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H1843L Beech 58P Baron, S/H: TJ-65 AIRCRAFT

1. 1000 26 14000 4p STATIC SYSTEM TESTED MA 0 7 16 000 6 STR 551 2013 Fe reste 35 FT 500 0 18 000 Sn encm 1 sno mmr JSK m 0 1000 20 20 000 __ 76 ALT 2 p SIN TESTED TO FES 1 500 2p 22 000 00 M A sin LC TESTED YO 2 000 22 25 000 40 TRANSPONDER 1 72 950 sn LS 2 3 000 3 30 000 TRANSPONDER 2 gt M 20 s r25 7 Eris 7 257 NENT DETAILS ARE ON FILE AT THIS REPAIR STATION Tak WOE ORDER f 19171 DATED 8 000 30 45 000 M LH THIS IS A PERMANENT LOGBOOK ETRY 10 000 4C 50 000 M AUTH 20 12 000 _ 30 SALT LAKE CITY UTAH ACSN 27 224 cd anu Alt Model 55205 jj paz S60 E LN au HN 7 1 i 418431 Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY January 11 2001 Aircraft Total Time 3 792 4 hrs Hobbs Reads 3 792 4 hrs Resealed the lefi wheel brake caliper Bleed left brake system and serviced brake reservoir with fluid meeting MIL H 5606 Royco 765A Ground operational check of brake system normal Work performed in accordance with Beech 58 58 series service manual and __ Cleveland wheel amp brakes service manual o N E AP147582140 DATE TOTAL TIME IN SERVICE REFERENCE OF MAJOR REPAIRS AND MAJOR ALTERATIO
2. condition 1 Addition o Removal of Requlred Exchanged for Optional equired Exchanged for Optional The following altimeter and altitude reporting equipment tests and inspections mM 77 E as required by FAR 91 411 IAW FAR Part ee E have been performed Part a Static System date Part h timeters Alof 7 520 Scales cur dis S N SIN e 20 aa Tested to 2 5 K feet _ DUNKIRK AVIONICS LLC FAA CRS DKZR372X ATC Transponder test arid inspections as required by FAR 91 413 FAR Part 43 PZN FSO been yw of Transponder Model 222 22 DUNKIRK AVIONICS LLC FAA CRS DKZR372X 22 105 aane rra GPS VER tl Fluti test Ste gt mere GPS Flight Test Completed 20 138 8 amem bine and FAR91 407 5 on file ct this under Salisfaclory unsatisfuctory date Cz Oc O3 Pins CNS vet OL RENE CCONSCS LLE FAA CRS DEZIO72X
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4. John E Caka AP147582140 t d 5 fadi Replaced forward and main batteries with new P N Installed G 25 S N Installed 0180 PW a L 1 amp G01797196 Ground Operational check of charging system normal Replaced d the fuel pressure sv A 2585 X THE lamp and auto pilot switch lamp with new 2 SPECTEDIN ACCORDANCE ___ ohn E APIATS2I40 Xp 0 FAA AND IS APPROVED FOR ___ 5 8 AlLS OF THE REPAIR ARE ON N1843L Beech 58 Baron S N 13 65 AIRCRAFT LOG ENTRY 5 T 18 1999 Aircraft Total Time 3 535 1 hrs t a 8 LA Poe Removed the flight director computer amplifier and sent to Century Flight Systems for inspect 2 a lt and repair Autopilot flight director computer amp P N 1D496 002102 S N 1812F reinstalled and st L system leak check and autopilot d ational check perfi d b Hay of En s Avioni ys and autopilot ground operational check performe by Steve pyden of g FOR Goud 1 DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS RECORDING 5 TODAYS TIME IN ENTRIES MUST BE ENDORSEO WITH NAME RATING AND CERTIFICATE NUMBER OF 1 TODAYS TIME IN ENTRIES MUST 19 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FO
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6. Mi843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY CONTINUED FROM PREVIOUS PAGE June 17 1996 Aircraft Total Time 3 090 1 hrs Hobbs Reads 3 090 1 hrs 19 5X6 75 8 S N Installed 60671961 Balanced wheel and tire assy and reinstalled Adjusted the left wain gear toe in to proper specs Replaced the left main landing gear brake linings with new units P N 066 04400 Replaced the airconditioner compressor drive belt with a new unit P N 642759 Replaced the left engine turbo oil reservoir scavenge oil return flex hose with new unit P N 131227F8 0264 Date code 3092 Replaced three 3 fuselage drain seals wit new units P N 50 420082 3 Repaired the left engine Low Thrust Detector System LTDS heater by replacing electrical ground wire terminal end i No wing bolt change at this time as per the tions of the wing bolts and fittings no defects ings Removed aircraft batteries serviced with charged batteries and reinstalled Serviced ight propeller unfeather accumulator precharges Serviced brake reservoir with fluid meeting MIL zens and drained sumps Checked all lights for 15 lubed landing gear Lubed uplock rollers Xil 636 lubricant Replaced the left and right italled two 2 new bushings P N 105739D 210250 1057398 0137 and two 2 new screws P N 35 nlock cable tension found satisfactory Reset id to proper specs Performed retraction and Switch operational check of landing gear system
7. Tet SAvaor BNIOV34 aasn 1N3Wdinos 30444 2 suomy sSuryr esu 5 ef paep sey oseayar 75 101991KT WS 814 woreg qgc 42298 1 5 52885 arvo tz AP147582140 AFT LOG ENTRY eling Adjusted left and right voltage regulators to iormal results Work performed in accordance with J ee CE E 47582140 7 Ky AND ALTERATIONS DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS 57 CERTIFICATE NUMBER OF TODAYS TIME IN ENTRIES MUST ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF AX HER SPECIFIC ENTRIES 19 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES i ENTRY N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY varranty repair Re March 13 1998 Aircraft Total Time 3 397 5 hrs Hobbs Reads 3 397 5 hrs 3 e P S I maintenance Performed compass calibration check Calibrated compass with all radios on Placarded deviation E Blk of flight director as follows 358 3 26 6 57 88 12 118 15 145 175 21 205 24 235 A ARS ck performed by Jim W 269 30 300 33 328 Straitened minor bend in rudder trailing
8. tcordanca with FAR 43 9 specified n block 13 or Attached above was with EAA aleworthiness requisitions and ia formed the part s ls are approved lor stive date left and cross check aligibiny with applicable technical data 12 freon A C Freon supply and recovery provided airconditioning system with normal results Work service manual EE CEE John E Caka AP1475821401A DATE 19 TIME IN RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS TACH TODAYS ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY September 26 1997 Aircraft Total Time 3 364 5 hrs Hobbs Reads 3 364 5 hrs Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par D a b c performed operational check of left and right switch functions with normal results This AD next due at aircraft total time 3 464 5 hours Complied with JanAero Devices formerly Janitrol Appliance AD 96 20 07 Combustion Heaters effective date 11 14 96 par a combustion tube and combustion air pressure switch tests satisfactory Current heater hobbs time 156 9 brs This AD note next due for the installed heater Model B3040 P N 82D20 1 Beech P N 102 384010 1 S N 2751198 at heater ho
9. DESCRIPTION INSPECTIONS TESTS REPAIRS AND ALTERATIONS RECORDING TOTAL TACH TODAYS TIME IN TIME FLIGHT SERVICE 18431 Beech 58P Baron S N Tj 65 AIRCRAFT LOG ENTRY CONTINUED FROM PREVIOUS PAGE June 17 1996 Aircraft Total Time 3 090 1 brs Hobbs Reads 3 090 1 hrs Conplied with Beech SI 0125 390 Calibration of T I T Indicating System replaced the left and right T I T probes with new units P N 86160 Recalibrated left and right indications Replaced the ELT battery with a neg unit Aviall FAA PHA P N BS2166 Performed the 12 month inspection requirements for E L T s as per FAR 91 207 in accordance with FAA Action Notice 8150 3 E L 1 Recommended Supplemental Inspection Procedure FAR Part 91 Operations No defects noted ELT Hake Narco Model ELT 10 S N 75731 Battery Expiration date June 30 1998 This inspection next ENTRIES MUST BE ENDORSED WITH RATING AND CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES due on or before June 30 1997 Note No record of wing bolt replacement found No wing bolt change at this time as per the owner operator s request Inspected the accessible portions of the wing bolts and fittings no defects evident Cleaned inspected and repacked all wheel bearings Removed aircraft batteries serviced with distilled water cleaned and neutralized battery box top charged batteries and reinstalled Servic
10. Engine installation performed in accordance with Beech 58P 58TC service manual and RAM installation instructions and drawings Installation approval is as per RAM Aircraft Corporation STC SA1207NW Inserted copy of FAA approved airplane supplemental flight manual dated April 1 1981 as amended October 28 ihe into the aircraft flight manual P O H sec FAA form 337 filed September 4 1999 for further details of alterations performed 4 CONTINUED ON NEXT PAGE Seplember 4 1999 Aircraft Total Tim Removed Hartzell model 6 6 3A 32C521 G82NLA propellers in the left and right positions of thi 14 Left Propeller S N 983957 Left Propeller Total Time at Insialil lt 118 3 81119 Right Propeller Model McCauley 2 52 1 installation 0 000 0 hrs 5 N A Right Prop Blade 5 E accordance with Beech 58I SSTC serv ice manual and RAM installat Corporation STC SA090225C 7 Installed Prop Guard Acrospsce Inc proted 5 installation instruction document FPLOOL CS1002 dated F ehrini Supplemental type cenificate SPOOS8INY Weight and balance cii n Air raft physically reweighed after all modifications we configuration Th following information was entered into the Weigh 4 388 Ibs New Bmpty Weight Momeni 325 329 1115 New Bi R Replaced th right engine pneumatic system air pump wit 1777448 Installed unit TSO 0000 0 hrs Repla
11. and neutralized battery box top charged batteries and reinstalled Serviced brake reservoir with fluid meeting MIL H 5606 Texaco 15 Serviced fuel strainer screens and drained sumps Checked Jights for proper operation Cleaned gaped and rotated spark plugs Drained left and right engine and replaced filters with new units Champion P N CH48108 left engine date code FO1M3I 1 right engine date code F07L29 1 inspected removed filters for abnormal contamination none found Serviced left and right engines with Phillips 20W50 Lubed flight and engine controls lubed landing gear Serviced all tires with air Lubed the left and right uplock downlock rollers with ASG 7 Cleaned inspected and repacked all wheel bearings Performed landing gear retraction and extension checks downlock tension rigging checks emergency extension checks and safety switch operational checks with normal results Complied with Raytheon Beech Executive Service Scries Communique 99 Announcement of Addition of Landing Gear Warning Test to Maintenance Manual Temp Rev 32 1 dated November 1999 as per communique instructions landing gear warning operation and safety operation normal Replaced the left and right pneumatic system inlet filters with new units P N D9 14 5 Replaced the left and right pneumatic system inline filters with new units P N 134 7 Replaced the airconditioner compressor drive belt with a new unit P N 642759 see Perf
12. PECTIONS TESTS REPAIRS AND ALTERATIONS WITH NAME RATING AND CERTIFICATE NUMBER OF ITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES FROM PREVIOUS PAGE ings replaced nose wheel bearing cup and cone IN 08125 Removed aircraft batteries serviced touched up battery box with acid proof paint top propeller dome charges Serviced left and right yrake reservoir with fluid meeting MIL H 5606 sumps Checked all lights for proper operation splaced the left main landing gear tire with a new Installed 80071845 Balanced wheel and tire d the nose landing gear steering yoke bolt with a xk downlock rollers with ASG 7 Performed tension check and safety switch operational check ssor drive belt with new unit P N 642759 f engine and aircraft systems with normal results aries service manual TCM TSIO 520 L LB WB ccordance with an ANNUAL inspection and was NO CaJohn E AP147582140 A RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY August 25 1998 Aircraft Total Time 3 450 0 hrs Removed flight director auto pilot computer for warranty repair and returned to Century Flight Systems Reinstalled flight director auto pilot computer
13. MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES NIB 3L Beech Baron S N 77 65 CONTINUED FROM PREVIOUS July 10 1998 Aircraft Total Time 3 449 3 hrs Cleaned inspected and repacked all wheel bearings replaced nose wheel bearing cup and cone pilots side with new units Cup P N 08231 and Cone P N 08125 Removed aircraft batteries serviced with distilled water cleaned and neutralized battery box touched up battery box with acid proof paint top charged batteries and reinstalled Serviced left and right propeller dome charges Serviced left and right propeller unfeather accumulator precharges Serviced brake reservoir with fluid meeting MIL H 5606 Texaco 15 Serviced fuel strainer screens and drained sumps Checked all lights for proper operation Lubed flight and engine controls lubed landing gear Replaced the left main landing gear tire with a new unit Goodyear Flight Custom 19 5X6 75 8 10 ply S N Installed 80071845 Balanced wheel and tire assy and reinstalled Serviced all tires with air Replaced the nose landing gear steering yoke bolt with a new unit P N 35 825005 Lubed the left and right uplock downlock rollers with ASG 7 Performed landing gear retraction and extension check emergency extension check and safety switch operational check with normal results Replaced the airconditioner compressor drive belt with a new unit P N 642759 Performed run up check and operational check o
14. TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING ANO CERTIFICATE NUMBER OF 19 FT LOG ENTRY ater Hobbs 156 9 hrs 1642 R 1 0 hrs 1811 53 0 hrs X ED761 1 9 hrs IN ED812 058 2 hrs with FAR part 91 409 a as per FAR part 43 or E L T sas per FAR 91 207 in accordance with applemental Inspection Procedure FAR Part 91 zl ELT 10 S N 75731 Battery Expiration date June 30 1998 te Alternators effective date 2 02 76 performed 5K000041 of alternator bearing bearing lube and ron SRI 2 lubricant Right alternator N A by next due for left alternator at aircraft total switches effective date 8 30 77 Par 1 a b c sions with normal results This AD next due at CONTINUED ON NEXT PAGE 1418431 Beech 58P Baron S N TJ 65 CONTINUED FROM PREVIOUS PAGE July 15 1997 Aircraft Total Time 3 314 2 hrs Complied with Raytheon Beech AD 97 09 09 Structural Cracking Longeron Inspection and Reinforcement effective date 6 30 97 par as per Beech SB 2630 no cracks or missing rivets found par b as per Beech SB 2691 Rev 1 Part 1 par 62 fabricated and installed longeron reinforcement as per Beech SB 2691 Rev 1 Part No further action required Note No record of wing bolt replacement found No wing bolt change at this time as per the owner operator s request Inspected the accessible portions of the wing bolts and fittings no defects evident Cleaned inspected
