Pratt & Whitney Canada
Contents
1. ro de s rie n Cumul de cette installation Cumul jusqu pr sent i 7 j isi depuis uis 2 D Installation d entretien de r vision bon de l installation du dum Mod le renl vement Accumulated This Installation Total Accumulated To Date travail et timbre du v rificateur Engine Modui Model Eng dee Remark ngin i D lemarks SN When Engine Module TSN When Maintenance Overhaul Facility Work Material Material Temps Time Cycles Temps Time Order amp inspection stamp ns T 0 PCE PK0594 PT6A 60A Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est install e This record must be with the engine module logbook where this part is installed Pratt amp Whitney Canada Cie Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp Life Limited Material History Record Une soci t de United Technologies A United Technologies Company des Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Code de traitement thermique mis le A M J Material Name eat Code Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel Issue Date Y M D consulter le Manuel d entretien du moteur ou le Bulletin de service IMPELLER2. 1 Mod le l enl vement Accumulated This Installation Total Accumulated To Date Date travail et timbre du v rificateur Engine Modul Model Eng Modul Remark n D emarks TSN When Engine Module TSN When Maintenance Overhaul Facility Work Temps Time Cycles Temps Time Cycles Order amp inspection stamp nstalle 0 PCE PK0594 PT6A 60A Ins rer le pr sent historique dans le livre du moteur du module la est install e This record must be kept with the engine module logbook where this part is installed Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Life Limited Material History Record Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name Code de traitement thermique Heat Code mis le Issue Date Y M D DISC COMPRESSOR ROTOR EPDCT 2004 10 20 Num ro du mat riel Num ro de s rie du mat riel N de s rie du mat forg Temps de Cycles de Material Number Material Serial Number Forging Mat Serial No fonction fonction Since New Cycles Since New 3034312 A001L3E7 0 0 Donn es sur fe moteur module Engine Module Data Donn es sur le mat riel Material Dat
3. CENTRIFUGAL PZBLW 2004 10 20 appropri selon le cas Num ro du mat riel Num ro de s rie du mat riel N de s rie du mat forg Temps de Cycles de z Material Number Material Serial Number Forging Mat Serial No Sen aen Note For deter nation V GE 3036793 000 502 015 We deg oe Ge S to the engine Maintenance Manual or Service Bulletin as applicable Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data EE JA Observations Num ro de s rie n Cumul de cette installation Cumul jusqu pr sent ion j isi depuis depuis 2 d jusqu pt Installation d entretien de r vision bon de l installation du du moteur d l enl vement Accumulated This Installation Total Accumulated To Date Date travail et timbre du v rificateur mat riel i e le R SN When Engine Module TEN When E Se Maintenance Overhaul Facility Work Material Material Temps Time Cycles Temps Time Cycles Order amp inspection stamp Installed Removed T PCE PK0594 Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est nstall e This record must be kept with the engine module logbook where this part is installed Historique du mat riel dur e de vie limit e Life Limited Material History Record Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834
