Airframe Log Entry Piper 32RT-300T

Airframe Log Entry Piper 32RT-300T

Aircraft Record General Information M•nufacturer _j?_,_~ ..,P="~r'-------- Model '3.2 ~T ~oT -. ..r ial '32~ - 'J~~ '7 \ :1.~' _______ ____ Registration Num ber >-.lc....li '-~~A D11tc of M•nufacture _ ___________ ____ _______~ -------- - -- I nqlne(s) currently installed: Mmlufacturer ~,_,tP""""'"~--"--;"'--'-'--'~i------- Model l.:L D- ~t..to~ S~A D Serial j)..L. -3.~7 5 - b \ iAi. M11nufacturer ___ ________ Model Serial ___ l,ropeller(s) currently installed: M.1nufacturer _\.i~w~+~-z.~c._\ \'-----------Model HC--i= 3. '-? ~ - 1. ~~ HUD Model ___________ Serial £M__i3_Q_\ ~-~- _ Serial "'·•de Model ___________ Serial _____ Serial ______ Serial m .. de M odel ___________ Serial ___ _ Serial Serial _______ MAKE PIPER ~ !'-,.,.,,.,, HIGH PERFORMANCE AIRCRAFT, INC. DAT E 11912012 MODEL PA-32RT-300T Ne TSN 3699 12 :1 Alterations SIN 32R-7887121 Repaor Station No HPFR569X 3676 07 REG NO 428RA 1850 JOE CROSSON DRIVE TACH ate Number of WORK ORDER El CaJOO CA 92020 5527--09-20 11 Phone 858-576-5000 pecific entries. ) Airframe Entries PERFORMED AN ANNUAL INSPECTION IN ACCORDANCE WITH FAR PART 43, APPENDIX 0 . USING CURRENT PIPER PA32RT-301T {LANCE II) INSPECTION REPORT PIN 230-953 AS A GUIDE. ALL AD'S CHECKED THRU REV 2011 -27, SEE ATIACHED LIST COMPLIED WITH AD 2009-02-03, DATED FEBRUARY 9, 2009 (TO PREVENT A LEAN RUNNING ENGINE. WHICH COULD RESULT IN A SUBSTANTIAL LOSS OF ENGINE POWER AND SUBSTANTIAL, CNTD)-8130 FORM DATED 812712008 SHOWS COMPLIANCE WITH AD 2008-06-51 "G" IS ST AMPED ON HEX PLUG NO FURTHER ACTION REQUIRED COMPLIED WITH AD 80-14-03. PIPER SB 681 . DATED JULY 1. 1980 (DISRUPTION OF RADIO COMMUNICATION )-INSPECTED SYSTEM FOUND THAT THE AFFECTED RELAY SYSTEM IS NOT INSTALLED NO FURTHER ACTION IS REQUIRED COMPLIED WITH AD 95-26-13, DATED 2/511996 (TO PREVENT OIL COOLER HOSES FROM FAILING OR RUPTURING, WHICH COULD RESULT IN ENGINE STOPPAGE AND SUBSEOUENT, CONTD)-REPLACED OIL COOLER HOSES WITH 1 EA OF TSO 53a.TYPE D HOSES, PIN'S 124F001-BCR0210 AND 124F003-6CR0266 TERMINATING ACTION FOR THIS AO. NEXT REPLACEMENT IS DUE ON CONDITION COMPLIED WITH AD 2010-15-10, PIPER SB 1197C. DATED AUGUST 31 . 2010 (TO DETECT AND CORRECT ANY INCORRECTLY ASSEMBLED CONTROL WHEEL SHAF TS)-MEASUREO INSERTION OF THE PIN PER PIPER SB 11970 WITH NO DISCREPANCIES NOTED AT THIS TIME NO FURTHER ACTION REQUIRED REPLACED E.LT SAITE.RY WITH PIN 2020 REV A INSPECTED THE Ell SYSTEM AND FOUND THAT IT MEETS THE REQUIREMENTS OF FAR 91 207{dl ON THIS DATE ELT BAITERY REPLACEMENT DUE NOV,201 3. LUBRICATED CONTROL CABLES WITH AEROSHELL 33 AS INSTRUCTED COMPLIED WITH PIPER SB 1006 {CORROSION INSPECTION OF MAIN SPAR BEHIND FUEL TANKS) NO CORROSION DETECTED AT THIS TIME ON SPARS OR TANKS. CLEANED ANO TREATED AREA WITH DINITROL AS INSTRUCTED REPLACED FUEL OTY SENDER GASKETS WITH 2 EA PIN 755-049, REPLACED HOSES ON VENT LINES WITH 4 EA OF PIN'S 6391 3--092, 63913-093. AND 6901 5-041 REPLACED TANK A ITACHING SCREWS WITH PIN'S MS27039-0809 AND MS27039-0812 AS REQUIRED NEXT INSPECTION DU E JANUARY. 