15. 24 ej Right Prop Blade S N s 2 158 091 12 57092 ohn E AP147582140 Performed ANNUAL t inspection in sith FAR NIBA3L Beech 58 Baron S N T 65 AIRCRAT OG 9 1 no Ni843L Beech 58 Baron S N 65 AIRCRAFT LOG ENTRY August 18 2001 Aircraft Total Time 3 900 7 hrs Hobbs Reads 3 900 7 hrs Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c performed operational check of left and T right switch functions with normal results This AD due at aircraft total time 4 000 7 hours switch fi Conil with mem AD Trid Queen Replaced ali spark plugs with new P N RHB32E for the left and right engines Serviced aircraft main batteries with distilled water cleaned ith normal resu be i f PE aj att E vices nitrol Appliance and neutralized battery box and top charged batteries Serviced brake reservoir with fluid meeting MIL H 5606 Royco 756A Serviced fucl strainer and leens and drained all sumps Checked all lights for proper operation Lubed exterior flight controls Lubed engine controls Lubed landing gear s tests combustion tube decay lest sat Bow the left and right uplock downlock rollers with Aeroshell grease ASG 7 Serviced all tires with Cleaned aircraft exterior engines and engine irent hobbs fime 158 Performed propeller
16. 40 0003 alt 24V150W Repaired magneto P Jead for the right 2liance with appliance AD 76 07 12 Magneto Switches effective date Jofin E Caka AP147582140 System Tracking Rel No ag lt 554 2 5 Work Order Contract or Invoice Number SAME AS 3 CRS amp CM2R747K anity 11 SeriayBatch Number 12 Status Work KE Lot l PERFORMED E 1 Accordance with FAR 43 9 specilied in block 13 attached above was ace with FAA airworthiness regulations and in formed the part s is are approved tor e 21 Certificate Number _ CM2R747K t led 23 Date d LA eee Central See lower motor id resealing a of Provo k performed pss check eligibility with applicable technical data S OR REPAIR FACILITY DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF TIME FLIGHT SERVICE SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY October 3 2000 Aircraft Total Time 3 777 7 hrs Hobbs Reads 3 777 7 hrs Left Engine Model T C M TSIO 520 WB S N 2741368 Left Engine Total Time 1 669 6 hrs T S O 215 0 hrs Right Engine Model T C M TSIO 520 WB S N 518721 Right Engine Tota
17. 02 7 Airwortbiness Alert for ECi Clasic Cast 7 d E Mane pund N A by new TCM RAM procesed cylinders installed at engine LN 1843L Beech 58 Baron S N TJ 65 AIRCKAFT LOG ENTRY April 8 2003 Aircraft Total Time 4 040 7 Hobbs Reads 4 040 7 brs ator noise filter clamp Retorqued right engine forward pan bolts Note Hobbs digit in the thousands place obscured Should reads 4 eld weld repair performed and reinstalled Replaced damaged rivnut Replaced left niain landing gear tire with new unit P N 301 361 311 Good Year 19 5x6 75 8 10PR S N Installed 30110371 cleaned and ine Replaced the left and right propeller spinner screws and washers wheel bearings and balanced assembly prior to reinstallation Removed lower oscillating beacon lens and inoperative lamp fwd replace lamp with aur and 100 hour functional checks and inspection with normal results new unit P N 70798 24 cleaned lens installed anti glare protection and reinstalled Replaced field switch for left ahernator P N 35 380053 7 Replaced aned and neutralized battery box top charged batteries and reinstalled lieft alternator field circuit breaker PN 524510 5 Replaced left voltage regulator with a serviceable unit P N B 00306 1 S N Installed 02444 Replaced el strainer screens und drained sumps Checked all lights for proper voltage r gulator perallcling wire with new wire meets 22759 16 18 MI
18. ED761 100 0 hrs S N ED812 1 193 3 brs ince with FAR part 91 409 a as per FAR part 43 5 for E L T s as per FAR 91 207 in accordance with Supplemental Inspection Procedure FAR Part 91 other defects noted ELT Make Narco Model July 31 2000 This inspection next due ou or Mite Alternators effective date 2 02 76 removed the alled left alternator P N ALV 9510 S N Installed ed right alternator P N ALV 9510R S N Installed jaintenance release forms for further detail of work er applies due to install alternator part numbers CONTINUED ON NEXT PAGE N1843L Beech 58P Baron S N TJ 65 CONTINUED FROM PREVIOUS PAGE July 10 1998 Aircraft Total Time 3 449 3 hrs Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c performed operational check of left and tight switch functions with normal results This AD next due at aircraft total time 3 549 3 hours Complied with Raytheon Aircraft Beech AD 97 25 01 Outflow and Safety Valves effective date 1 11 98 par a removed the outflow and safety valves and sent to AlliedSignal Aerospace for repair and modifications Installed outflow valve P N 103648 3 S N 124 283 and safety valve P N 103648 3 S N 44 265 after repair modification and overhaul Note Poppet date code for both valves 11 13 97 functional test date for both valves June 26 1998 No further action required Removed the flight director computer amplifier f
19. 1 234 0 brs 5 0 0 000 0 hrs Left Propeller Model McCauley 3AF32C521 C G 82NLA A S N 983957 Left Propeller Total Time 0 000 0 hrs 5 0 N A Left Prop Blade S N s 1 1086 2 SJ118 3 7119 Right Propeller Model McCauley 3AF32C521 C G 82NLA A S N 983955 Right Propeller Total Time 0 000 0 hrs 5 0 N A Right Prop Blade S N s 1 1091 2 7092 3 51112 Performed an ANNUAL inspection in accordance with FAR part 91 409 as per FAR part 43 appendix D P Performed the 12 month inspection requirements for E L T s as per FAR 91 207 in accordance with FAA Action Notice 8150 3 7 Recommended Supplemental Inspection Procedure FAR Part 91 Operations No defects noted ELT Make Narco Model ELT 10 SIN 831 ELT Battery Expiration Date July 31 2000 This inspection next due on or before July 31 2000 Verified compliance with Appliance AD 76 02 07 Prestolite Alternators effective date 2 02 76 found N A by alternator part auiinber es left and right alternators Left alternator P N ALV 9510 S N A 132260 and right alternator P N ALV 9510 S N A 100459 installed onio engines by RAM aircraft during engine build up Note AD note recurring inspection no longer required 7 Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c performed operational check of left and tight switch functions with normal results This AD next due at aircraft total time 3 662 7 hours Com
20. FI 65 AIRCRAFT LOG ENTRY January 4 2002 Aircraft Total Time 3 939 8 hrs Hobbs Reads 3 939 8 brs Replaced the left and right over voltage relays with new units P N 50 380048 1 Replaced the left over voltage sensor with a new unit P N 191002 Replaced the right over voltage sensor with a new unit P N B00305 1 S N installed 80191012 Replaced the left 306 2 5 installed 80293712 Replaced the right voltage regulator with a new unit P N B00306 2 S N installed cft ind right alternators for Y purposes Tostalled d overhauled alternator on the left side P N ALV9510 SIN d Maa Bonzer radar altimeter indicato and removed Alcor EGT wiring harnesses and probes Note EGT indicator previously removed luring radar altimeter reinstallation Installed J truments twin temperature indicating system EGT CHT TIT Engine Analyzer and associated llation manual Inserted light manual suppl ipplement into aircraft flight manual Twin e TERR ae system installation approval per JP STC SA00729S issued 8 31 99 see FAA form 337 filed 1 04 02 pe further details viis Change negligible updated aircraft equipment list to reflect current aircraft configuration rent aircraft basic em ht 4391 Ibs Weight ment 325 545 Ibs Current Empty Weight C G 74 14 7 Ground operational check of engine ini a ing system normal ES John E AP
21. GENERAL AVIATION MAINTENANCE RELEASE _ THE AIRORAF _________ of Salt Lake City Utah i APPLIANCE WAS REPAIRED AND INSPECTED IN ACCORDANCE ACTAE dai NS m WITH CURRENT REGULATIONS OF THE EAA IS APPROVED FOR ________ _ eck of engine and airera systems with normal results RETURN TO SERVICE PERTINENT DETAILS OF THE REPAIR ARE ON TC series service manual TCM TS1O 520 L LB WB FILE AT THIS STATION UNDER ztions ORDER DATE 7 H 22 SIGN e ORS KD6R661N P N xd in accordance with an ANNUAL inspection and was John E Caka AP147582140IA 4 TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS T TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF 3 3 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES Pn hien ELM SIRE HAE CEP ALE PELE ENP t ds Before FEAE ADES Bou UR GTR EAE CHEE DATE Wo RECORDING TIME TACH DE TODAYS TIME IN ENTRIES FLIGHT SERVICE MECHANI MU Yer KE LEE CE 58 Baron S N 1 65 AIRCRAFT LOG ENTRY August 25 1997 Aircraft Total Time 3 340 5 hrs Verified compliance with Priority Letter AD 97 16 10 Rapco In Line Pressure Filters effective date 7 31 91
22. IN TO SERVICE system in line filter with a new P N 174 7 Ground operational check of right side pneumatic system normal Work performed in accordance beh with Beech S8P S8TC series service manual and Rapco installation instruction checklist ZZ UU Title up EOTRR ELLE __ SERES ma y John E Caka AP147532140 ITA KANSAS N1843L Becch 58 Baron S N 1 65 AIRCRAFT LOG ENTRY Juno 21 2001 EE Evacuated freon air conditioning system and re serviced with R 12 Freon Certified Freon supply and recovery provided by Clay Liston of Provo Performed operational check of air conditioning system with normal results Work performed in accordance with Beech 58 58 a a CAZ John E Caka 147582140 i 1 65 AIRCRAFT LOG EN rRY uem 7 929 irs Hobbs Reads 3 9 N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY August 1 2001 Aircraft Total Time 3 855 6 hrs Hobbs Reads 3 855 6 hrs Performed functional check of stafl warning and fue vent heat operation with normal results Serviced right main landing gear strut with nitrogen to proper extension Complied with Appliance AD 2001 08 01 GanAero Devices Heater Fuel Regulator Valve Inspection effective date 5 10 01 found peed N A by affected component not installed John 147582140 E cf MIEASL Beech SBP Baron S N 17 65 AIRCRAFT LOG ENTRY ps gust 1
23. S N Installed 506 blower motor date code 11 99 Repaired the vent blower housing by gluing and resealing Evacuated freon airconditioning system and re serviced with R 12 Freon Certified Freon supply and recovery provided by Clay Liston of Provo i Performed operational check of airconditioning system with normal results AC vent outlet temp 63 deg F at O A T 85 deg F Work performed ccordance with Beech 58P 58TC series service manual z Book Entry _ 49 WOR 052612 icription of Work on Cip Naika Pt 2 279 00 wA SHTCRAFT INC GPR831D ature Cha TACH i with induction Air Filter Appliance AD 84 26 engine induction air filters with new units P N Verified cdmpliance with Raytheon Beech AD 2000 1 N A liy no clesntor skins replaced during the affected time period e Verified compliance with Raytheon Aircraft servi 7 Metal Bonded Elevator Assembly revision date 2000 fo nd N No record of wing bolt repiacement found No ble portions of the wing bolts and fittings defects evider 7 R plat d aileron trim iab Actuator tod bolts with new 8 crack in upper left skin Repaired taxi light Wiring Replaced lef right J hn AP147582140 FLIGHICRAFT 4 brs
24. and repacked all wheel bearings Removed aircraft batteries serviced with distilled water cleaned and neutralized battery box touched up battery box with acid proof paint top charged batteries and reinstalled i Serviced left and right propeller dome charges Serviced left and right propeller unfeather accumulator precharges Serviced brake reservoir with fluid meeting MIL H 5606 Texaco 15 Serviced fuel strainer screens and drained sumps Checked all lights for proper operation Lubed flight and engine controls lubed landing gear Replaced the right main landing gear tire with a new unit Goodyear Flight Custom II 19 5X6 75 8 10 ply S N Installed 70310906 Balanced wheel and tire assy and reinstalled Serviced all tires with air Replaced the left and right main landing gear center drag link bolts with new units P N 58 810017 5 Replaced the left and right uplock downlock rollers with new units P N NAS505 6J and lubed rollers with ASG 7 Replaced steering idler arm bushing with a new unit P N A779 Replaced the nose gear torque link bushings bolt and lower pin with new units as follows 4 each P N 060003 upper amp lower bushings 2 each P N 105740X ZL0104 center bushings 1 each P N 105739 0820 center thru bushing 1 each P N 130909B170 center bolt and 1 each P N 60 820029 3 lower pin Performed landing gear retraction and extension check emergency extension check and safety switch operational check with norma
25. found N A by no Rapco FAA PMA in line filters installed Airborne P N 174 7 installed left and right itioning system with 1 Ib of R 12 freon A C Freon supply and recovery provided Serviced aircond by Tunex of Provo Performed operational check of airconditioning system with normal results Work performed in accordance with Beech 58P 58TC series service E REL 7 John Caka AP 14758214014 N1843L Beech 58 Baron S N September 26 1997 Aircraft Total Complied with Appliance AD performed operational check of left an aircraft total time 3 464 5 hours Complied with JanAero Devic effective date 11 14 96 par com Current heater hobbs time 156 9 hrs P N 82D20 1 Beech P N 102 3 9 30 99 whichever comes first No Pressure Decay Test Replaced the left engine prie Installed RA 442CW 4 S N Installer Replaced the pneumatic system inlet fi line filter with a new unit P N 114 7 couplings with new units P N Serviced batteries with distil and serviced left and right propeller i propeller de ice system functional chi Repaired airconditioner com AN101319 tensioned belt to proper Rebushed left and right main gear to Performed run up check and oper performed in accordance with Beech 3 System Tracking No 3 stem Trac Is io ys 7 ER OF ITRIES 5 Work Order Contract Or inyoice Number 7 cud 12 Sutus Werk