4. E 6834 1998 06 D signation du mat riel Material Name DISC TURBINE e Pratt amp Whitney Canada C Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Une soci t de United Technologies A United Technologies Company Code de traitement thermique Heat Code mis le MN Issue Date Y M D LASWY 2004 10 20 Nota Pour connaitre les dur es de vie Longueuil Qu bec Canada JAG 1A1 accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Num ro du mat riel Material Number 3040311 Temps de fonctionnement depuis l installation du mat riel Engine Module SN When Material L Installed Num ro de s rie du moteur module Engine Module Serial Number Num ro de s rie du mat riel Material Serial Number A001KWCY Donn es sur le moteur module Engine Module Data Temps de fonctionnement depuis l eni vement du mat riel Eng Module TSN When Material Removed N de s rie du mat forg Temps de Cycles de fonction fonction Forging Mat Serial No 3 Since New Cycles Since New 4270 0 0 Donn es sur le mat riel Material Data Cumul de cette installation Cumul jusqu pr sent Accumulated This Installation Total Accumulated To Date Temps Time Cycles Temps Time Cycles Note For d
5. provide a representative sample of the engine condition While every attempt will be made to identify all items considered be abnormal items may be missed that could cause future damage In no event shall MTU BB be liable for compensatory consequential incidental special punitive or other damages whether the claim for damages is based on contract tort or otherwise MTU BB limits its liability to the value of this contract 6 Recommendations Inspect damage at 100 hours ref page 8 measured crack Subsequent inspections are at operator s discretion but must not exceed 400 hours Name Marcel Hellmann Date 16 October 2013 Signature y R D Comment All pictures including those used for the report will be forwarded to MTU Maintenance Berlin Brandenburg GmbH PT6A 60A Date 17 Oktober 2013 PAGE 6 of 8 MTU Maintenance Field Service Report Borescope Inspection PT6A 60A Everest VIT J Evorest VIT Evorost VIT PT6A 60A Date 17 Oktober 2013 PAGE 7 of 8 MTU Maintenance Field Service Report Borescope Inspection PT6A 60A Evorest VIT Everest VIT Everest VIT Everest VIT Everust VIT Everest VIT PT6A 60A 17 Oktober 2013 PAGE 8 of 8
6. 0000000000 0 OOOOGRGROODOODEBEGEOOOD D External Oil Leak PT6A 60A 17 Oktober 2013 PAGE 3 of 8 MTU Maintenance MTU Field Service Report N Maintenance Borescope Inspection PT6A 60A 2 5 Hot Section Area Hot Section Area Duct Assy Small Exit Vane Ring Assy CT Liner Assy CC N A due to Post configuration Duct Assy Large Exit N A due to Post configuration Liner Assy CC Inner no findings Liner Assy CC Outer loss of coating accompanied by a crack for pictures see page 9 PT6A 60A Date 17 Oktober 2013 PAGE 4 of 8 MTU Maintenance Field Service Report Borescope inspection PT6A 60A Gas Generator Case Area Gas Generator Case not inspected only borescope Fuel Nozzles Fuel Nozzle Tip no findings for pictures see page 7 PRIMARY AND SECONDARY FUEL MANIFOLD ADAPTER ASSEMBLIES PT6A 60A Date 17 Oktober 2013 PAGE 5 of 8 Maintenance Borescope Inspection PT6A 60A MTU Maintenance MTU Field Service Report 3 Exclusion Engine Bearing Inspection is not possible without disassembly 4 Work Performed Borescope Inspection performed i a w P amp WC Maintenance Manual PN 3034342 Chapter 72 00 00 Engine General Inspection Borescope Inspection Revision No 42 dated dec 07 12 Note Only hot section components were inspected as requested by the customer 5 Limitation of Liability A borescope inspection is intended to
