Aircraft Log

AIRCRAFT LOG . AIRCRAFf DESCRIPTION Registration No N ~ qN G Model: ?A- lj: t,- t, Q QT -p Popular Name:__._f1~ft,~Q~Q~------ . al No.: L/- ft, q 8 Q 3 q Type Certificate No.: A ~ 5 S Q :;on:..MATTFit~i~ liJHITE/FF..J.%1.~~ED $ Gt.b!fillc..r /r,8 .,'-jJ,f:iA Engine Manufacturer "PRAJI ~ \JJH ITNf '/ Serial Numbers: Single "PC.£- 7?l"J O 7 35 QriginalEngineModcl· -PTL,A- '+~A Left ___________ _ Propeller Manufacturer. HA "RTZ £ LL Onginal Propeller Model· 5 D 3- N 33 8A I Left 13saos :55;2.01 135:JOO 135~0lo BS II a Right __________ _ Hub or Serial Numbcr:Singlc _..S~~-4: __ 3.__ ____ _ Left __________ _ Right _________ _ Blade Numbers Right ~2017 MODEL COMPLIANCE WITH FAA AIRWORTHINESS DIRECTIVES -- A. D. No. Method of Compliance Time on Date of Signature and and Date (S.• log for DetoU1) Aircraft Compliance Certificate N o. //7 lfAY 1 9 20J -- All applicable Federal Aviation Administration Airworthiness 'Directives, through Bi-Weekly e2 C) I 7 ....... / 0 ' have beeo .complied with at the time of manufacture. Signed: ~-;.. ~-;-,,, -~-..~ - Pipe • • ~~R~c~:~W_75679 ~ ~- - - - -- Date NAY J 3 2DJ7 Aircraft Time This Date Brought forward Total AIRCRAFT LOG Recorder Reading Maintenance The Altimeter and Static System Test required b FAR performed. T alti eter(s) have been tested: y 9 1. 4 11 have been ?.~ •• ~~~'.~... ······~ ········~~.~.~~~.~ ... ~:'.'.'.~?.# 6 /4Z.t ~00011. ~~;;~r ~:~;i:c~~:~~:~~R 9£:ffl1 <2. ~·~·;······--···-·-- ................................................... 3 •••••••••••••······· .. The ATC Transponder Tests and Inspections req.ul;;·~~;-~;~-~~·······- were performed this date and found to comply with FAR ... 3 A ' 413 'T • Ppendlx F. 1. Make Garmin Model CTX33£I. SfN.K'tl";Io 5q7 2. Make Garmin Model CTX33ES S/N.8'.lf5S:,,:Zq = Details of this inspections are on File at this facility under: AFT S/N 46980 3'9 Date <::-,f -2 "{7 The Automatic Pressure Altitude Reporting Equlp~t 'lj,st )"'"'lj'Y FAR Part 91.217 have been performed this date: - 6 - () / ·············································································-······-··-···--····· The standby altimeter and static system test required by FAR Part 91.411 have been performed. 1,h~ st¥tdby altimeter has been tested to 40,000 ft. on ~/,.:II/ ~"L'7 ............................................ l=-...1 ................................................ - --------+-------t------- 7 I find that the aircraft meets the requirements for the certification • - request,ed and have issued a Standard Airworthiness Cerdficate. ~--------..- -- --- -------+-------t-------signat · M. r,_ 111,,,._..., Total To Carry Forward Date:MAY 1 3 2017 75679 - - - - Total Carry Aircraft Time Dote This Dote Total Brought + forward MAKE Piper MODEL PA~TP SIN <4698039 REG NO N39NG WORK ORDER 2V62~2017 Airframe Entries Piper Aircraft, Inc. 2928 Piper Drive Vero BHcn, Fl 329e0 Phone 772-567...C3e1 ut 2871 Al RC RAFT LOG . Recorder Reading Maintenance DATE &17/2017 AICTSN 5 land1ng1 HOBBS 5 Right wing strobe light lntenntttent Removed Flasher Current Box assembly, Piper pin 47g.001, 1/n 00581. Installed new Flasher Current Box assembly, 1/n 00602 Operational check and Installation acceptable ... Left and right strobe lights have one or more LED• Inoperative. Removed wing tip hght assemblies, Piper pin 47g.005, 1/n 00202 and 47g.ooe, 1/n 00201. Installed new w,ng tip hght 1ssembhe1, 1/n 00207 and 1/n 00207. Operational check and Installation acceptable. Me1nlenenc:e Rel .... Th• aircraft and/or 00mponenl(1) on N39NG wea rap111red and lnlpeded In accordance with current n.,ln cf ttle Federal Aviation Regulat10n1 ena wu found Airworthy for rwtum to MtVlce Pertinent deta,11 cf ttle,.. • on file at ttlla pair Station, ZPAR410X. under Wortc Order No 2962-08-2017 D•ed 6/1/2017 ' ' DATE. 817/2017 SIGNED:~~ Wort< Order: 2982-08-2017 Printed by E811 3 (datcomedil com) - - - - - -- - - , •.