2019 .. COMPLIED WITH PIPER SB 656 (WINDOW CURTAIN ROD SUPPORT AREA INSPECTION)-NIA. CURTAIN ROOS NOl INSTALLED COMPLIED WITH PIPER SB 657A (TURBO-CHARGER EXHAUST COUPLING AND TAILPIPE FLANGE INSPECTION)- REPLACED TURBOCHARGER EXHAUST COUPlll'IG ANO TAILPIPE FLANGE WITH 1 EA OF PI N'S 556-1 08, LW12093-S, ANO GASKET PIN 78084 COMPLIED WITH SB 747 (NOSE LANDING GEAR ACTUATOR BOLT REPLACEMENT) BY INSTALLATION OF SPACERS WITH 2 EA PIN 86700-046 ON EACH SIDE OF THE NOSE LANDING GEAR ACTUATOR AND BOLT WITH PIN 402-869 PER SB INSTRUCTIONS .. COMPLIED WITH PIPER SB 866A (BACK-UP LANDING GEAR EXTENDER REMOVAL) PART I BY INSTALLATION OF BACK UP LANDING GEAR EXTENDER REMOVAL KIT PIN 765- 199 PER SB INSTRUCTIONS.. COMPLIED WITH PIPER SB 946 (FORWARD LEFT FUSELAGE FRAME INSPECTION) PERFORMED DYE PENETRANT INSPECTION AS DIRECTED IN PART 1 OF SB INSTRUCTIONS . NO CRACKS DETECTED AT THIS TIME, REINSPECT DUE EA. 100 HRS. COMPLY WITH PIPER SB 977 {INSPECTION OF WING REAR ATIACH FIITING AND ADDITION OF INSPECTION ACCESS PANELS) INSPECTED, FOUND WING A TIACH FITTINGS TO BE FREE OF CORROSION. HOWEVER BRACKETS ABOVE WERE DETERIORATED. REPLACED BRACKETS WITH 1 EA OF PIN'S 96884-000 AND 96884-001 WITH NEW A TIACHING HARDWARE COMPLIED WITH PIPER SB 1134 (SERVO METERED '"" PRr RE PORTlrGE. PRECISION BULT PRS ""·"::~::~·:J:::R:ER: ::ER;:: ~ --7~- - COMPLIED WITH PIPER SB 1161 (RIB ASSEMBLY INSPECTION AND MODIFICATION-AFT WING. WS 49 "•l ACCOMPLISHED TERMINATING ACTION ON LEFT MAIN GEAR BY MODIFYING RIBS WITH REPAIR KIT PIN 767-397 IAW and Alterations 1<11 INSTRUCTIONS INITIAL INSPECTION OF RIGHT WING REVEALED NO CRACKS AT THIS TIME. REINSPECT RIGHT WING EA 100 HOURS NEXT DUE@ 377607 TACH OBTAINED AND PROVIDED OWNER WITH DUPLICATE OF AFM ficate Number of VB900 AND ORIGINAL WEIGHT AND BALANCE REPLACED CENTER SEAT ATTACH OUTBOARD NUT PLATES WITH 2 EA r specific entries.) f'IN 37650-002 REPLACED PILOT SEAT UP/DOWN TRAVEL ACTUATOR WITH PIN 567-404 OPERATION IS NORMAL AT rHIS TIME REPLACED INDUCTION AIR FILTER WITH PIN BA7 .. REPLACED PARKING BRAKE VALVE ORINGS WITH 1 EA OF P1N·s MS28775-012, MS28775- 113. AND MS26775-114 REPLACED PLACARDS ON THE MAIN AND CARGO DOORS WITH 2 EA P/N 563-536 AND PIN 582-619. REPLACED RIGHT LOWER ENGINE MOUNT WITH PIN J-3804-37 REMOVED PROP, REMOVED SLUDGE FROM CRANKSHAFT. REPLACED ALTERNATOR DRIVE BELT WITH PIN 73965-014 HEINSTALLED PROP WITH ORING PIN 755-BOO AND SAFETIED PER M1M PARA 6-6 ... REPLACED PILOTS WINDSHIELD WITH PIN LP926 REMOVED LEFT FLAP. REPLACED UPPER INBOARD SKIN WITH PIN 65587-600, AND LOWER INBOARD <;KIN WITH PIN 65592-600 PAINTED TO MATCH ORIGINAL FINISH .. REPLACED MUFFLER ASSY WITH PIN K96705-000, SIN 211905 REPLACED# 6 CHT PROBE WITH PIN 553-673 REPLACED BATTERY PIN CB35-AXC. SIN 20002910 WITH PIN 035, SIN G02549544 REMOVED RUDDER. REPLACED RUDDER SKIN DUE TO A 1 112" CRACK IN SKIN. WITH PIN 78928-802. PAINTED TO MATCH ORIGINAL FINISH, CHECKED THAT BALANCE IS WITHIN ACCEPTABLE RANGE PER MIM Sl:.C TION 4-26, REINSTALLED RUDDER REPLACED COPILOT WINDSHIELD WITH PIN LP926 .. REMOVED CLEANED INSPECTED, AND REINSTALLED FUEL FILTER NO ABNORMALITIES NOTED AT THIS TIME WEIGHED AIRCRAFT IAW INS TRUCTIONS IN POH. INSTALLED NEW POH WEIGHT ANO BALANCE