7. 1173 1824 1815 1895 1860 36750 36500 0 562 0 547 9 25 9 10 FUEL TEST LHV 0 818 73 S G OIL TYPE OIL CONSUMPTION T O OIL PRESSURE OIL TEMPERATURE RIM DELTA T UNTRIMMED TRIMMED RIM DELTA T UNTRIMMED TRIMMED TRIM CLASS TRIM RESISTANCE COLD HARNESS RESISTANCE CPW 204 18480 PWA 521 0 117 2 152 8 28 2 15 7 29501 951 29501 551 6 58 20 92 TRIMMED MAX NG UNTRIMMED MAX NG DATA PLATE SPEED IDLE SPEED ACCEL TIME F I TO MAX 1 ENGINE DRY WEIGHT PRODUCTION SIGNATURE INSPECTION SIGNATURE RPM 3 35 SECS 8 42 2 DEGF Z GOVERNMENT INSPECTOR LBS THE UNDERSIGNED CERTIFIES THAT THIS RECORD ACCURATELY SETS FORTH THE EVENTS DURING THE TEST MADE ON T DATE 0072 02004 FOREMAN ASSY amp TEST INSP R MEUNIER SIPE THEREIN IDENTIFIED e 4 58 NO 044 Pratt amp Canada Cie Pratt amp Whitney Canada Pratt amp Whitney Canada Corp me inite nologies ni echn Marie Victorin Liste des composants moteur num ros de s rie Une ost de United Hommages A Una Technologies Company Longueuil Qu bec Canada Engine Serialized Component Summary GH 4 LU 450 677 0411 Page 1 P amp WC JR3 6830 E 05 1998 PT6A 60A N de s rie PCE PK0594 Garnet de montage 51024 Serial No i i i i Code de trait de s rie du N de lot pour trait e i i N du mat riel D s
8. 980 3112696 03 BEARING BALL 1 181X2 8345X 743 FLG FC142379 3112748 01 LINER COMBUSTION CHAMBER INNER ASYO A001KXON 3114832 01 COUPLING COMPRESSOR REAR HUB PKAA000U333 3117032 01 VALVE ASSY COMPRESSOR BLEED AHX001834 3119290 02 CASE GAS GENERATOR ASSY OF RWA08A392 3120081 04 HOUSING ASSY PROP REDUCTION GEARBOX XUAA000A110 3120295 01 DUCT ASYO TURBINE EXHAUST A001L872 3120644 01 FUEL CONTROL TURBOPROP 13999890 3121632 01 HOUSING POWER TURBINE STATOR A000A425 S mis d E Approved By so MEUNIER Beiden C Historique du mat riel dur e de vie limit e Pratt amp Whitney Canada Pratt amp Whitney Canada Corp 4 Pratt amp Whitney Canada Corp Life Limited Material History Record Une sede de United TochnalogiaaTA Uniad Technologies 1000 Marie Victorin Longueuil Qu bec Canada J4G 1A1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 Nota Pour connaitre les dur es de vie D signation du mat riel Code de traitement thermique mis le A M J accumul e et r siduelle du mat riel Material Name Heat Code Issue Date Y M D consulter le Manuel d entretien du moteur ou le Bulletin de service DISC TURBINE LALBZ 2004 10 20 appropri selon le cas Num ro du mat riel Num ro de s rie du mat riel N de s rie du mat Temps de Cycles de Material Number Material Serial Number Forging
9. Mat l Serial SC As fonction Note For determination of accumulated Time Since New Cycles Since New and remaining lives on this material refer 3029312 00116 1361 0 0 to the engine Maintenance Manual Service Bulletin as applicable Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data T Temps de Temps de ent Num ro de s rie fonefonnome nt Cumul de cette installation Cumul jusqu pr sent Installation vision bon de l installation du du menn i Mod le l enl vement f Accumulated This Installation Total Accumulated To Date Date travail et timbre du v rificateur En Mul Model di Remark ngine ule D emarks When Regine Module TSN When Maintenance Overhaul Facility Work Material Material Temps Time Cycles Temps Time Cycles Order amp inspection stamp Installed Removed 0 PCE PK0594 PT6A 60A Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est nstall e This record must be kept with the engine module logbook where this part is installed Historique du mat riel dur e de vie limit e Life Limited Material History Record Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du m
