dn kroky b Pokud p i tvrd m p ist n byly p ekro eny limitn n sobky zat
273. visl na v konu motoru a atmosf rick ch podm nk ch Kontrola tlaku v proh vac v tvi praporovac ho erpadla jen p i z stavb syst mu praporov n s praporovac m erpadlem 1 Ovl dac p ku motoru p estavte do polohy max trval ho v konu 2 Signalizace PRAPOROVE ERPADLO se nerozsv t SYST M OVL D N VRTULE E 1500 INSTALLATION AND OPERATION MANUAL Perform in the extent to verify appropriate functionality after exchange of other propeller control system instruments 61 10 00 Start the engine according to the aircraft Flight Manual Warm up engine oil to 60 65 C 140 150 F Purge the propeller control system Place the engine condition lever into idle position Move the propeller condition lever into feather position propeller RPM reduces to 350 rpm Move back the propeller condition lever after about 15 s delay to maximum RPM position and wait to previous RPM 4 Repeatthe cycle times wait about 40 s between the cycles IDS Ico Propeller RPM check at idle only for twin engine aircrafts Set engine control lever to idle Move the propeller control lever to maximum RPM position RPM difference at idle should be 40 RPM max If higher refer to Troubleshooting section in this manual I IN Maximum RPM check Propeller control lever in maximum RPM position Move engine control lever to maximum take off power position Maximum ground RPM should be 2080 120 rpm
274. whereas the brush assembly is mounted on the engine Cables connect the slip ring with de icers De icing system is controlled by timer which distribute power to the system and heat de icers in timed intervals in specific sequence Cil The propeller operates with oil supplied from engine lubricating system Refer to engine manufacturer s manual for more information The minimum oil temperature for propeller operation is 40 C 40 F Page 4 3 DESIGN AND OPERATION INFORMATION 2013 12 05 AVIA PROPELLER E 1500 INSTALLATION AND OPERATION MANUAL Obr zek 4 1 Sestava vrtule V508 D D AG D 2 Z Figure 4 1 V508 D D AG D 2 Z Propeller assembly Strana 4 4 e Page 4 4 17 1 2014 KONSTRUK N A PROVOZN INFORMACE 61 10 00 DESIGN AND OPERATION INFORMATION 2014 01 17 AVIA PROPELLER 1 1 Vrtulov list 2 32 Pouzdro 3 1 P edn kryt 1 2 Odmrazovac t leso 2 33 Vlo ka 3 2 Zadn kryt 1 3 O krou ek 2 34 roub 3 3 N tovac matice 2 35 Pf ruba krytu 3 4 N tovac matice 2 0 Vrtulovy n boj 2 36 Kol k 3 5 N t 2 1 P st 2 37 Kol k 3 6 roub 2 2 V lec 2 38 Vlo ka 3 7 Podlo ka 2 3
275. y se p estav na velk hel a ot ky vrtule klesaj na rovnov n stav U regul toru LUN7816 je prostor velk ho hlu servomechanismu pod st l m tlakem 0 6MPa z d vodu pomoci p i p echodu do velk ho hlu c Nedot en Sledujte obr zek 11 1C Odst ediv s la p sob c na z va je men ne s la od d c pru iny Z va se vyklon dovnit d c oup tko se posune dol a propoj kan l mal ho hlu s kan lem p vodu oleje Listy se p estav na mal hel a ot ky vrtule se zv na rovnov n stav U regul toru LUN7816 mus b t tlak oleje na mal m hlu servomechanismu dostate n velk aby p ekonal tlak 0 6MPa na velk m hlu servomechanismu a v echny ostatn s ly Strana 11 3 13 4 2010 SYST M OVL D N VRTULE E 1500 61 10 00 INSTALLATION AND OPERATION MANUAL together Centrifugal force of flyweights acts against speeder spring This force represents real propeller RPM The flyweight centrifugal force acts on pilot valve support The force from speeder spring acts on the second side of the support The pilot valve support is connected with pilot valve which controls oil flow to or from the propeller There are three basic conditions for propeller governing onspeed overspeed and underspeed a Onspeed Refer to figure 11 1A The centrifugal force acting on the flyweights is balanced by the speeder spring and the pilot valve is neither d

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