26. with a new unit Goodyear Flight Custom II CONTINUED ON NEXT operational check of LTDS and LTDS heat system normal Deferred the aircraft auto pilot system Deactivated system by removing auto pilot control head and pulling the auto pilot circuit breaker in accordance with 91 203 Auto pilot removal and deferral performed by Avtronix of Provo Performed run up check and operational check of engine and aircraft systems with normal results Work performed in accordance with Beech 58P 58TC series service manual TCH TS10 520 L LB WB Operators manual X30505 and TCH Service Instructions I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in airworthy condition John E AP1475821401A E W1843L Beech 58 Baron S N 14 65 AIRCRAFT LOG ENTRY July 29 1996 Aircraft Total Time 3 124 3 hrs Hobbs Reads 3 124 3 hrs gt Adjusted flap travel approach limit switch operational check through complete flap extend and retract cycle normal 2E John E P1475821401A DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF 9 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES Hoverber 18 1996 A
27. 1 right filter date code FO8M12F 1 Complied with T C M service bulletin M94 2 Oil Filter Adapter Inspection dated 2 10 94 during filter change Serviced engines with Phillips 20W50 oil Performed propeller de ice system 50 hour polished propeller blade leading edges Ms Performed run up check leak check and engine propeller and aircraft systems ground operational checks with normal results Work performed in accordance with Beech 58P 58TC series service manual T C M TSIO 520 L LB WB Operators manual X30505 T C M Service Instructions McCauley acceptable and no looseness detected for the left and right engines functional checks and inspection with normal results Dressed and MPC 12 operators manual and RAM Aircraft Corp maintenance match Serviced fuel strainer screens and drained sumps Checked all fights for landing gear torque link and resafetied Repaired ie dva Verified compliance with Devices formerly 4 effective date 510 01 found N A by this AD note superseded by Jan Ach Inspection Mise eeu LIS ues 2217 Verified compliance with JanAero Devices formerly Janitrol effective date 9 11 01 found N A by affected type regulator and shut off C Verified compliance with Raytheon Becch AD 2002 10 13 with by placard installation as per Raytheon Deech Service Bulletin SB 11 3 Piston Issued June 2001 sce log entry dated 4 18 02 ELE Verified compliance wit
28. Aircraft Total Time 3 827 7 hrs Hobbs Reads 3 827 7 hrs 325 545 Ibs New Empty Weight C G 74 14 Replaced Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c performed operational check of left 5 0221 1 Removed emergency oxygen bottle assembly and sent out for and right switch functions with normal results This AD next at aircraft total time 3 927 7 hours acture Puritan Zepp Bottle Assembly P N ZC406 15 DOT 3AA1800 Drained left and right engines oil and removed filters inspected removed fillers for abnormal contamination found installed ydrostatic test in 5 year on or before January 31 2006 Removed the new FAA PMA oil fillers Champion P N CH48 108 tefi filter date code F02L29 1 right filter date code FO7L29 1 complied with service ng behind instrument panel Reinstalled previously removed Bonzer radar bulletin M94 2 Oil Filter Adapter Inspection dated 2 10 94 during filter change stud height acceptable and no looseness detected for the lett and Weight change between indicators negligible Updated aircraft equipment right engines Cleaned gaped and rotated all spark plugs for the left and right engines Serviced aircraft main batteries with distilled water cleaned smal Work performed ip accordance with Beech S8P 58TC series service and neutralized battery box and top charged batteries Serviced brake reservoir with Quid
29. Engine Model TSIO 520 WD SIN 274 136R Eef Tolal Time 1 669 6 hr Right Engine Model TS10 520 WB S N 518721 Right Engine Total Time 1 449 0 hrs Left Propeller Model McCauley 2 5 Left Propeller Total Time 215 0 hrs 7 5 NIA Left Prop Blade 5 57086 2 57118 3 57119 h Cauley 3AP32C521 C G 82N 5s ie 215 0 hrs N1843L Beech 58 Baron S N 65 AIRCRAFT LOG ENTRY August 15 2000 Aircraft Total Time 3 756 2 hrs Hobbs Reads 3 756 2 brs Drained all fuel sumps Performed engine run up check with normal results ze E AP147582140 EE e 1 51091 2 57092 3 52112 18431 Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY e quU n ah Dot Performed an ANNUAL Inspection in accordance wit 2 Performed the 12 month inspection requirements for zi 7 August29 2000 Aircraft Total Time 3 770 7 hrs Hobbs Reads 3 770 7 hrs IL T Recommended Supplemental Inspection Procedure PAR Part ELT Maker Narco Model BLT 10 S N 15731 BLT Batten Removed the auto pilot computer and sent out for repair Reinstalled auto pilot computer after repair by Autopilot Central Sce maintenance release tag and work order from Autopilot Central for details of repairs performed Replaced the aft aircondition r vent blower motor with a new unit P N 1523218 2
30. FAR Part 91 ans Operations Replaced ELT battery with a new unit no other defects noted ELT Make Narco Model El 5 gt ELT 10 S N 75731 ELT Battery Expiration Date July 31 2000 This inspection next due on ot M 52g before July 31 1999 PA ad 38 Complied with Appliance AD 76 02 07 Prestolite Alternators effective date 2 02 76 removed the a 55 and right alternator for inspection and repair Installed left alternator P N ALV 9510 S N Installed S E 4 pras 1080183 after overhaul by West Star Aviation Installed right alternator P N ALV 9510R S N Installed 88 8 8000005 after overhaul by West Star Aviation see maintenance release forms for further detail of work T UN E EN amp pmmeutiauc SI recien line filters with new units PIN No record owner operator s request Inspe CONTINUED ON NEXT PAGE TS l INSPECTIONS TESTS REPAIRS AND ALTERATIONS DRSED WITH NAME RATING AND CERTIFICATE NUMBER OF FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES DATE 19 RECORDING TOTAL DEBI OT Ur INSEES HONS Tenia meneame bee areena TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AN CERTIFICATE NUMBER OF TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES AFT LOG ENTRY Heater Hobbs 157 7 hrs 27642 R 88 1 hrs 241811 R 388 1 hrs
31. Inspection 1 pplian s tian Heater Fuel Regulator and Shut Off Valve ticed fuel strainer screens and drained sumps Checked all tights for MES cane this AD note seperate byllanAcro Devic Appl tires with air Lubed the left and right uplock downlock rollers with um cater Fuel Regulator and Shut Off Valve Inspection dined left and right engines oil and removed filters inspected removed with Jana shes AD 2001 17 13 Heater Fucl Regulatoi ampion P N CH48108 left filter date code FO6M26F 1 right filter tis found Walfected t 7 d previously complied dapter Inspection dated 2 10 94 during filter change stud height ers i AD 200 161 Door Placed date iens 4 ath Phillips 20W50 oil Performed Bulletin 58 11 3404 Placards and Markings Door Opening Placar leading edges tems ground operational checks with normal results Work performed Operators manual X30505 T C M Service Instructions McCauley lements gt ka AP147582140 propeller de ice system 50 hour crvice Bulletin SB 33 3452 Lights Electroluminescent Panel Retaleing Screw Inspection Issued May talled sce log entry dated 4 18 02 N1843L Beech 58 Baron SIN T5 65 AIRCRAFT LOG ENTRY CONTINUED December 6 2002 Aircraft Total Time 4 034 5 with Phillips 20W50 Lubed flig
32. M TSIO 520 WH S N 2741368 Left Engine Total Time 1 926 4 hrs T S O 471 8 hrs Right Engine Model TSIO 520 WB S N 518721 J Right Engine Total Time 1 705 8 brs T 8 05 47158 d Left Prop tler Model McCa ley 3Ai 32C521 C G B2NLA A S N Left Propeller Total Time 471 8 hrs N A Left Prop Blade S N s 41 8086 F2 5118 3 5119 Right Propeller Model McCauley F32C521 C G 82NLA A Right Propeller Total Time 471 8 hry T S O N A E Right Prop Blade S N s 1 SJO91 2 51092 ipe 5 s lobbs digit ia the acc obscured Reads 4 _ 1 b c performed operational check of left and Tights Notel in pA with Donat DC performed the 12 month inspection requirements for Recommended Supplemental Inspection Procedure PAR 91 Opera ion ELT Make Narco Model ELT 10 S N 25731 ELT Battery Expiration with Appliance AD 76 07 12 Magneto switches Verified compliance with Raytheon Beech AD 2002 11 07 Electroluminecent Pane Screw Inspection effective date 7 5 2002 found previously ndi f nctlons with normal results This AD duc at complied with by compliance with Raytheon Beech Service Bulletin SB 33 3452 Lights Electroluminescent Panel Retaining Screw Inspection Issued 2001 found N A by affected type panel screw not installed Performed 50 hour servicing Removed aircraft batt
33. P N 1D496 002002 S N 1812F after repairs Performed static system leak check with satisfactory results Performed auto pilot ground preflight operational checks with normal results LE Comm Caka APTATSS21AOIA N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY October 18 1998 Aircraft Total Time 3 503 5 hrs Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c performed operational check of left and right switch functions with normal results This AD next due at aircraft total time 3 603 5 hours Complied with Beech service bulletin 2670 Fuel Selector Placard Install by installation of required placard Lubed all flight control hinges Checked and serviced left and right propeller dome pre charges and unfeather accumulator pre charges Performed propeller de ice system functional check with satisfactory results Serviced all tires with air Repainted the right engine inboard and outboard cowling door upper white area and right side forward lower fuselage area near the propeller ice shield white matching color Performed run up check and operational check of engine and aircraft systems with normal results Work performed in accordance with Beech 58P 58TC series service manual 227 Cohn AP147582140IA i jesse po DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS T
34. REG N1843L 590 02 05 01 FHM3809 4 REINSTALLED LANDING GEAR BOX MOTOR P N 95 810017 23 S N ALG 4359 AFTER REPAIR BY AERO ELECTRIC CRS NV2R045L INSTALLED NEW L H MAIN L G GEAR UPLOCK CABLE ASSY P N 106 810011 1 AND CABLE PRESSURE SEAL P N NAS302 33 0404 ADJUSTED L G CABLE TENSIONS AND RIGGED IAW 58P M M CHAPTER 32 30 00 REF RAS WO 04 01 3815 OVER RETURN TO SERVICE Title albspeorar Certified Repair Station tBWVR672C RAYTHEON AIRCRAFT SERVICES INC Box 9162 WICHITA KANSAS 18210 2 E i sawat mowina uno senvo santo WO Lammi muii eve Laz saduy Gevieav Of Trony DEF vam pr oni E RED 9101001777 mies leone ADS W REPAIRS AND DATE TOTAL WORK eu V NUMBER ARS THE E TIME IN REFERENCE OF MAJOR REPAIRS AND MAJOR ALTERATIONS TO S 19 SERVICE FAA FORM ACA 337 BY DATE OR TO THE WORK ORDER NUMBER AND THE APPROVING AGENCY RY i 5 3 800 4 hrs Ni843L Beech 58P Baron S N 11 65 AIRCRAFT LOG ENTRY dual control yoke net exchange weight increase 3 Ibs 72 0 March 9 2001
35. Right Engine Total Time 2 269 0 hrs T S O 1 253 0 hrs Left Propeller Model Hartzell PHC J3YF 2UF S N ED761 Left Propeller Total Time 3 314 2 hrs 5 0 564 9 hrs Right Propeller Model Hartzell PHC J3YF 2UF S N ED812 Right Propeller Total Time 3 314 2 hrs T S O 1 058 2 hrs Performed an ANNUAL inspection in accordance with FAR part 91 409 a as per FAR part 43 appendix D Performed the 12 month inspection requirements for E L T s as per FAR 91 207 in accordance with FAA Action Notice A8150 3 E L T Recommended Supplemental Inspection Procedure FAR Part 91 Operations No defects noted ELT Make Narco Model ELT 10 S N 75731 Battery Expiration date June 30 1998 This inspection next due on before June 30 1998 Complied with Appliance AD 76 02 07 Prestolite Alternators effective date 2 02 76 performed visual inspection for left alternator P N ALV9407 S N 6K000041 of alternator bearing bearing lube and shaft end no defects noted Lubed bearing with Chevron SRI 2 lubricant Right alternator by alternator P N ALV9510R S N 85000005 This AD next due for left alternator at aircraft total time 3 414 2 hrs Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 performed operational check of left and right switch functions with normal results This AD next due at aircraft total time 3 414 2 hours CONTINUED ON NEXT PAGE TOTAL DESCI R
36. TRIO 661 py 12925 9 1 uoieq 485 42998 IEV8IN El HYL arva DINVHOSW 3214335 AW SalulN3 NI AWIL SAYQOL 1953 WLOL 1 M d Ee E qj 4667 199092901 viOricScLpldv A TYO 2225 22 zO peuoperado Ajayeg MU PM 8010105 101281191 5521781 510110 pooedoy z 6Lc WEL 18301 Merov 1661 11 1990120 AWINH DOT L4VuOuIV S9 LL N S uoreg 485 42224 IEPSIN CSALNI 21312345 YIHLO 3994 XDY8 33 4 DINVHOaW 3214335 30 317514432 QNY ONYX 3WYN 5 38 1501 5318143 NI 3WIL SNOILVNiilV 61531 SNOIL23dSNI 40 491813553 ONIGsODaY x Home of Gold Medallion Instruments The Professional Choice VIOPICSSLpldV EXE 9 L DE punou 8 ISI qons Jo x 1 8 ye Ap peirdew 088 N S 1 aeu Bugy ap peoejdew payoune oser LTT N S 126104 parredox e 514 688 speog SqqoH 514 6 DOT LAV eos OrIC8SLPIdV Vou g uyor 5 iun D ai AND oe dies jo Suoy ss
37. a b c performed operational check of and right switch functions with normal results This AD next due at aircraft total ime 3 824 0 hours Serviced batteries with distilled water and top charged Lubed all flight control hinges Performed propeller de ice system functio check with satisfactory results Serviced all tires with air Performed run up check and operational check of engine and aircraft systems with no results Work performed in accordance with Beech 58P 58TC series service manual TCM TSI L LB WB Operators mamal X30505 TCM Service Instructions FE Jobn AP147582140 RECORDING 5 rorat eo pesERIPT PACH 7 TODAYS TIMETN ENTRIES MUST FLIGHT SERVICE MECHANIC N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY July 14 2000 Aircraft Total Time 3 729 4 hrs Hobbs Reads 3 729 4 hrs Replaced the upper flashing beacon lamp with a new unit P N 40 0003 alt 24V150W Repaired magneto P lead for the right 1 engine left magneto and performed operational check of mag switch by compliance with appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1Y a b c both engine mag switches functions normal This AD next duc at aircraft total time 3 829 4 honrs E 2 L E Caka AP147582140 o N18431 58P Baron October 312000 Aircraft Total Time 3 7777 hrs Hobbs Reads