10. Material History Record Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 D signation du mat riel Material Name DISC COMPRESSOR ROTOR Heat Code e Pratt amp Whitney Canada C Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Une soci t de United Technologies A United Technologies Company Code de traitement thermique EPDCT mis le A M J issue Se MD Num ro du mat riel Material Number 3034313 Num ro de s rie du mat riel Mater al Serial Number 00112 5 Donn es sur le moteur module Engine Module Data bg N de s rie du mat forg Forging Mat Serial No 2004 10 20 Temps de Cycles de fonction foncti lon Time Since New Cycles Since New 0 0 Donn es sur le mat riel Material Data Longueuil Qu bec Canada J4G 1A1 Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Tonos de Temps de i onctionnement onctionnemen 1 1 servations Num
11. UPLING POWER TURBINE SHAFT 07 660 3100767 01 GEAR SUN 1ST STAGE RED N PKAA000X702 3101647 01 BEARING BALL ANNULAR 0422826 3102336 01 SHAFT STUB COMPRESSOR FRONT RWAQ05A468 3102360 01 GEAR RING 2ND STAGE REDUCTION 94 T PKAA004A939 3107500 01 BEARING ROLLER FLANGED FC141266 3107504 01 BEARING ROLLER FL 3 14 X 5 23 X 760 FC142115 Pratt amp Whitney Canada Prat Whiney Ganada n ne s nite nologies A United Technologies Com Marie Victorin Liste des composants moteur num ros de s rie ne Uniad re FC Doe Longueui Qu bec Canada Engine Serialized Component Summary urere Page 2 P amp WC JR3 6830 E 05 1998 SEH Ka PCE PKOS94 Ers BS1024 N de fot pour trait i 3 x Code de trait N de s rie du e i i N du mat riel D signation du mat riel N de s rie i N de mat riel du fournisseur Material Number aterial Name Serial No thermique mat riel forg thermique Vendor Material No Heat Code Forging Serial Heat Treat Batch No 3109239 01 BUS BAR NEGATIVE TERMINAL T5 NR06139 3109240 01 BUS BAR POSITIVE TERMINAL T5 NR06115 3109766 01 COUPLING POWER TURBINE 007 467 KAVUU 3112117 03 BEARING BALL FC141011 3112214 01 WIRING HARNESS THERMOCOUPLE NR17920 3112368 01 BEARING ROLLER FLANGED 94X1 65X 47 0420940 FA0420941 FA0420947 FA0420948 FA0420949 FA0420950 FA0420951 FA0420965 FA0420966 FA0420978 FA0420979 FA0420
12. a Une soci t de United Technologies A United Technologies Company Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Longueuil Qu bec Canada J4G 1A1 Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel consulter le Manuel d entretien du moteur ou le Bulletin de service appropri selon le cas Note For determination of accumulated and remaining lives on this material refer ine Maintenance Manual or ulletin as applicable Temps de Temps de Der Num ro de s rie fonctonnement Cumul de cette installation Cumul jusqu pr sent instalation du du L mapun Mod le l enl vement Accumulated This Installation Total Accumulated To Date En Engine Module Model Eng Module Material Serial Number Material Temps Time Cycles Temps Time Installed Removed Observations Installation d entretien de r vision bon de travail et timbre du v rificateur Remarks Maintenance Overhaul Facility Work Order amp inspection stamp PCE PK0594 PT6A 60A Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est install e This record must be kept with the engine module logbook where this part is installed Historique du mat riel dur e de vie limit e Life Limited
13. at riel e Code de traitement thermique Pratt amp Whitney Canada Une soci t de United Technologies A United Technologies Company mis le A M J Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 1000 Marie Victorin Longueuil Qu bec Canada J4G 1A1 Nota Pour connaitre les dur es de vie accumul e et r siduelle du mat riel Donn es sur le moteur module Engine Module Data Donn es sur le mat riel Material Data Material Name Heat Code Issue Date Y M D consulter le Manuel d entretien du moteur ou le Bulletin de service DISC TURBINE LALBZ 2004 10 20 appropri selon le cas Num ro du mat riel Num ro de s rie du mat riel N de s rie du forg Temps de Cycles de Material Number Material Serial Number Forging Mat Serial Now tion fonction Note For determination of accumulated Time Since New Cycles Since New and remaining lives on this material refer 3029313 0011621 1395 0 0 to the engine Maintenance Manual or Service Bulletin as applicable 4 A Temes de i Temos de i Ob fonctionnement i fonctionnement servations i Num ro de s rie n Cumul de cette installation Cumul jusqu pr sent jon d 5 isi depuis depuis 1 Installation d entretien de r vision bon l installation du du morour