•. •.··········i·•············~-·.···· To :::::::::::::::::::::::::::::::::::::::: forward :;:::::::•:::•:•:::•:•:•:•:•:•:•:•:•:•:•=·=•:•:-:=:•:=:=:•:=·=·=·=·=·=·=·=·=::•: ......... ················· ... - - - - - and Remarks MAKE: Piper MODEL: PA-416-SOOTP SIN:~98039 REG. NO: N39NG WORK ORDER: 2969-06-2017 Airframe Entries Registration No. _____________ Signature Piper Aircraft, Inc. 2926 Piper Drive Vero Beech, Fl 32960 Phone: 772-567-4361 ext 2671 Certificate No. DATE: 612612017 AJCTSN:5 Landings: HOBBS: 5 Aircraft defueled .... Removed wing tip lenses for wing tip repaint after removal of wing tips for strobe light replacements. Reinstalled wing tip lenses. Installation acceptable. Maintenance Release The aircraft and/or component(s) on N39NG was repaired and inspected in accordance with current rules of the Federal Aviation Regulations and was found Airworthy for return to service. Pertinent de~ai of the repair are on file at thi Repair Station, ZPAR410X, under Work Order No. 2969-06-2017, Dated 612612017. • ' DATE: 6/26/2017 SIGNED: ~ Work Order: 2969-06-2017 Printed by EBis 3 (datcomedia.com) N3fNG Model: PA~-4iOOTP SIN: 44598039 Date: 11 August 2017 Hobbs Time: 9.1 Total Time: 9.1 Landings: 9 Work Order: S-17-00230 complied with AD 2017-16-03, effective date 9 Aug 2017 para (g) per the global AMOC approved for Piper Aircraft, Inc. dated 9 August 2 011 by complying with the instructions contained in Piper SB 1317 revision C and determining that all measurements meet the limits specdied in tables 1, 2 & 3. Ultrasonic testing for thickness measurements performed by Paragon and recorded results on page 2 of SB inspection form Paragon NOT FAA CRS #172R877C under 'NO# 8040817 No further action required. Removed LH flap PIN 46W47A030-001 SIN 03301734196 and RH flap PIN ~6W47A030-002 SIN 04211744024 for SB 1317 access and remstalled per Piper AMM 767-617 ch 57-50-00. Drained left and nght tanks and removed sealer for SB 1317 access, re-applied sealer, closed tanks and leak checked per Piper AMM 767- 617 ch 28-10-00 Replaced LH & RH flap chafe tape as required. Installed new static wicks PIN •56-904 on the RH aileron outboard and center positions. Accomplished all required operational and functional checks with satisfactory results, no leaks noted The Aircraft identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and 1s approved for return to service. Pertinent details are on file under the above work order. Signed -~ 7:_;;, Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C 'f ~ 1 I Model: SIN: Date: Airframe N39NG PA~-600TP 4698039 26 October 2017 -----~ef-------· I c.....__. .... C. Hobbs Time: W C\. l Total Time: W'\. lLandings: JI- C\ Work Order: A.-17-00441 Removed roll servo GSA PIN 011-00878-20, SIN 1A1016734 and installed overhauled servo PIN 011-00878-20, SIN 1A1016956 in accordance with Piper AMM 767-617, Ch. 22-10-00. Installed unit overhauled by Garmin lntemat1onal, CRS #G6XR582Y under W/0 14137386. Accomplished all required operational and functional checks with satisfactory results. I certify tha • • Pertinent een inspected in accordance with an Annual inspection and is determined to be in an airworthy condition. der the above work order. Olathe KS 66062 (913) 782-0530 FAA Repair Statton #AMYR171C Registration No. ___________ _ and Remarks