38. compres left engine turbo oil reservoir scavenge oil code 3092 Replaced three 3 fuselage drain engine Low Thrust Detector System LIDS he operational check of 170 and LTDS heat syster Deferred the aircraft auto pilot syster and pulling the auto pilot circuit breaker j deferral performed by Avtronix of Provo Performed rum up check and operational Work performed in accordance with Beech 58P 58 manual X30505 and Service Instructions I certify that this aircraft has been deternined to be in airworthy condition L 91843 Beech 58P Baron S A TJ 65 AIRCRA July 29 1996 Aircraft Total Time 3 124 3 h Adjusted flap travel approach linit s retract cycle normal ANSPECTIONS TESTS REPAIRS AND ALTERATIONS JRSED WITH NAME RATING AND CERTIFICATE NUMBER OF FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES ERY CONTINUED FROM PREVIOUS Reads 3 090 1 hrs of T I T Indicating System replaced the left alibrated left and right 7 1 7 indications ll FAA PHA P N BS2166 Performed the 12 month 1 in accordance with FAA Action Notice 8150 3 FAR Part 91 Operations No defects noted ELT tion date June 30 1998 This inspection next RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESYS REPAIRS AND ALTERATIONS TACH TODAYS IME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES
39. edge upper corner and inspected n 5 Ei 2 vund pum a ie E for cracks none found MEE rat e 9 _ 5 lol 3 EN XP147582140 7 E AP147582140 g N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY 5 c gt April 30 1998 Aircraft Total Time 3 419 6 hrs Hobbs Reads 3 419 6 hrs Re 5 Bd G ENTRY Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c he rformed in accordance performed operational check of left and right switch functions with normal results This AD next due at ur aircraft total time 3 519 6 hours z T 74 m Complied with Appliance AD 76 02 07 Prestolite Alternators effective date 2102176 performed visual inspection for left alternator P N ALV9407 S N 6K000041 of alternator bearing bearing lube and shaft end no defects noted Lubed bearing with Chevron SRI 2 lubricant Right alternator N A by alternator P N ALV9SLOR S N 85000005 This AD next due for left alternator at aircraft total time 3 519 6 hrs Complied with Beech AD 98 04 24 Severe Icing Conditions effective date March 13 1998 par a 1 2 inserted copy of AD note into the limitations section and the normal procedures section of the aircraft flight manual Serviced batteries with distilled water and top charged Lubed all flight control hinges Checked and serviced lett and right propeller dome pre charges and unfeather accumulator pre charges Performed pr
40. jn tine fillers with new units P N 1J4 7 Replaced the airconditioner compressor drive belt with a new unit P N 642759 Replaced the aft nav light lens with a new unit Replaced the left and right T I T probes with new unils P N 86160 and new gaskets P N 70354 performed T 1 T calibration as per Beech service instruction and Alcor Alcal calibration system instruction manual Replaced the nose landing gear tire with new unit Goodyear Flight Custom 5 00 5 6 ply S N Installed 83221578 balanced nose wheel and tire assy and reinstalled Note No record of wing bolt replacement found No wing bolt change at this time as per the owner operator s request Inspected the accessible portions of the wing bolts and fittings 20 defects evident Cleaned inspected and repacked all wheel bearings replaced nose wheel bearing grease seals Removed aircraft batteries serviced with distilled water cleaned and neutralized battery box top charged batteries and reinstalled Serviced brake reservoir with fluid meeting MIL H 5606 Royco 756A Serviced fuel strainer screens and drained sumps Checked all lights for proper operation Lubed flight and engine controls Lubed landing gear Lubed the left and right uplock downlock rollers with ASG 7 Serviced all tires with air Performed landing gear retraction and extension check emergency extension check and safety switch operational check with normal results Performed run up check and operational ch
41. meeting MIL H 5606 Royco 756A Serviced fuel strainer screens and drained sumps Replaced the right inboard fuel tank sump drain valve with new unit Curtis P N CCA3400 Checked all E ura lights for proper operation Lubed exterior flight controls Lubed engine controls Lubed landing gear Serviced all tires with air Lubed the ohn AP147582140 left and right uplock downlock rollers with Acrosbell grease ASG 7 Performed run up check leak check and engine and aircraft systems ground operational checks with normal results Work performed in accordance with Beech 58P 58TC series service manual T C M TS10 520 L LB WB Operators manual X30505 T C M Service Instructions AK TOTAL i inte i 1 S N 11 65 REGE NIS4AL 5 and RAM Corp maintenance tips and manua supplements 522 EART Cohn E AP147582140 N 95 8 10017 23 S N ALG 4359 AFTER REPAIR N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY DNE L H MAIN LG GEAR UPLOCK CABLE ms April 17 2001 Aircraft Total Time 3 836 0 hrs Hobbs Reads 3 836 0 hrs SEALI IN NAS302 33 0404 ADJUSTED L G i Replaced the right pocumatic system air pump with a Rapco Inc overhauled unit P N Installed RA 442CW 4 S N Installed 32 30 00 REF RAS WO 04 018815 75489 installed TSO 0000 0 hrs Replaced the right pucumatic system inlet filter with a new unit P N D9 14 5 replaced the right pneumatic __
42. meeting MIL H 5606 Royco 756A Serviced fuel strainer flight controls Lubed engine controls Lubed landing gear iced all res with air Cleaned aircraft exterior engines and engine dl checks and inspection with normal results for the left and right aft systems ground operational checks with normal results Work ISIO 520 L LB WB Operators manual X30505 T C M Service ance tips and manual LL Caka 1475821 m N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY October 5 2001 Aircraft Total Time 3 929 9 brs Hobbs Reads 3 929 9 hrs qm Replaced the right horizontal stabilizer de ice boot with new unit P N 25S 7D5057 08 S N MT11620 Cure Date June 2001 functional check of aircraft de ice systems with normal results Serviced brake reservoir with fluid meeting MIL H 5606 Royco 756A Work per Ped in accordance with Beech 58P 58TC series service manual and B F Goodrich Installation Maintenance and Repair Manual for Pneumatic De Icers 30 10 _ 31 and instruction sheet 13001 Installation Procedure for Pneumatic De icers LE EGE _ 7 John E AP147582140 NI843L Beech 58 Baron S N TI 65 AIRCRAFT LOG ENTRY November 17 2001 Aircraft Total Time 3 936 3 brs Hobbs Reads 3 936 3 hrs Left Engine Model T C M 510 520 S N 274136R Left Engine Total lime 1 828 2 brs 5 0 373 6 hrs Right Engine Model TSIO 520 WB S N 518721 Ri
43. the propeller biade blade track Performed propeller de ice system 50 hour and 100 hour 1 tum Reparalleled alternators Replaced taxi light lamp with E 3 right engine induction air box support bracket Overhauled shimmy i master cylinder Repaired and repainted right forward fuselage area gs Removed aircraft batteries serviced with distilled water cleaned i oir with fluid meeting MIL H 5606 Texaco 15 Serviced fuel strainer ind rotated spark plugs Drained left and right engine oil and replaced it engine date code F07L29 1 inspected removed filters for abaormal ubed flight and engine controls lubed landing gear Serviced all tires inspected and repacked all wheel bearings Performed landing pear checks and safety switch operational checks with normal results ncement of Addition of Landing Gear Warning Test to Maintenance inding gear warning operation and safety operation normal Replaced 3 the left and right pneumatic system inline filters with new units P N 79 systems ground operational checks with normal results Engines meets nce with Beech 58P 58TC series s rvice manual T C M TSIO 520 operators manual and RAM Aircraft Corp maintenance tips and manual performed by John ANNUAL INSPECTION and was determined to be airworthy m 2 1475821401 wiring harnesses and probes in accordance with Pl 1843 Beech 58 S N
44. 0IA RECORDING TACH TIME TOTAL TIME IN SERVICE DESCRIPTIO ENTRIES MUST BE MECHANIC OR RE TODAYS FLIGHT N1843L Beech 58P Baron S N TJ 65 AIRCE March 22 1997 Aircraft Total Time 3 242 5 hi Complied with Appliance AD 76 02 07 Pre visual inspection for left alternator P N ALV9407 S shaft end no defects noted Lubed bearing with C alternator P N ALV9510R S N 85000005 This time 3 342 5 hrs Complied with Appliance AD 76 07 12 May performed operational check of left and right switch f aircraft total time 3 342 5 hours Repaired the left 9 JES with MS20470 4M 3828 neutralized battery boj and tight propeller dd 8 i Replaced the right BE p hydraulic brake reservi Ei E Performed run up El K performed in accordarj 8 5 E RECS lt B lt 228 5 5 a 8 RS Bl gg V J 68 eo 3 R eu 5 3 3 Z Bs Bg F E BS 84 lt 4 B E iss iSED WITH NAME RATING AND CERTIFICATE NUMBER OF TACH TODAYS TIME IN ENTRIES MUST ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS CILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES 19 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SE
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46. 147582140 3 718431 58 Baron S N 11 65 AIRCRAFT LOG ENTRY _ o um August 13 2002 Aircraft Total Time 3 997 0 hrs Hobbs Reads 3 997 0 hrs Left Engine Model T C M TSIO 520 WD S N 274136R Left Engine Total Time 1 888 9 hrs 5 0 434 3 hrs Right Engine Model T C M TSIO 520 WB S N 518721 Right Engine Total Time 1 668 3 hrs T S O 434 3 hrs Left Propeller Model McCauley 3AF32C521 C G 82NLA A S N 983957 Left Propeller Total Time 434 3 hrs T S 0 N A Left Prop Blade S N s 1 57086 2 571 18 3 57119 Right Propeller Model McCauley 3AF32C521 C G 82NLA A S N 983955 Right Propeller Total Time 434 3 hrs 5 0 N A Right Prop Blade S N s 1 51091 2 57092 3 57112 Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par switch functions with normal results This AD next due at aircraft total time 4 097 0 hours Verified compliance with Raytheon Becch AD 2002 10 13 Cabin Door Placrd Installation effective date 7 08 2002 found previously complied on with by placard installation as per Raytheon Beech Service Bulletin SB 11 3404 Placards and Markings Door Opening Placard Modifications for Pressurized Piston Aircraft issued June 2001 Baron SINT TISS ENTRY December 6 2092 Aircraft Total Time 4 034 5 hrs Hobbs Reads Left Engine Model T C
47. 4 2001 Aircraft Total Time 3 895 3 hrs Hobbs Reads 3 895 3 hrs hd 5 ft Engine Model TSIO 520 WB S N 2741368 ED November 17 2001 Aircraft Total Times 3 936 31 hrs Hobbs Read Lefi Engine Model TS1O 52 SIN 2741366 Left Engine Total Time 1 787 2 hrs T S O 332 6 hrs Left Engine Total Times 1 828 2 hrs 5 0 373 6 hrs Right Engine Model T C M TSIO 520 WB S N 518721 Right Engine Total Tine 1 566 6 his T S 0 332 6 hrs gine T C M TSIO 520 WH S N S187211 Drained left and right engines oil and removed filters inspected removed filters for abnormal contamination none fc insta Times 1607 6 A ound led imei 1 607 6 hra T S O 373 6 hrs new FAA PMA filters Champion P N CH48108 left filter date code FOSLOI 1 righ filter date code FO7L29 1 complied with T C M service peerd 1 2 C G B2NLA A SIN bulletin M94 2 Oil Filter Adapter Inspection dated 2 10 94 during filter change stud height acceptable and no looseness detected for the left and j right engines Serviced engines with Phillips 20W50 oil RAM recommendation Performed run check jeak check and engine and aircraft m systems ground operational checks with normal results Work performed in accordance with Beech 58P 58TC series service manual TSIO 520 L LB WB Operators manual X30505 T C M Service Instructions Alem Corp maintenance Upo ned
48. 92680 id a new Unit and repaired alternator ignition tinit and sent to Aircraft Ground operational check of hentenn water cleaned and neutralized batieg Performed ground ni i accordance with Beech SES NIB43L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY November 29 1999 Aircraft Total Time 3 618 1 hrs Hobbs Reads 3 618 1 hrs Performed 50 hour servicing and Iubrication requirements as per Beech 50 58 series service manual NEC S distilled water and top charged Lubed all flight control hinges Performed Serviced all tires with air Checked lights for proper operation Performed Operators manual X30505 and TCM Service Instructions Serviced batteries with propeller de ice system functional check with satisfactory results ground run up and leak check and operational check of engine andi aircraft systems with normal results Work performed in accordance with ye series service manual TCM TSIO 520 L LB WB 467 ABL JE im E Caka API47582140 e ii PIRE AHORA aeii riti e P SN D and ight s itch functions with normal results This AD next due a Performed 50 hour servicing aad lubrication as per A Complicd with AD 76 07 12 Magneto sw Serviced batteries with distilled water andi t p charged ALTERATIONS LOGBOOK ENTRY NUMBER OF R SPECIFIC ENTRIES Field Airport C
49. A 94520 5615 2100 925 676 5580 FAX sas 42199 SSS N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY March 24 2000 Aircraft Total Time 3 625 2 hrs Hobbs Reads 3 625 2 brs Complied with Appliance AD 76 07 12 Magneto switches effective and right switch functions with normal results This AD next duc at aircraft total time 3 125 2 hours Replaced the left and right main landing gear brake discs with new units P N 164 66 Replaced the left and right brakc lin with new units P N 066 04400 Replaced the left main landing gear tire with a new unit Goodyear Flight Custom Il 19 5 6 75 8 10 ply 301 361 311 S N Installed 92680181 Replaced the left tire tube with a new unit Balanced left wheel and tire assembly and reinstalled Repl dyear Flight Custom II 19 5X6 75 8 10 ply 301 361 311 S N Installed 92711 Replaced the right tire tube with new unit Balanced right wheel and tire assembly and reinstalled Replaced the left alternator noise filter Replaced the combustion air heater fuel solenoid valve with a new unit P N 85042 1 Removed h Hed repaired combustion heater ignition unit P N date 8 30 77 Par 1 2 b c performed operational check of the right main landing gear tire with a new unit Goo a new unit and repaired alternator wiring ignition unit and sent 0 Aircraft Heating amp Electrical for repair reinstal Ground operational check of heater normal Cleaned insp
50. ACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF 19 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY November 4 1998 Aircraft Total Time 3 507 7 hrs Verified compliance with Parker Hanifin Corp appliance AD 98 23 01 Dry Air Pumps effective date October 29 1998 found N A by no affected pump couplings installed currently installed air pumps SIN 60508 Left and S N 60506 Right both overhauled by Rapco Replaced the right engine 6 E Cc G T probe with a new unit P N 86255 S N Installed 9839 ohn E AP147582140 KINGS AVIONICS INC _ 4 THIS 15 A PERMANENT LOGBOOK ENTRY 1 Lesbos et Gels Annne edet Re sortalhd factory Ve pa ad North star vac Ground ested turf Se dA a pound fer FILE AT THIS STATION UNDER GENERAL AVIATION MAINTENANCE RELEASE X THE AIRCRAFT 1 APPLIANCE WAS REPAIRED AND INSPECTED IN ACCORDANCE WITH CURRENT REGULATIONS OF THE FAA AND IS APPROVED FOR __ RETURN SERVICE PERTINENT DETAILS OF THE REPAIR ON CRS KD6R661N ORDER 224 6 DATE Z wa 7 _ E REF GPS REmeveo SENT ner PEPI BEwWsTA OPS ek or 2065 Avzona PLY TS
51. E BACK PAGES FOR OTHER SPECIFIC ENTRIES IRE CONTINUED FROH PREVIOUS NIS43L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY ig Reads 3 191 8 hrs p TT March 22 1997 Aircraft Total Time 3 242 5 hrs Hobbs Reads 3 242 5 brs 9r Mightened airconditioner compressor belt D Complied with Appliance AD 76 02 07 Prestolite Alternators effective date 2 02 76 performed 1 8 6000 3 4 hose visual inspection for left alternator P N ALV9407 S N 6K000041 of alternator bearing bearing lube and _ mit P N Installed 646275 N Installed 0 shaft end no defects noted Lubed bearing with Chevron SRI 2 lubricant Right alternator N A by DOL7801 98 Starter S N DO47801 98 150 at alternator P N ALV9SIOR S N 85000005 This AD next due for left alternator at aircraft total 7 5 ope time 3 342 5 hrs Data nd aircraft systems with normal results Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c service NES performed operational check of left and right switch functions with normal results This AD next due at aircraft total time 3 342 5 hours john Caka APLA758214014 Repaired the left nacelle trough panel P N 102 980000 7 by patching with 304 stainless steel fastened with 520470 4 monel rivets Serviced batteries with distilled water and top charged Cleaned and neutralized battery box Lubed all flight
52. ECORDING TACH TODAYS TIME IN ENTRIES MU TIME FLIGHT SERVICE MECHANIC 1 N1843L Beech 58P Baron S N TJ 65 July 15 1997 Aircraft Total Time 3 314 Complied with Raytheon Beech AD Reinforcement effective date 6 30 97 par a b as per Beech SB 2691 Rev 1 Part par t Beech SB 2691 Rev 1 Part No further acti Note No record of wing bolt replace owner operator s request Inspected the accessit Cleaned inspected and repacked distilled water cleaned and neutralized batter charged batteries and reinstalled Serviced left propeller unfeather accumulator precharges Texaco 15 Serviced fuel strainer screens an Lubed flight and engine controls lubed landing unit Goodyear Flight Custom II 19 5X6 75 8 assy and reinstalled Serviced al tires with air link bolts with new units P N 58 810017 5 units P N NASSOS 6J and lubed rollers with A P N A779 Replaced the nose gear torque lin 4 each 0601003 upper amp lower bushings P N 105739X YG0820 center thru bushing 820029 3 lower pin Performed landing gear and safety switch operational check with normi ee EE AEN AM ACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES 4 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES REPAIRS AND ALTERATIONS DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS 1 ME RATING AND CERTIFICATE NUMBER OF 5
53. ERKO n 3 T UNITED STATES 2 4 Organization FAA CRS PKOSRG6IN FAX 801 355 6445 Po 6 tem 5 Part Number charged 2 i 13 Remarks Secon IRE Mot this se Limited on parts must be accompanied by maintenance history includ 7 97 New Overhaul O service Certifies that the new or newly overhauled part s Identified above 5 otherwise specified in block 13 was were manufactured In accordano with FAA approved design date and alrworthiness time 33 importing country have been met Note In case ot part to be exported the special requirements of the 15 Signature 16 FAA Authorizal E 3 17 Name Typed or Printed 1843 FAA Form 8130 3 g x E a _________ as Replaced forward and gt amp 601797196 Ground Operatit 55 lamp and auto pilot switch lampy x t Bea MEINE cide aS rag 885 NI843L Beech 58P Sf as May 18 1999 Aircraft Total Removed the flight direc and repair Autopilot flight system leak check and autopilot gt S 4 3 5 1 TRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERAT UST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CE
54. Flight Controls Flap Flex Shaft Cable Assembly Inspection Replacement Issued September 3 ME nas Vlt pitis nona picis t 5 2 SIN instal 93712 2001 found N A by 20 shaft replacement during the affected time period 80293603 Swaped the Te and right ahernators T r trouble Complied with TCM SB M84 15 Cylinder Leak Check dated 12 21 84 for the left and right engines with the following results Left engine 3 2 000010 Ref s T dvi oe row ng purp cylinders 1 75 80 2 75 80 3 73 80 4 71 80 5 77 80 6 76 80 Right engine cylinders 1 79 80 2 76 80 3 74 80 44 77 80 5 78 80 6 Inspection UM installed right side alterna 16 80 Complied with TCM SB94 2 Oil Filter Adapter Mounting Stud Inspection dated 2 10 94 during filter change stud height acceptable and no looseness F and Drive Instat M du 3 1934 during alternators installa detected Complied with T C M MSB94 8A Magneto to Engine Timing dated 10 09 96 checked magneto timing with satisfactory results for all mag vim T C M 9 1989 during Complied with T C M service information letter buletins SB96 7 Torque Limits dated 6 11 96 SIL95 5 Hose and Tubing Installation dated 8130 95 sd ar orque Limits dated January and 51 93 15 General Procedures for use of Lock Wire Tab Washers and Cotter Pins dated 9 13 93 during engine maintenance and
55. IME IN ENTRIES M FLIGHT SERVICE MECHANIC 7725 TESTS AND INSPECTIONS KEQUIRED BY SPAR 91 411 REAR 91 413 HAVE BEEN PERFORMED AS FOLLOWS PILOT STATIC SYSTEM TESTED TO COPILOTSTATIC 20 ALT Ane sw 2021560 suc 4 16 5 ALT 2 Jain 14 oup _ 602 150 TESTED ENC 2 M TRANSPO TRANSPO PERTIN ENTf UNDER WOR AUTH SIGN KINGS CRS KD R I 5 i supo 1 UNITED STATES 2 M Organization i FAACRS ien LEX 801 38 5 Description For 950 a 13 Remarks KA parts must be accompanied by maintenance his 14 New New Overhaul Certifies that ibe new nr newly overhauled part s identified otherwise specified In block 13 was were manut ctured in FAA approved design date and airworthiness Note In case of pari to be exported the P Importing country have been mel i 15 Signature T7 Name Typed or Printed FAA Form 8130 3 OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF YEPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES spections Tests Repairs and Alterations ndorsed with Name Rating and Certificate Number of Mechani
56. IN m ores DESCRIPTION OF INSPECTIONS TESTS REPAIR ALTERATIONS DATE RECORDING TOTAL performed Note Recurring AD 76 02 07 no longer applies due to install alternator part numbers No further action required 5 TACI OD ro UGH MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES RE MEUM Ee eji me E PY 18431 Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY 528 __ 10 1998 Aircraft Total Time 3 449 3 hrs Heater Hobbs 157 7 hrs zis Left Engine Model T C M TSIO 520 L S N 227642 R Pg Left Engine Total Time 2 765 1 hrs T S O 1 388 1 hrs 9873 MEE Right Engine Model T C M TSIO 520 L S N 241811 R D DR Right Engine Total Time 2 404 1 brs T S O 1 388 1 hrs 28 a Fan Left Propeller Model Hartzell PHC J3YF 2UF S N ED761 Ln Left Propeller Total Time 3 449 3 hrs T S 0 700 0 hrs Right Propeller Mode Hartzell PHC J3YF 2UF S N ED812 an Right Propeller Total Time 3 449 3 hrs T S O 1 193 3 hrs gt i Performed an ANNUAL inspection in accordance with FAR part 91 409 a as per FAR part 43 3 4 qo appendix D Performed the 12 month inspection requirements for E L T s as per FAR 91 207 in accordance with Ss IM I FAA Action Notice A8150 3 E L T Recommended Supplemental Inspection Procedure
57. ION oem Hor soo the feh wheel ake Bleed ind operational cheek of brake system normal INSPECTIONS TESTS REPAIRS AND ALTERATIONS RSED WITH NAME RATING AND CERTIFICATE NUMBER OF ACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES TINUED hrs raft balteries serviced with distilled water cleaned and neutralized h uid meeting MIL H 5606 Texaco 15 Serviced fuel strainer atand engine controls lubed landing gear Serviced all tires with Janding gear retraction and extension check emergency extension rconditioner compressor drive belt with a new unit P N 642759 raft systems with norma results Work performed in accordance ors manual X30505 and TCM Service Instructions an ANNUAL inspection and was determined to be in airworthy PLE E AP1475821401A DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS TACH TODAYS TIME ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF 192 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES TESTS AND INSPECTIONS REQUIRED BY Scale Corrections Add Algebraically JMransiin MrAnsLAS QFARSI 217 Altimeter Room Altimeter Room HAVE BEEN PERFORMED AS FOLLOWS Bi EE Reads Temp Reads Temp PILOT STATIC SYSTEM TESTED TO 7 4
58. L Spec Removed left and right losd meters cleaned contacts and reinstalled ind replaced filters with new units Champion P N CH48108 left engine Performed alucrnator paralleling to 28 25 volis and performed charging system ground operational checks with normal results Replaced wedge lighting for for abnormal contamination none found Serviced left and right engines 2 load meter 1 fuel quantity gage and MAP gage Removed glovebox and right side forward interior panel sealed leak in door seal pressure tube secured CONTINUED ON NEXT PAGE hose and reinstalled removed items Ground operational check of door seal system normal Repaired glareshield connector Replaced defroster lex duct eee 40 glareshield Inserted A F M Supplement P N 58 590000 59 dated August 2002 and new supplement revision sheet into flight manual Cleaned uircraft interior Cleaned and polished aircraft exterior Performed run up check leak check and aircraft systems ground operational checks with normal results Work performed in accordance with Beech 58P 58TC Series service manual la John AP147582140IA n performed calibration of left and right indicating systems Spar Caps by inspection defects noted Complied with Beech of Fuel by inspection no defects noted Verified compliance with x issued February 1993 found N A by unfeather accumulators ance with Raytheon Beech SB 52 2693 R2 Doors Inspection of the
59. NS FAA FORM 337 BY DATE OR TO THE WORK ORDER BY NUMBER AND THE APPROVING AGENCY New aircraft hasic empty weight 4391 Ibs New Empty Weight Moment 325 545 Ibs New Empty Weight C G 74 14 Replaced the N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY Januaty 24 2001 Aircraft Total Time 3 800 4 hrs Hobbs Reads 3 800 4 hrs Removed single type throw over control yoke and installed dual control yoke net exchange weight increase 3 Ibs 72 05 right wing tip strobe light lamp flash tube with a new unit P N W55 0221 1 Removed emergency oxygen bottle assembly and sent out for hydrostatic test Reinstalled bottle after hydrostatic test Bottle Manufacture Puritan Zepp Bottle Assembly P N ZC406 15 DOT 3AA1800 Heavy Weight Bottle S N 33638 Oxygen bottle next due hydrostatic test in 5 year on or before January 31 2006 Reinoved system indicator only insulated and secured associated wiring behind instrument panel Reinstalled previously removed Bonzer ra altimeter indicator only in place of were the EGT indicator came Weight change between indicators negligible Updated aircraft equipment list to reflect change Ground operational check of radar altimeter normal Work performed ccordance with Beech 58P 58T Series servk manual aa 147582140 PIS A See Ake TORE AIRFRAME LOG RAYTHEON MODEL 58P S N TJ 65
60. P 58TC series service manual TCM TSIO 520 L LB 19 65 AIRCRAFT LOG ENTRY 147582140 gine right magneto with a factory rebuilt unit P N of engine and aircraft systems with normal results Work performed 2103 30505 and TCM Service Instructions built unil P N T RECORDING DATE TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS 3 563 7 brs TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF ble unit P N Installed 10 349260 6 Model SGRN 1205 S N Installed 19 FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES unit P N Installed 10 349260 6 Model S6RN 1205 S N Installed T teck of engine and aircraft systems with normal results Work performed 320 L LBLWB and TCM Service Instructions KINGS AVIONICS INC NL y 515 PERMANENT LOGBOOK ENTRY John Caka AP147582140 aD Co bsp Keer Gak SEC For hmm CrP Cue ofc r Rte 3 969 6 brs GENERAL AVIATION MAINTENANCE RELEASE ___ THE AIRCRAFT sed servicable unit Adjusted left and right engine oil pressures to proper APPLIANCE WAS REPAIRED AND INSPECTED IN ACCORDANCE eft engine fuel supply hose for servo to transducer with a new unit WITH CURRENT REGULATIONS OF THE FAA AND IS APP
61. R OTHER SPECIFIC ENTRIES TIME FLIGHT SERVICE MECHANIC OR i gt SETS TAN MT E N1843L Beech 58P SIN TJ 65 AIRCRAFT LOG ENTRY n August 15 1999 Aircraft Total Time 3 562 7 hrs 7 Left Engine Model T C M TSIO 520 L S N 227642 R Left Engine Total Time 2 878 5 hrs T S O 1 501 5 hrs Right Engine Model T C M TSIO 520 L S N 241811 R 7 Right Engine Total Time 2 517 5 hrs 5 0 1 501 5 hrs i Left Propeller Model Hartzell PHC J3Y F 2UF S N ED761 Left Propeller Total Time 3 562 7 hrs T S O 813 4 hrs Left Propeller Blade Design FC8468 6R Blade S Ns 41 H60393 2 H60398 3 H60399 Left Propeller Blade Total Times 1 813 4 hrs 2 813 4 hrs 3 813 4 hrs Right Propeller Model Hartzell PHC J3YF 2UF S N ED812 3 Right Propeller Total Time 3 562 7 hrs T S O 1 306 7 hrs inse 22 E es s DT 2004 1 UNITED STATES 2 Co MPH Organization FAA PKDGREGIN Fay 801 355 445 J Right Propeller Blade Design FC8468B 6R Blade S Ns 1 H25392 2 H25400 3 H25406 TL Part Number Right Propeller Blade Total Times 1 1 306 7 hrs 2 1 306 7 hrs 3 1 306 7 hrs Ve Z6 5 7 Removed left propeller serial number ED 761 from this aircraft Left propeller total time at removal 3 562 7 hrs propeller T S O at removal 813 4 hrs 2d Removed