14. d Service Report Borescope Inspection PT6A 42 1 GENERAL Date 16 Oct 2013 PO Customer 13 0022 MTU BB WO 1135 13 Customer Beechcraft Augsburg Location Augsburg 49 0 3378 824 440 49 0 3378 824 371 49 0 176 10005903 marcel hellmann mtu de Report author Marcel Hellmann 49 0 2392 649 771 49 0 2392 649 772 49 0 172 872 2386 Dirk Brockhagen pwe ca Field Representative Dirk Brockhagen Engine Model PT6A 60A Unit Serial No 0594 TSN 1914 4 CSN 1621 TSO N A CSO N A TS HSI REPAIR unknown Date last HSI REPAIR unknown Date last Inspection unknown Type of Aircraft Hawker Beechcraft King Air350 Aircraft Registration unknown Aircraft Serial No FL 419 Engine Installation Right Hand Left Hand Single Installation PT6A 60A Date 17 Oktober 2013 PAGE 2 of 8 MTU Maintenance MTU Field Service Report b Maintenance Borescope Inspection PT6A 60A 2 Borescope Inspection Inspected Findings Reduction Gearbox Duct Assy Exhaust 5 System 3 Stage PT Blades 2 Stage PT Blades Vane Ring Assy PT Blades CT Shroud Segments Duct Assy Small Exit Vane Ring Assy CT Liner Assy CC Duct Assy Large Exit Liner Assy CC Inner Liner Assy CC Outer Gas Generator Case Fuel Nozzles Fuel Nozzle Tip Impeller Compressor 1st Stage Compressor Inlet Case Accessory Gearbox Engine Externals Engine Accessories LEO HL D D D BOCDISBSBIET S 0000 D OOOOOOOOOO0BO
15. e l aviation du pays d approbation pays 2 BON DE SORTIE AUTORISEE AUTHORIZED RELEASE CERTIFICATE 3 Num ro de suivi du formulaire Form tracking No Approving national aviation authority country TCCA 24 0078 SEE BLOCK 5 Transport Canada 4 Nom et adresse de l organisme agr Approved organization name and address Pratt amp Whitney Canada Cie Pratt amp Whitney Canada Corp 5 Bon de travail contrat facture Work order contract invoice 1000 Boul Marie Victorin P 0 4000240320 Pratt amp Whitney Canada Longueuil quebec Canada J4G 1A1 Une societe de United Technologies A United Technologies Company 7 Description 8 N de pi ce Part No 9 Admissible Eligibility de s rie de lot SeriaVbatch No 12 EtatAravall Status ark FREE TURBINE 3102700 01 VARIOUS PCE PK0594 MANUFACTURED TURBOPROP PT6A 60A Includes 5 0594 13 Remarques Remarks CANADIAN TYPE CERTIFICATE E 12 FAA TYPE CERTIFICATE E4EA THIS ENGINE CONFORMS TO ITS UNITED STATES TYPE DESIGN TYPE CERTIFICATE NUMBER E4EA AND IS IN CONDITION FOR SAFE OPERATION THIS ENGINE HAS BEEN SUBJECTED BY THE MANUFACTURER TO A FINAL OPERATION CHECK AND IS IN A PROPER STATE OF AIRWORTHINESS 14 Le pr sent bon certifie que les articles indiqu s ci dessus ont t construits conform ment Certifies that the items identified above were manufactured in conformity to xd des donn es de conception approuv es et qu ils peuvent tre utilis s en t