RECORD DATED 11912012 . ADJUSTED AILERON CABLE TENSIONS IAW M!M SECTION V, RIGGING INSTRUCTIONS TENSIONS ARE WITHIN LIMITS AND OPERATE NORMALLY AT THIS TIME ADJUSTED RUDDER AND STABILATOR CABLE TENSIONS IAW MIM SECTION V RIGGING INSTRUCTIONS TENSIONS ARE WITHIN LIMITS AND OPERATE NORMALLY AT THIS TIME ADJUSTED RUDDER CABLE I ENSION PER MIM 5-25. ADJUSTED ELEVATOR TRIM CABLE TENSIONS IAW MIM SECTION V . RIGGING INSTRUCTIONS I ENSIONS ARE WITHIN LIMITS AND OPERATE NORMALLY AT THIS TIME . REMOVED OIL COOLER FLUSHED, AND HEINSTALLED WITH NO LEAKS DETECTED AFTER ENGINE RUN NEXT FLUSH DUE @4199 2 TTAF .. RESEALED LEFT AND RIGHT MAIN GEAR STRUTS WITH 2 OF EA PIN'S 167-630, MS28775-227, AND MS28775-327 SERVICED WITH 5605 ~ LUID AND NITROGEN. NO LEAKS DETECTED AFTER SERVICING REPLACED AIRFRAME INTERIOR BRAKE LINE HOSES AND LANDING GEAR BRAKE HOSES WITH 2 OF EA PIN'S 11 1417-4S0084 AND 111417-4S0186. AND 1 OF EA PIN'S t 11417-4S0110 AND 111417-4S0150 SERVICED AND BLED BRAKE SYSTEM NO LEAKS DETECTED AT THIS TIME REPLACED MAIN LANDING GEAR UPPER TORQUE LINK BUSHINGS WITH 4 EA PIN 67026-007 REPLACED LEFT ANO HIGHT MAIN INBOARD WHEEL BEARINGS AND RACES WITH 2 EA OF PIN'S 13636-20629 AND 13889-20629 REPLACED LEFT MAIN LANDING GEAR DOOR WITH PIN 67090-010 PERFORMED NORMAL AND EMERGENCY LANDING GEAR OPERATIONS. NO ABNORMALITIES NOTED AT THIS TIME . LUBRICATED AND SERVICED AIRCRAFT IAW MIM CHAPTER 12 CHARTS AND INSTRUCTIONS I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN /\NNUAL INSPECTION AND WAS DETERMINED TO BE IN AIRWORTHY CONDITION 1h f> aircraft and/or component(s) 1ndent1fted above was repafred ancJ Klspected 1n accordance with currenl rnarntenance rules of the Fede<al Aviation uLog ulatmns and 1s approved le< return 10 serv~ce Per11ne 1n1 s repair are on file at this repa~r stAt•on under Work Order No ~527...09 201"' l>.)~ ed OATE· 1/912012 SIGNE Work O rder 5527-09-2011 Oan Salzmao Printed by EB1s 3 1dalcomed1a com) Cert1f1ed Repair Station No HPFR569X I certify that the Alumcter Automatic Pressure Altitude Reporting and Static Systems Tests Repairs and Alterations and Inspections c.:quired by FAR 91 411 ha~ been performed and found to e<>mply wuh FAR Part 43, Append1K E. g and Certificate Number of Altimeter tcstetl 10: 25,000 Jes for other specific entries.) Pilot Allimeter SIN In Ain:rafl Co-Pilot Altimeter SIN In Ain:ran I certify that the ATC Transponder Tests and lnspeaions required by FAR 91.413 (a) ha"' been perfonned and found to comply with FAR Part 43. Appendix F NEf\L .: ->; .... Transpmder #I SIN In Aircran /\Vl/\TION ....l N428RA "">1"'1J1T~~I '-tOl..llH ,,•• ~r.. Fi\i\ Repair Station #NOER688Y I 860 Joe Crosson Dr. El Ca1on, CA 92020 I Hanger I /I I 619-857-8770 Date: ' Z.c I( -;1-------- ------------ --- - YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations 20 - TACH FLIGHT TIME IN Entries must be endorsed with Name. Rating and Certificate Number of DATE TIME SERVICE Technician or Repair Facility. (See back pages for other specific entri es.) Airframe Log Entry N428RA March 3 rd, 2012 S/N 32R-7887121 TACH 3688.84 1.

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