62. ROVED FOR ck of engine and aircraft systems with normal results Work performed RETURN TO SERVICE PERTINENT DETAILS OF THE REPAJR ARE ON 0 L LB WB Operators manual X30505 and TCM Service Instructions FILE AT THIS STATION UNDER oL zr ORDER 36 22 _ paTE D27 27 SIGNE E Caka API47582140 CRS KD6R661N i hrs the left engine right magneto with a factory rebuilt unit P N laced the right engine right magneto with a factory rebuilt unit P N n LEN F of engine and aircraft systems with normal results Work performed JLB Operators 30207 and TCM Service Instructions fin AP147582140 4 RECORDING TACH TIME TODAYS FLIGHT Pot ay tat 56 7 Buchanan Airport c oncord 94520 5615 54925 676 2100 925 676 5580 FAX ALTERATIONS LOGBOOK ENTRY NUMBER OF R SPECIFIC ENTRIES i 24I 0247 12 47 56 Tach Reg N IS43e Hobbs F A A REPAIR STATION CERTIFICATE NO WQ3R954L with new units P N 066 04400 Ri th right main landing gear tire wit Replaced the right tire tube with a March 34 2000 Aircraft Total T 7 Complied with Apptiait and rightswitch functions with no Replaced the left 61 311 S N Instalied
63. RTIFICATE NI OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES 4 1927 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC 15 AIRCRAFT LOG ENTRY N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY 3 507 7 hrs January 8 199 Aircraft Total Time 3 514 9 hrs anifin Corp appliance AD 98 23 01 Dry Air Pumps effective Repaired wiring to HSI back lighting Operational check of instrument panel lights normal 1 iffected pump couplings installed currently installed air pumps charged aircraft batteries and serviced with distilled water both overhauled by Rapco Verified compliance with Raytheon Aircraft Co service bulletin SB 2691 Rev 2 Fuselage R T probe with a new unit P N 86255 S N Installed 9839 tod Second Cabin Window Lower Longeron Inspection Repair Reinforcement dated December 1998 for E Ct this service bulletin revision requires no further action due to previous compliance with Raytheon Bee ohn E AP147582140 AD 97 09 09 Structural Cracking Longeron Inspection and Reinforcement in accorance with ae service bulletins SB 2630 and SB 2691 Rev 1 previously complied with on July 15 1997 at aircraft tt time 3 314 2 hrs AGE AP1475821401A 1843 2 Repaired broken Re stalp a N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY March 6 1999 Aircraft Total Time 3 519 1 hrs
64. ade S N s 1 5086 2 51118 3 51119 Right Propeller Model McCauley 3AF32C521 C G 82NLA A Right Propeller S N 983955 Right Propeller Total Time ut Installation 0 000 0 hrs T S O N A Right Prop Blade S N s 1 53091 2 1092 3 S 112 Propeller installation performed in accordance with Beech 58 58 service manual and RAM installation instructions and drawings Installation approval is as per RAM Aircraft Corporation STC 540902 X Installed Prop Gnard Aerospace Inc polyurethane protective tape on the propeller blade jeading in accordance with Prop Guard installation instruction document FP1001 CS1002 dated February 25 1997 Installation approval is as per Prop Guard Aerospace Inc supplemental type certificate SPO0582NY Weight and balance change negligible Aircraft physically reweighed after all modifications weight and balance and equipment list data updated to reflect current aircraft configuration The following information was entered into the Weight amp Balance section of the aircraft flight manual New Basic Empty Weight 4 388 Ibs New Empty Weight Moment 325 329 inlbs New Empty Weight C G 74 14 in Replaced the right cngine pneumatic system air pump with a Rapco Inc overhauled unit P N Installed RA 442CW 4 S N Installed 77448 Installed unit TSO 0000 0 hrs Replaced the left and right pneumatic system inlet filters with new units P N D9 14 5 replaced the and right pneumatic system
65. bbs time 256 9 hrs or 9 30 99 whichever comes first Note This AD note supersedes Janitrol Appliance AD 82 07 03 Heater Pressure Decay Test Replaced the left engine pneumatic system air pump with a Rapco Inc overhauled unit P N Installed RA 442CW 4 S N Installed 60508 Installed unit TSO 0000 0 hrs S N Removed 11AH846 Replaced the pneumatic system inlet filter with a new unit P N D9 14 5 replaced the pneumatic system in line filter with a new unit P N 1J4 7 Replaced the left engine compartment pneumatic system flex hose couplings with new units P N MIL H 6000 3 4 Serviced batteries with distilled water and top charged Lubed all flight control hinges Checked and serviced left and right propeller dome pre charges and unfeather accumulator pre charges Performed propeller de ice system functional check with satisfactory results Serviced all tires with air Repaired airconditioner compressor idler sheave by replacing bearing P N 643368 and bolt P N AN101319 tensioned belt to proper specs Replaced left side brake linings with new units P N 66 44 Rebushed left and right main gear torque links Performed run up check and operational check of engine and aircraft systems with normal results Work performed in accordance with Beech 58P 58TC series service 2 CAD _ John E Caka 147582140 9 yoays Daan CPG 8
66. c or Repar k pages for other specific entries Model S amp P S N TI 6S Zemovedt Century Autko Pilot iDYGb 0200 or Fears Ber model 2496 0909 Yn TIAE On Plat Century Systems tne velis 7608 E Sittin a eos ce SeaieCorrections Add Algebraically DATE RECORDING TOTAL DESCRI TACH TODAYS TIME IN ENTRIES MUST Altimeter Room C Altimeter 19 TUAE FLIGHT SERVICE MECHANIC OF Reads Temp Reads Tem 1 001 14 000 TESTS AND INSPECTIONS REQUIRED BY 0 16 000 SO FAR 91 411 AFAR 91 413 18 000 HAVE BEEN PERFORMED AS FOLLOWS 20 000 4j oun FT PILOT STATIC SYSTEM TESTED TO T COPILOT STATIC SYSTEM TESTED TO FT 92 1275291 p ALT oe yu 202 150 TESTED BS 7 mcn IC san Fr 1 FT ara sm ence sm __ resen to FT TRANSPONDER 1 CoL Lass 1821 TRANSPONDER 2 NA PERTINENT DETAILS ARE ON FILE AT THIS REPAIR ST gt UNDER WORK ORDER Os 7 DATED 2 236 742 THIS IS A PERMA ENT LOGBOOK ec cm SALT LAKE CITY UTAH 2 174 5 1 AUTH SIGNATU KINGS AVIONICS INC CRS KD RGGIN 22 000 Alt Model 99281 32524 j amp Alt S
67. ced the left and righi 1 and right pneumatic sysiem filters with new units P N 642759 Replaced the aft nav light lens with new unit Replaced tke 70354 performed calibration as per Beech service landing gear tire with anew unit Goodyear Hight Custom 5 00 reinstalled Notel No record i of wing bolt replacement fond accessibl portions of the wing bolts and fittings no defects evidi gt ih Cleaned inspected and repacked all wheel bearings D with distilled water cleaned and neutralized battery box top charged 606 Royco 156A Serviced fiel strainer screens and drained sump Lub d landing gear Lubed the teft and right upfock downlock rotiers cand extension ch ck emergency extension check and safety switch Performed Up check and operational check of engit with Beech SSP SETC series service manual TENT 510 520 VLBW drawing and instructions gt 1 thai this sire has been inspected in accore 55 409 as per FAR 43 appendix D ES AR 91 207 in accordance with FAA Action Notice A8150 3 E L T To defects noted ELT Make Narco Model FLT 10 S N 75731 or before July 31 2000 nors effective date 2102116 found N A by alternator part number ind right alternator P N ALV 9510 S N A 100459 installed onto inspection no longer required 1 date 8 30 77 Par La b c p
68. control hinges Lubed uplock rollers Checked and serviced left RY p and right propeller dome pre charges and unfeather accumulator pre charges Serviced all tires with air teads 3 237 2 hrs 2 Replaced the right main landing gear brake linings with new units 6 each P N 066 04400 Serviced serviceable unit P N 701571 S N Installed hydraulic brake reservoir with fluid MIL H 5606 ed the left engine low thrust detector system Performed run up check and operational check of engine and aircraft systems with normal results Work xi terminal and securing probe wiring Replaced performed in accordance with Beech 58 58 series service manual e with a new unit Alcor P N 86255 Performed G at with normal re ohn E 1475821401 John E 147582140 DATE 19 RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES TIME FLIGHT SERVICE N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY July 15 1997 Aircraft Total Time 3 314 2 hrs Heater Hobbs 156 9 hrs Left Engine Model T C M TS10 520 L S N 227642 R Left Engine Total Time 2 630 0 hrs 5 0 1 253 0 hrs Right Engine Model T C M TSIO 520 L S N 241811 R
69. de ice system 50 hour and 100 hour functional checks and inspection with normal results for the left and right 3 AD 82 07 03 Heater Pressure Deny Tes Performed run up check leak check and engine propeller and aircraft systems ground operational checks with normal results Work icd performed in accordance with Beech S P S8TC series service manual T C M TSIO 520 L LB WB Operators manual X30505 T C M Service Instructions McCauley MPC 12 operators manual and RAM Aircraft Corp maintenance tips and manual supplements m x eril comp lance with JanAcrs Devices p effective aies 9 11 0 found Nia by affected type regulator and shut off E AP147582140 a with normal results Serviced right main landing gear strut el Regulator Valve inspection effective date 5 10 01 found LEGA John E AP147582140 ted filters for abnormal contamination none found installed 7 ight filter date code FO7L29 1 complied with T C M service ___ J height acceptable aad no looseness detected for the left and Performed up check check and engine and aircraft ___ with Beech S8P 58TC series service manual T C M TSIO M ONE ATTE 7 ohn E AP147582140 8 30 77 Par 1 a b c performed operational check of left and 14 000 77 hours P igines Serviced aircraft main batteries with distilled waler cleaned 1 fluid
70. e aircraft serial number and model Complied with Raytheon Beceh boots Cleaned aircraft interior Cleaned and polished aircraft exteriori Cleaned engines and engine compartments Check dated June 2002 as per communique pre flight start and Performed run up check leak check and engine propeller and aircraft systems grouad operational checks with normal results Engines meets dght pneumatic systems the performance requirements of FAR 43 15 Par 00 Work performed in accordance with Beech 58 8 series service manual T C M TSIO 520 1 for the left and right engines with the following results Left engine L LB WB Operators manual X30505 Service Instructions McCauley MPC 12 operators manual and RAM Aircraft Corp maintenance tips and manual cylinders 1 78 80 2 76 80 3 76 80 4 76 80 5 72 80 6 supplements Work performed by John Pollock Wade Saxton and John Caka Inspection performed by John Caka 1 2 10 94 during filter change stud height acceptable and no looseness 21 certify that this aircraft bas beca inspected in accordance with an ANNUAL INSPECTION and was determined to be in airworthy 09 96 checked magneto timing with satisfactory results for all mags ted 6 11 96 SIL95 5 Hose and Tubing Installation dated 8 30 95 15 dated 9 13 93 during engine maintenance and repairs as required ders dated 9 10 96 Part 1 Annual Inspection Requirements results Service Alert S A No
71. eck of engine and aircraft systems with normal results Work performed in accordance with Beech 58P 58TC series service manual TCM TSIO 520 L LB WB Operators manual X30505 and I CM Service Instructions and RAM Aircraft Corp drawing and isstructions I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in airworthy Mo E E AP1475821401A condition D 118431 Becch 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY DATE RECORDING gt IB September 4 1999 Aircraft Total Time 3 563 7 hrs Hobbs Reads 3 563 7 hrs v TODAYS TIME N V RNTRIESCMU arcere Replaced the left engine right magneto with a used serviceable unit P N Installed 10 349260 6 Model S6RN 1205 S N Install ed SML FLIGHT SERVICE MECHANIC 8138063 Replaced the right engine right magneto with a use serviceable unit P N Installed 10 349260 6 Model SGRN 1205 S N Insta ted P d aircraft systems with normal results Work performed heck and operational check of engine an Operators manual TSIO 520 L LB John AP147582140 E118756FR Performed ground run up and leak jn accordance with Beech 58P 58TC series service X30505 and TCM Service Instructions RINGS AVIONICS INC i THIS ISA PERMANENT PME 7 4 ecu Eor Co P Gr o CPC
72. ected and repacked ali wheel bearings Removed aircraft batteries serviced with dis water cleaned and neutralized battery box top charged batteries and reinstalled Serviced brake reservoir with fluid mecting MIL H 5606 15 Serviced fuel strainer screens and drained sumps Checked all lights for proper operation Lubed flight and engine controls lubed lat gear Lubed the left and right uplock downlock rollers Performed ground run up and leak check in accordance with Beech SSP 58TC series service manual 17524 4 after re 4 operational check of engine and aircraft systems with normal results Work perfe 1 TCM TS1O 520 LILBIYB Operators manual X30505 and TCM Service Instruc ULE LE Jolin E Caka AP147582140 474 Tach N CERTIFICATE NO WO3R954L H s 3 618 1 hrs as per Beech SOP S8TC series service manual Serviced batteries with wmed propeller de ice system functional check with satisfactory results 4 armed ground run up and leak check and operational check of engine and vith po seri ice manual TCM TSIO 520 L LB WB LE ACE john E AP147582140 g L 4 L N1843L Beech 58 Baron S N TJ 65 AIRCRAFT LOG ENTRY July 8 2000 Aircraft Total Time 3 724 0 brs Hobbs Reads 3 724 0 hrs Performed 50 hour servicing and lubrication as per Raytheon Beech 58P 58TC service manual Complied with appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1