16. etermination of accumulated and remaining lives on this material refer to the engine Maintenance Manual or Service Bulletin as applicable Date Observations Installation d entretien de r vision bon de travail et timbre du v rificateur Remarks Maintenance Overhaul Facility Work Order amp inspection stamp PCE PK0594 PT6A 60A Ins rer le pr sent historique dans le livre du moteur ou du module la pi ce est install e This record must be kept with the engine module logbook where this part is installed Pratt amp Whitney Canada Cie Historique du mat riel a dur e de vie limit e Pratt amp Whitne nad Pratt amp Whitney Canada Corp Life Limited Material History Record 1000 Marie Victorin Une soci t de United Technologies A United Technologies Company Longueuil Qu bec Canada JAG 1 1 Num ro du dessin ST3582 01 Drawing Number ST3582 01 P amp WC JR3 6834 E 6834 1998 06 S 7 Nota Pour connaitre les dur es de vie D signation du mat riel Code de traitement thermique mis le A M J CCUML iduell iel Material Name Heat Code Issue Date MD consulter e Manuel entreen du moteur ou le Bulletin de service ROTOR COMPRESSOR REAR EPDDA 2004 10 20 appropri selon le cas Num ro du ma
17. ignation du mat riel N de s rie N de mat riel du fournisseur thermique mat riel for thermique i Material Number laterial Name Serial No Heat Forging Serial Heat Trost Batch No Vendor Material No 3022846 HE STAGE REDN 000 705 3022847 GEAR RING FIRST STAGE REDUCTION PKAA001A627 3023408 GEAR SUN 2ND STAGE RED N 46TEETH PKAA001A423 3023886 ADAPTER SPLN FIRST STAGE RDCN PKAA008A162 3024502 GEAR PLANET SECOND STAGE REDUCTION PKAA003A248 PKAA003A253 PKAA003A257 PKAA003A268 PKAA003A273 3027698 SHAFT POWER TURBINE RWA04A692 3028004 BEARING OPTION BB0037920 BB0038299 3029312 DISC TURBINE A001L6AB 3029313 DISC TURBINE 0011 621 3029699 CARRIER FIRST STAGE REDUCTION PKAA006A652 3029722 GEAR PLANET FIRST STAGE REDUCTION PKAA000P404 000 408 000 427 3034312 DISC COMPRESSOR ROTOR A001L3E7 3034313 DISC COMPRESSOR ROTOR A001L2M5 3034853CL01 VANE RING TURBINE BL215 3035563 CARRIER SECOND STAGE REDUCTION PKAA006A595 3035889 EXCITER IGNITION NNA04352053 3036640 FLOW DIVIDER amp PURGE VALVE 9959514169 3036793 IMPELLER CENTRIFUGAL EAAA000H502 3038252 VANE RING TURBINE E041 3040311 DISC TURBINE A001KWCY 3040760 PUMP FUEL 006958 3041271 ROTOR COMPRESSOR REAR TXA1A4739 3041861CL01 COMPRESSOR TURBINE STATOR ASSY OF 946A 3054481 01 SHAFT PROPELLER 0000232 3057249 01 HEATER OIL TO FUEL WA21197 3057250 01 GOVERNOR PROPELLER 13999184 3070268 01 LINER COMB CHMBR OUTER ASYO FTAA000A919 3100742 01 CO
18. oute s curit ZN Approved design data and are in condition for safe operation Certification apr s maintenance en vertu du RAC 571 10 Car 571 10 Maintenance relegse des donn es de conception non approuv es indiqu es la case 13 la case 13 a t effectu conform ment au Non Approved design data specified in block 13 Certifies that except where otherwise specified in block performed in accordance with CAR 571 6 N d agr ment d autorisation Certificate Approval 20 Signature autoris e Authorized signe P1 N d agr ment d autorisatian Certificate Approval Pei No Ref b 4 Te u 24 0078 12 09 2001 P amp WC 5720 2003 02 Le monteur doit contre v rifier l admissibilit avec les donn es approuv es Installer must cross check eligibility with approved data 1 Le pr sent document n autorise aucunement le montage de la pi ce 1 This document does not constitute authority to install the part 2 Si le monteur se base sur la r glementation nationale d une autorit de navigabilit autre que celle indiqu e la case 1 il doit s assurer que l autorit de navigabilit dont il rel ve accepte les produits ou les travaux de maintenance de l autorit de navigabilit indiqu e la case 1 2 Where the installer works in accordance with the national regulations of an airworthiness authority other than the authority specified in block 1 the installer must ensure that his her ai