73. ed left and right propeller dome charge Checked left and right propeller unfeather accumulator precharges both found satisfactory Serviced all tires with air Serviced brake reservoir with fluid meeting HIL 5606 Texaco 15 Serviced fuel gascolators and screens and drained sumps Checked all lights for proper operation Lubed all flight and engine controls lubed landing gear Lubed uplock rollers Serviced landing gear transmission with one 1 oz Mobil 636 lubricant Replaced the left and right pneumatic inlet filters with new units P N D9 14 5 Installed two 2 new bushings P N 105739D 210250 two 2 links P N 35 815078 two 2 new bushings P N 1057395 0137 and two 2 new screws P N 35 815183 at the downlock cable attach point Checked downlock cable tension found satisfactory Reset left and right main landing gear inboard door preload to proper specs Performed retraction and extension check emergency extension check and safety switch operational check of landing gear system with normal results Replaced the left main gear tire with a new unit Goodyear Flight Custom II CONTINUED ON NEXT PAGE RECORDING TOTAL DESCR TACH TODAYS TIME IN ENTRIES MUS TIME FLIGHT SERVICE MECHANIC Wi843L Beech 58P Baron S N 14 65 June 17 1996 Aircraft Total Tine 3 090 1 hr 19 5X6 75 8 S N Installed 60671961 Balance main gear toe in to proper specs Replaced the 066 04400 Replaced the airconditioner
74. ems with normal results i RETURN TO SER Work performed in accordance with Beech 58P 58TC series service manual TCM TSIO 520 L LB WB FILE hee 27 Operators manual X30505 and TCM Service Instructions i ORDER NO certify that this aircraft bas been inspected in accordance with an ANNUAL inspection and was H CRS determined in airworthy condition rmined to be in airworthy con Se FEES 558 v John AP1475821401A 28 tee 242 pL im 4 oa A mei i age oS 4 F i E pow 4 B PC i i zad _ RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATI INSPECTIONS TESTS REPAIRS AND ALTERATIONS ED WITH NAME RATING AND CERTIFICATE NUMBER OF i TACH TODAYS TIME IN e CILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES t TIME FLIGHT SERVICE E IC OF ed pou i TINUED FROM PREVIOUS PAGE KINGS AVIONICS INC 1 Replaced the left and right pneumatic system inlet BS Pi PERMANENT S left and right pneumatic system inline filters with new L 12437 5 356 Ground A tube from the inlet filter to the engine aft baffling with BEES Chadha fee EDR 25 13 20 _ i ft auto pilot system Deactivated system by removing 3 uit breaker in accordance with FAR 91 203 Auto pilot ____
75. erformed operational check of left 1 time 3 662 7 bours Induction Air Filters effective date 1 29 85 Par replaced lelt agine installation This AD next duc at aircraft total time 4 062 7 Placard Lack of Fuel Flow to Engine effective date 4 19 99 Par 5 hrs as per Beech service bulletin 2670 R1 Fuel Selector Placard 0 1 engines from the left and right sides of this aircraft Installed aircraft Left Engine SIN 2741368 Left Engine Total Time at hrs Right Engine SIN 518721 Right Engine Total Time at with new vibration isolators repaired and new exhaust system compartment pncumal system flex hoses and all engine components se binder and component status sheet for details of component part 3rdance with Beech SgP SST C service manual and RAM installation poration STC SAI207NW Inserted of FAA approved airplane 36 into the aircraft flight manual P O H see FAA form 337 s filed CONTINUED ON NEXT PAGE N1843L Beech 58 Baron SIN TI 65 CONTINUED FROM PREVIOUS PAGE September 4 1999 Aircraft Total Time 3 562 7 brs Removed Hartzell model PHC I3Y F 2UF FC8468 6R propellers from the left and right sides of this aircraft Installed McCauley model 3AF32C521 G82NLA propellers in the right positions of this aircraft Left Propeller Model McCauley 3AF32C521 C G 82NLA A Left Propeller S N 983957 Left Propeller Total Time at Installation 0 000 0 brs 5 0 N A Left Prop Bl
76. eries serviced with distilled water cleaned and neutralized battery box top charged batteries P ETE Bleed right brake system with MIL H 5606 and serviced brake reservoir and reinstalled Resealed the right brake caliper assembly Complied with tiduetion Air Filter Appliance 0 84 26 027 induction air fitters with new units P N 50 389070 23 This ADI Verified compliance with JanAero Devices formerly Janitroi Replaced right brake tine 29 i NOn i heater hobbs times 160 3 hrs el linings with new P N 066 04400 informed owner of brake lining conditioning procedure as per Cleveland product reference memo 14A Cleaned left lows eet PIN 820201 Beech 102 384010 1 S N 2751 198 thrust detector hose amp pitot tube assembly Tightened control yoke collar Replaced lock washer for right engine fuel spill pan attach screw and resafeticd Ta lt f E turbo PRV Dressed and polished left and right propeller blade leading edges Tightened left main damage from propeller to right side forward fuselage and painted panel to proper operation Lubed flight and engine controls lubed landing gear Serviced all tires with air ASG 7 Cleaned gaped and rotated all spark plugs for the left and right engines Drained left and right engines oil and removed filters inspected removed filters for abnormal contamination none found installed new FAA PMA oil filters Champion P N CH48108 left filter date code FO6M26F
77. f engine and aircraft systems with normal results Work performed in accordance with Beech 58P 58TC series service manual TCM TSIO 520 L LB WB Operators manual X30505 and TCM Service Instructions I certify that this aircraft has been inspected in accordance with an ANNUAL inspection and was determined to be in airworthy condition ee john Caka AP147582140 A cd ia mini DESCRIPT RECORDING TOTAL TACH TODAYS TIME IN ENTRIES MUST TIME FUGHT MECHANIC OR i SERVICE N1B43L Beech 58 Baron S N TJ 65 August 25 1998 Aircraft Total Time 3 4 Removed flight director auto pilot coi 7 Systems Reinstalled flight director auto pilot i performed static system leak check with sat operational checks with normal results N1843L Beech S amp P B Bar n S N TJ 65 October 18 1998 Aircraft Total Time 3 5 Complied with Appliatice AD 76 07 i E performed operational check of left and right sv aircraft total time 3 603 5 hours Complied with Beech service bulletin Wii EN PN H placard CAM gt Lubed all flight control hinges Clieckd inf ather accumulator pre charges Performed i results Serviced all tires with air Repainted white area atid right side forward lower fuselag 3 Performed run up check and operational che 5 in accordance with Beech 58P 58TC i i
78. ght Engine Total Time 1 607 6 brs T S O 373 6 hrs Left Propeller Model McCauley 3A132C521 C G 32NLA A S N 983957 Left Propeller Total 373 6 hrs 5 0 N A Left Prop Blade S N s 1 3086 2 51118 3 5719 Right Propclicr Model McCauley 3AF32C521 C G 82NLA A S N 983955 Right Propeller Total Time 373 6 brs T S O N A Right Prop Blade S N s 1 1091 2 81092 3 51112 Performed an ANNUAL inspection in accordance with FAR part 91 409 a as per FAR part 43 appendix D Performed the 12 month inspection requirements for E L T s as per FAR 91 207 in accordance with FAA Action Notice 8150 3 E L T Recommended Supplemental Inspection Procedure FAR Part 91 Operations No defects noted ELT Narco Model ELT 10 S N 75731 ELL Battery Expiration Dale October 3 2002 This inspection next due on or before October 31 2002 1 Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 4 b performed operational check of left and right switch functions with norma results This AD next duc at aircraft total time 4 036 3 hours Complied with JanAero Devices formerly Janitrol Appliance AD 96 20 07 Combustion Heaters effective date 11 14 96 par a combustion tube and combustion air pressure switch 10515 combustion tube decay test salisfactory adjusted combustion pressure switch to proper specs and rechecked with satisfactory results Current heater hobbs tine 158 8
79. h Raythoon Beech AD 2002 1 1 07 al complied with by compliance with Raytheon Beech Service Bulletin SR 33 Lubed the left and right uplock downlock rollers wii i i HEF ond monval sy mio 2 1 2001 found N A by affected type panel screw aot installed see en Ohn AP147582140 d p a tan Engine Toal im S N 518721 3 BOO 5 Be dm ae i bide ease 3 Ob Ss CIOS 1 i y thousands place iei 8 30 77 Par 1 a b performed operational check of left and rig f Performed an ANNUALS accordance with FAA Action Notice A8150 3 3 L T 7 0 hours pis poer od npecprdunce lacrd Installation effective date 7 08 2002 found previously ied ds and Markings Door Opening Placard Modifications for Pressurized sent Panel Screw Inspection effective date 7 1 5 2002 found previoi s Electroluminescent Panel Retaining Screw Inspection Issued stilled water cleaned and neutralized battery box top charged batteries vith MIL H 5606 and serviced brake reservoir Replaced right brak ure as per Cleveland product reference memo 14A Cleaned left ock washer for right engine fuel spill pan attach screw and resafe ened left main landing gear torque link and resafetied Repaired Compliance Acro Garey t atb 2 1 Fuel Regulator und Shut Off Valve
80. hrs This AD note next duc for the installed heater Model B3040 P N 82D20 1 Beech P N 102 384010 1 S N 2751 198 at heater bobbs lime 258 8 hrs or 11 30 2003 whichever comes first Note This AD note supersedes Janitrol Appliance AID 82 07 03 Heater Pressure Decay Test Verified compliance with JanAcro Devices formerly Janitrol Appliance AD 2001 08 01 Heater Regulator and Shut Off Valve Inspection effective date 5 10 01 found N A by this AD note superseded JanAero Devices Appliance AD 2001 17 13 Heater Fuel Regulator and Shut Off Valve 71 Inspection i won i Inspection Verified compliance with JanAero Devices formerly Janitrol Appliance AD 2001 17 13 Heater Fuel Regulator and Shut Off Valve effective date 9 11 01 found N A by affected type regulator and shut off valve not installed 7 INUED ON NEXT 18131 Beech 58P Baron S 2002 Kern Tol Timet 3 939 8 hi 3 muary 4 2002 Aircraft Total Time 3 939 8 hrs Hobbs Reads 31 Replaced the left and right over voltage relays with new un November 17 2001 Aircraft Total Time 3 936 3 hrs Hobbs Reads 3 936 3 hrs p Complied with Raytheon Beech AD 2001 23 10 Flap Flex Shaft Assembly Inspection Note effective date not until 12 13 2001 by records lt E gt d B00305 1 om 5 check as per Raytbeon Beech Service Bulletin SB 27 3478
81. ht and engine controls lubed landing gear Serviced all tires with air Lubed the left and right uplock downlock rollers with ASG 7 Cleaned inspected and repacked all wheel bearings Replace right main wheel inboard bearing cup and cone Replaced the right nai landing gear tire with a new unit Goodyear Flight Custom H 19 5X6 75 8 10 ply S N Installed 22641422 Balanced right wheel and tire aie d 3 model Verified compliance with Raytheon Beech SB 53 3341 2 reinstalled Performed landing gear retraction and extension checks downlock tension tigging checks emergency extension checks and safety s h found N A by aircraft serial number and model Verified compliance operational checks with normal results Complicd with Raytheon Beech Executive Service Series Communique 99 Announcement of Addition of Landing ch 2001 found OPTIONAL not in compliance at this time comply Gear Warning Test to Maiatenance Manual Temp Rev 32 1 dated November 1999 as per communique instructions landing pear warning operation and Flight Controls Flight Control Gust Lock Inspection Replacement safety operation normal Replaced the left and right pneumatic system inlet filters with new FAA PMA units P N RA D9 14 5 L amp R codes 16202 Verified compliance with Raytheon Beech SB 55 3524 Stubilizers Replaced the left and righ pneumatic system inline filers with new FAA PMA units P N RAIH 7 L amp R codes 10702 Cleaned and treated all de ic
82. ircraft Total Tine 3 191 8 hrs Hobbs Reads 3 191 8 hrs Cleaned and securred left landing light electrical connector Tightened airconditioner compressor belt __ Replaced section of left engine breather line with new HIL H 6000 3 4 hose Replaced the left engine starter with a NEW T C H unit P N Installed 646275 S N Installed 0 258909 Removed Prestolite P N MHJ 4002 S N Removed D047801 98 Starter S N D047801 98 TSO at removal 1 130 6 hrs Performed run up check and operational check of engine and aircraft systens with normal results Work perforned in accordance with Beech 58P 58TC series service manual ALL 2 irt pa ohn 2 147582140 CERO Beech SEP Baron S N 10 65 AIRCRAFT LOG ENTRY CONTINUED FROM PREVIOUS PAGE 1843 Beech 58 Baron S N 10 65 AIRCRAFT LOG ENTRY March 6 1997 Aircraft Total Time 3237 2 hrs Hobbs Reads 3 237 2 hrs Replaced the strobe light system power supply with a serviceable unit P N 701571 S N Installed 77 see maintenance release attached herein Repaired the left engine low thrust detector system 77 p T D S probe heat by installed new electrical ground terminal and securing probe wiring Replaced the right engine number three 3 cylinder 6 7 probe with a new unit Alcor P N 86255 Performed operational check of strobe lights and LTLD probe heat with normal re 2 2 m John E AP14758214
83. l Time 1 449 0 brs T S O 215 0 hrs Left Propeller Model McCaulcy 3AF32C521 C G 82NLA A S N 983957 Left Propeller Total Time 215 0 hrs T S O N A Lefi Prop Blade S N s 1 51086 2 SJ118 3 SJ119 Right Propeller Model McCauley 3AF32C521 C G 82NLA A S N 983955 Right Propeller Total Time 215 0 brs T S 0 N A Right Prop Blade S N s 1 3091 2 1092 3 SJ112 Performed an ANNUAL i inspection in accordance with FAR part 91 409 a as per FAR part 43 appendix D Performed the 12 month inspection requirements for E L T s as FAR 91 207 in accordance with FAA Action Notice A8150 3 Recommended Supplemental Inspection Procedure FAR Part 91 Operations Replaced ELT battery with new unit no other defects noted ELT Make Narco Model ELT 10 S N 75731 ELT Battery Expiration Date October 31 2002 This inspection next due on before October 31 2001 Complied with Appliance AD 76 07 12 Magneto switches effective date 8 30 77 Par 1 a b c performed operational check of left and right switch functions with normal results This AD next due at aircraft total time 3 877 7 hours Complied with Induction Air Filter Appliance AD 84 26 02 Paper Induction Air Filters effective date 1 29 85 Par A replaced left and right engine induction air filters with new units P N 50 389070 23 This AD next duc at aircraft total ti 4 277 7 hours Verified compliance with Raytheon Beech AD 2000 18 02 Elevator Skin Inspection Rep