19. pal THIS PAGE IS PROVIDED FOR INSERTION BETWEEN THE BINDER AND THE FIRST PAGE OF THE MANUAL IT WILL PREVENT THE PRINTED TEXT FROM ADHERING TO THE INSIDE BINDER COVER Index of Engine Documentation Engine Number PCE PK0594 Document Name Final Acceptance Test Record Sheet Engine Serialized Component Summary Life Limited Material History Record Life Limited Blades History Record when applicable Engine Build Record Status Report SB Engine Log Book Yellow Book Final Vibration Survey when applicable Authorized Released Certificate Form 24 0078 Date Note This index reflects the quantity of Shipping Documentation supplied with the engine Quantity of Documents Quantity of set X Quantity per set 1X2 N A Quantity of set X Quantity per set 1X 1 Note 1 copy or set is staple in the SB section of the Yellow Book if H E i October 20 2004 Issue Date June 10 2000 PRATT amp WHITNEY CANADA CORP 68 PROGRAM 4 3 32 0113 BUILD SPEC 1024 2004 OCT 20 TEST CELL ENGINE TESTED AND ACCEPTED IN ACCORDANCE WITH E amp TI FINAL VANE FLOW AREAS PROP SPEED S L S STD DAY POWER TSA TRIMMED T5D DERIVED GAS GEN SPEED SFC 8 18400 BTU LB LB SHP HR PRESSURE RATIO 8 36500 FIRST STAGE SECOND STAGE 393 1700 1700 1173
20. rworthiness authority accepts products or maintenance from the airworthiness authorily specified in block 1 3 Les nonc s des cases 14 et 19 ne constituent en aucune facon une certification du montage Dans tous les cas le dossier technique de l a ronef doit renfermer une certification de montage d livr e conform ment la r glementation de l tat d immatriculation et ce avant que tout vol puisse avoir lieu 3 Statements 14 and 19 do not constitute installation certification In all cases the aircraft technical record must contain an installation certification issued in accordance with the national regulations of Li Q 2 p 4 4 H LH MTU Maintenance Berlin Brandenburg Ein Unternehmen der MTU Aero Engines Maintenance Field Service Report Borescope Inspection PT6A 60A S N PK0594 Field Service Engineer Marcel Hellmann Reason for Inspection pre buy inspection Date of Site Visit 15 october 201 Issued by e UT Approved by Marcel Hellmann Jeanne Koitzsch Field Service Engineer Customer Support Engineer Mobile Repair Team SBPM Mobile Repair Team SBPM MTU Maintenance Berlin Brandenburg GmbH Sitz der Gesellschaft Gesch ftsf hrer Dr Ernst Zimmermann Str 2 Ludwigsfelde Andr Sinanian 14974 Ludwigsfelde Handelsregister Vorsitzender des Aufsichtsrats Tel 49 0 3378 824 00 Potsdam HRB Nr 1807 Dr Stefan Weingartner Fax 49 0 3378 824 300 www mtu berlin com MTU Maintenance Fiel
21. t riel Num ro de s rie du mat riel de s rie du mat forg Temps de Cycles de was Material Number Material Serial Number Forging Mat l Serial No fonction fonction Note For determination of accumulated Time Since New Cycles Since New and remaining ies on this material refer 3041271 TXA1A4739 65 0 0 to the engine Maintenance Manual Service Bulletin as applicable Donn es sur ie moteur module Engine Module Data Donn es sur le mat riel Material Data i Temps de 25008 de i Ob fonctionnement Num ro de s rie fonctionnement c i EEN servations depuis depuis umul de cette installation Cumul jusqu pr sent Installation d entretien de r vision bon de l installation du SR Mod le renl vement Accumulated This Installation Total Accumulated To Date Date travail et timbre du v rificateur Engine Modul Model Eng Modul Remark ine Module n ule M emarks SN When Engine Module TSN When Maintenance Overhaul Facility Work Matera ene Temps Time Cycles Temps Time Cycles Order amp inspection stamp nstalled f 0 PCE PK0594 PT6A 60A Ins rer le pr sent historique dans le livre du moteur ou du module o la pi ce est install e This record must be kept with the engine module logbook where this part is installed 1 Autorit d
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