84. l results Replaced the airconditioner CONTINUED ON NEXT PAGE DATE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS DATE RECORDING TOTAL gt amp TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF t TACH TODAYS TIME IN 19 TIME FLIGHT SERVICE MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES TIME FLIGHT SERVICE 3 2 N1843L Beech 58 Baron S N TJ 65 CONTINUED FROM PREVIOUS PAGE d E Fuly 15 1997 Aircraft Total Time 3 314 2 hrs EIS A CERNI Sg compressor drive belt with a new unit P N 642759 Replaced the left and right pneumatic system inlet STE 058 filters with new units P N D9 14 5 Replaced the left and right pneumatic system inline filters with new Lisa LE H units P N 174 7 Replaced the left pneumatic inlet tube from the inlet filter to the engine aft baffling with i i T new unit P N 102 910037 19 Deferred the aircraft auto pilot system Deactivated system by removing auto pilot control head and pulling the auto pilot circuit breaker in accordance with FAR 91 203 Auto pilot GENERAL Mibi APPLIANCE removal and deferral performed by Kings Avionics of Salt Lake City Utah i WITH CURRENTE Performed run up check and operational check of engine and aircraft syst
85. lacement effective date 9 22 00 found N A by no elevator skins replaced during the affected time period Verified compliance with Raytheon Aircraft Beech service bulletin 27 3396 Flight Controls Reskin Replacement of Magnesium Metal Bonded Elevator Assembly revision date June 2000 found N A by no elevator skins and or elevators replaced during the affected time period Note No record of wing bolt replacement found No wing bolt change at this time as per the owner operator s request Inspected the accessible portions of the wing bolts and fittings no defects evident Replaced aileron trim tab actuator rod bolts with new Replaced the aft nav light electrical connector housing and pins Stop drilled crack in upper left flap skin Repaired taxi light wiring Replaced left strobe light lamp with new Resecured landing gear emergency extension placard CONTINUED ON NEXT PAGE DATE RECORDING TOTAL TACH TODAYS TIME IN 19 TIME FLIGHT SERVICE DESCRIPTION OF INSPECTIONS TESTS REPAIRS AND ALTERATIONS ENTRIES MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF N1843L Beech 58P Baron S N TJ 65 AIRCRAFT LOG ENTRY CONTINUED October 3 2000 Aircraft Total Time 3 777 7 hrs Hobbs Reads 3 777 7 hrs Cleaned inspected and repacked all wheel bearings Removed aircraft batteries serviced with distilled water cleaned and neutralized battery box top charged batteries and reinstalled Serviced b
86. light director steering gyro and auto pilot mode selector and sent to Century Flight Systems for inspection and repair Reinstalled flight director computer amp P N 1D496 002002 S N Installed 1812F reinstalled flight director steering gyro P N 52C77 SIN Installed 942C and reinstalled mode selector P N 1C497 8 S N Installed 1306 Performed Sjgjic system leak check and with normal results eplaced aircraft Pilots Operating Handbook and Aircraft Flight Manual with a current issue unit Transferred flight manual supplemental data weight and balance data and copies of AD 98 04 24 to new manual Replaced the right engine pneumatic system air pump with a Rapco Inc overhauled unit P N Installed RA 442CW 4 S N Installed 60506 Installed unit TSO 0000 0 hrs Replaced the left and right pneumatic system inlet filters with new units P N D9 14 5 replaced the left and right pneumatic system in line filters with new units P N 114 7 Note No record of wing bolt replacement found No wing bolt change at this time as per the owner operator s request Inspected the accessible portions of the wing bolts and fittings no defects evident CONTINUED ON NEXT PAGE RECORDING TOTAL DESCRIPTION OF INSPECTIONS TESTS REPAIRS ALTERATIONS TACH TODAYS TIME IN ENTRIES MUST BE ENDORSED WITH NAME RATING CERTIFICATE NUMBER OF TIME FLIGHT SERVICE
87. ofc E 1 PEN eet N1843L Beech 58 Baron SIN TJ September 15 2000 Aircraft Total Time 3 Replaced the left engine turbocharger air oil separa specs Repaired wiring for the left engine fuel flow indicator Performed ground run up and leak check and operation dance with Beech 58P 58TC series service manual TCM TSIO 520 L LB WB c 65 AIRCRAFT LOG ENTRY g 66 569 6 hrs Hobbs Reads 3 669 6 brs Replaced left engine fuel supply hose for servo to transducer wil al check of engine and aircraft systems with normal results ors accor Cohn Caka AP1475821 tor with a used servicable unit Adjusted left and right engine oil pressures to proper X30505 and TCM Service Instructions GENERAL AVIATION MAINTENA APPLIANCE i WAS REPAIR WITH GURRENT REGULATIONS RETURN TO SERVICE PERTINE FILE AT THIS STATION UNDER d ORDER 3 25__ DATE Q27 th a new unit Work performed CRS KD6R661N leue N1843L Beech 58 Baron S N October 13 1999 Aircraft Total Time 3 587 6 hrs Hobbs Reads 3 587 6 hrs Adjusted airconditioner compressor idler and belt tension Replaced the left Installed 10 349460 1 Model S6RN 1255 S N Installed D079916FR Replaced the right engine right magneto with a factory rcl dinstalled 10 349460 1 Model S6RN 1255 S N Installed H269917FR Performed ground run up and leak check and operational chec in accordance with Beech 58
88. opeller de ice system functional check with satisfactory results Serviced all tires with air Performed run up check and operational check of engine and aircraft systems with normal results Work i an ith P series ic r performed in accordance w th Beech 58 58 series service P cC E j hn E AP147582140 AND ALTERATIONS RECORDING TOTAL DESCRIPTIO M OF INSPECTIONS TES TACH TS REPAIRS T TODAS M oe MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER O ECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES DATE REC i i ALE oe ned 5 of Inspections Tests Repairs and Alterations An 19 g Tact E ries must be endorsed with Name Rating and Certificate Number of Mechanic or Repair Facility See back pages for other specific entries BeechOat Model 58 sp TI 65 Removed lt entur Auto P flo Y E ESL ode 1D496 0200 IN Gur bo led anglifier model D49 6 0200 errr in ds conducked around ak Checker HS Plight Yo s area Dateo6 08 45 1 Certify The Sines E Century Flight n wea Repair Slfion No EDA rm SK RECORDING TACH TOTAL Des TODAYS T
89. ormed up check Jeak check and engine propeller and aircraft systems ground operational checks with normal results Engines meets the performance requirements of FAR 43 15 Par QQ Work performed in accordance with Becch 58P 58TC series service manual T C M TSIO 520 L LB WB Operators manual X30505 T C M Service Instructions McCauley MPC 12 operators manual and RAM Aircraft Corp maintenance tips and manual supplements Work performed by John Pollock Wade Saxton and John Caka Inspection performed by John Caka I certify that this aircraft bas been inspected in accordance with an ANNUAL INSPECTION and was determined to be in airworthy condition LE Ce John E AP1475821401A S ED s ly Inspection Note effective date not until 12 13 2001 by records Shaft Cable Assembly Inspection Replacement Issued September 4 for the left and right engines with the following results Left engine ae cylinders 1 79 80 2 76 80 3 74 80 4 77 80 5 78 80 6 i 2 10 94 during filter change stud height acceptable and looseness 29 96 checked magneto timing with satisfactory results for all mags ed 6 11 96 SIL95 5 Hose and Tubing Installation dated 8 30 95 15 dated 9 13 93 during engine maintenance and repairs as required ders dated 9 10 96 Part 1 Annual Inspection Requirements results d Aerospace Inc polyurethane protective tape on
90. plied with Induction Air Filter Appliance AD 84 26 02 Paper Induction Air Filters effective date 1 29 85 Par A replaced left andright engine i induction air filters with new units P N 50 389070 23 during engine installation This AD next duc at aircraft total time 4 062 7 hours Complied with Raytheon Beechcraft AD 99 05 13 Fuel Selector Placard Lack of Fuel Flow to Engine effective 4 19 99 Par a verified placard previously installed 10 18 98 at aircraft total time 3 503 5 hrs as per Beech service bulletin 2670 Ri Fuel Selector Placard Install No further action required Removed Teledyne Continental Motors model TSIO 520 L engines from the left and right sides of this aircraft installed T C M model TSIO 520 WB engines in the left and right positions of this aircraft Left Engine S N 274136R Left Engine Total Time at Installation 1 454 6 hrs Left Engine T S O at Installation 0 000 0 hrs Right Engine S N 518721 Right Engine Total Time at Installation 1 234 0 brs T S O at Installation 0 000 0 hrs Engine installed with new vibration isolators repaired and new exhaust system components new engine compartment flammable fluid flex hoses new engine compartment pneumatic system flex hoses and all engine components Een left side pneumatic vacuum pump overbauled sce 3 ring maintenance binder and component status sbeet for details of component part numbers and serial numbers
91. rake reservoir with fluid meeting MIL H 5606 Texaco 15 Serviced fuel strainer screens and drained sumps Checked all lights for proper operation Lubed flight and engine controls lubed Janding gear Serviced all tires with air Lubed the left and right uplock downlock rollers with ASG 7 Performed landing gear retraction and extension check emergency extension check and safety switch operational check with normal results Replaced the airconditioner compressor drive belt with a new unit P N 642759 Performed run up check and operational check of engine and aircraft systems with normal results Work performed in accordance with Beech 58P 58TC series service manual TCM TSIO 520 L LB WB Operators manual X30505 and TCM Service Instructions 1 certify that this aircraft has been inspected in accordance with an ANNUAL Z and was determined to be in airworthy condition 222222 John EA MECHANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES RECORDING gt TOTAL Dtsch T CH TODAYS TIME IN ENTRIES MUS 7 SERVICE MECHANIC T STSANDINSPECDONSREQUIREDRYL 7 1 9 3 O FAROL i HAVE BEEN PERFORMED AS FOLLOWS stati svstmcresren ro LA 2800 we 6 SN n PT COPILOT STATIC SYSTEM TESTED AA orm 9251 32520 32520137 10 Eoi ea tr THIS REPAIR STAT
92. repairs as required during radar akimeter indicator a 4 noved Complied with TCM SB96 12 Continued Airworthiness Instructions for TCM Cylinders dated 9 10 96 Part 1 Annual Inspection Requirements results wiring harnesses and probes in s pn eae er M T A manual temperature indicating system installation approval is per JPI STC 5 00 5 H satisfactory Performed the following maintenance and repairs Removed Prop Guard Aerospace Inc polyurethane protective tape on the propeller blade i 1 Mm 5 cha A 3 b leading edges weight and balance change negligible Checked left and rigbt propeller blade track Performed propeller de ice system 50 hour and 100 hour change e erat equipment reflect current aircra Adjusted left engine oil pressure up 1 turn Reparalleled alternators Replaced taxi light lamp with W functional checks and inspection with normal results new P N GE4596 Replaced rigbt forward upper wing attach fitting cover Repaired right engine induction air box support bracket Overhauled shimmy damper and serviced with MIL H 5606 hydraulic fluid Resealed pilots side right brake master cylinder Repaired and repainted right forward fuselage area due to propeller ice sling damage Cleaned inspected and repacked all wheel bearings Removed aircraft batteries serviced with distilled water
93. right propeller serial number ED 812 from this aircraft Right propeller total time at d gt removal 3 562 7 hrs propeller 5 0 at removal 1 306 7 hrs Win Removed left engine T C M model TSIO 520 L S N 227642 R from this aircraft Left engine gt 13 Remarks EE Limited on parts must be accompanied by maintenance history includ 14 New 1 Hew Overhaul D 4 Ceriiies that the new oi newly overhauled partis idemitied above 0 otherwise specified in block 13 was wert manutactured In accordang total time at removal 2 878 5 hrs engine T S O at removal 1 501 5 hrs NN Removed right engine T C M model TSIO 520 L S N 241811 R from this aircraft Right pog coto ho ben imet z engine total time at removal 2 517 5 hrs engine T S O at removal 1 501 5 hrs M aero M Propellers and engines removed as cores no return to service issued rungen 18 Dit FAA Form 81303 x At NSPECTIONS TESTS REPAIRS AND ALTERATIONS SED WITH NAME RATING AND CERTIFICATE NUMBER OF TILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES FT LOG ENTRY 7642 R 1 5 hrs 41811 R 1 5 hrs N BD761 3 4 hrs Ns 1 H60393 4 2 H60398 3 H60399 1 813 4 hrs 3 813 4 hrs 5 N ED812 1 306 7 hrs S Ns 1 H25392 2 H25400 3 H25406 2 1 306 7 brs 3 1 306 7 hrs from this aircraft Left propeller total time at 1 813 4 hrs from
94. this aircraft Right propeller total time at 1 306 7 hi LL S N 227642 R from this aircraft Left engine at removal 1 501 5 hrs 520 L S N 241811 R from this aircraft Right T S O at removal 1 501 5 brs no return to service issued DATE RECORDING TOTAL DESCRIPTION OF INSPEC J TIONS TESTS REPAIRS AND ALTE soe TIME Maia ORS MUST BE ENDORSED WITH NAME RATING AND CERTIFICATE NUMBER OF 4 R ANIC OR REPAIR FACILITY SEE BACK PAGES FOR OTHER SPECIFIC ENTRIES KINGS AVIONICS INC HIS 15 A PERMANENT LOGBOOK ENTRY Lexie ad Lights et ham bes CRBS Lire Pise ess obest Ceu S Top __ be Sahinpat LUST Hawt sitine Kis ALES c GENERAL AVIATION MAINTENANCE RELEASE THE AIRORAFT APPLIANCE WAS REPAIRED AND INSPECTED IN ACCORDANCE EUM OF THE FAA 15 APPROVED FOR RVICE PERTINENT DETAILS OF THE REPAIR x RE FILE AT THIS STATION UNDER _ a gt ORDER NO 2 620 3 79 SIGNED ZA PA CRS KD6R661N 1431 Beech 38P Baron S N TJ 65 AIRCRAFT LOG ENTRY September 4 1999 Aircraft Total Time 3 562 7 hrs Left Engine Model T C M TSIO 520 WB S N 274136R Loft Engine Total Time 1 454 6 hrs T S O 0 000 0 hrs a 7 Right Engine Model TSIO 520 WB S N 518721 Right Engine Total Time
95. ury Jo 2421 q pounopred 52202 18 pue ewou uozuoq 0248 put ordone 3487 JO JP 5 uay pauoene 661 FEI 1 4 5 OTHE PAISUI N S LLOCS payyeasuy N d IM UOZHOH 819315 yuni ON Paesu 5194201 1201 456439 DLS 8 8 Jed se 1980 pue yor Y N a00 QV SHP 661 12912924 eiep 124204 rojos Isnera 90 10 86 GY 1 qi 30 65 8 QV AMBUJ sepasredns 41 97 46 stp 590105 JAAD TM ISEI 501309 397 p3AOUISI ST jjEQS3UE13 297 1545 10 Jn QI3AO jJxou 5901809 71813 pur 2700 pinoy 9661 Ez Krenuef yeysyueID L1 97 L6 AY mi 14 706 SPEA SIY amp 06 18 01 1661 pI S9 L N S Voeg 485 YIA VIOPIZSSLP dV PWO H XA 72505 AP QVOTERLY N d

H1843L Beech 58P Baron, S/H: TJ-65 AIRCRAFT

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