Airframe N39NG Model: PA-46-&00TP SIN: 4698039 Date: 1 February 2018 I<L C. Installed lanyard PIN ◄ 72-059 on left and nght fuel filler caps Accomplished all required operabonal and function al checks with satisfactory results Signature CertiRcate No. Hobbs Time: 35.8 Total Time: 35.8 Landings: Work Order: S-18-00033 The Aircraft Identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Adm1rnstrat1on and Is approved tor return to service Pertinent details are on file under the above work order Signed ~ Olathe KS 66062 (913) 782-0530 FAA Repair Statton #AMYR171C Airframe N39NG Model: PA-46-600TP SIN: 4698039 Date: 06 April 2018 Hobbs Time: 72.2 Total Time: 72.2 Cycles: 63 Work Order. S-18-00030 A-18-00044 Complied with initial 50hr inspection in accordance with Piper Aircraft Warrantable 1 11 50hr Inspection Report PN 765-044 Performed ground functional check of stall warning system In accordance with Piper AMM 767-617, Ch 27-30-00 Complied with Piper SB N. 1318A Part I by inserting limitations into POH per SB instructions Accomplished all required operational and funebonal checks with satisfactory results The Aircraft identified abo e was repaired and inspected in accordance with current Regulations of the Federal Aviation Admm1strabon and Is approved f retu t rvice Pertinent details are on file under the above work order Signed ..Jt.~~~l,-lL ____ _ Olathe KS 66062 (913) 782-0530 FAA Repair Statton #AMYR171C Aircraft Time Date This Date Total lrought Forward - Airframe N3tNG Model: PA-4•00TP SIN: 4198039 Date: 26 April 2018 .. Al RC RAFT LOG Recorder Reading t<arwCioi,Avt •••a.,_. Installed new K303 relay PIN ~--i23 and new F302 fuse PIN •61-659 Accomplished all required operational and functional checks with satisfactory results Maintenance Hobbs Time: 82.4 Total Time: 82.4 Landings: Work Order: s-11-00122 The Aircraft identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and Is approved for return to service Pertinent details are on file under the above work order Stgned ~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Total To ::;::::::::::::::::::::~::::::::::::::: Carry Forward •:-::::•:•:-~:-:•:•:•:•:•:•:•:•:-:::•:• :::::::::::::::::::::::::::::::::::::::: Model: SIN: Airframe N39NG PA-46-600TP 4698039 Registration No. ____________ Hobbs Time: 114.3 Total Time: 110 Landings: 110 Work Order: S-18-00036 S-18-00030 A-18-00044 Complied with an Annual Inspection using Piper AMM 767-617, Chapter 5-20-00, event #1 and #2 forms as a guide to comply with the inspection requirements of FAR 43 Appendix D. Date: 26 June 2018 I<~C-----_ Keneee City Aviation Center Complied with 50 hour inspection of the strut extensions per Piper AMM 767-617 ch 12-10-00. Complied with 12 month aircraft lubrication in accordance with Piper AMM 767-617, Ch. 12-20-00. Complied with 90 day hydraulic pump reservoir fluid level check per Piper AMM 767-617 ch 12-20-00. Complied with 90 day brake fluid reservoir fluid level check per Piper AMM 767-617 ch 12-20-00. Complied with 6 month cleaning and application of Age Master #1 in accordance with manufacturers' instructions. Complied with 12 month GFC 700 servo inspection per Piper AMM 767-617, Ch 22-10-00. Complied with 12 month main battery capacity check per Piper AMM 767-617 ch 24-30-00. Battery capacity is 106.0%. Complied with 30 day fire extinguisher condition and weight check per Piper AMM 767-617 ch 26-20-00. Complied with 12 month gauged fire extinguisher maintenance check per Piper AMM 767-617 ch 26-20-00. Complied with 90 day ELT transmitter self-test. Complied with 12 month 14 CFR 91.207(d) inspection of the ELT for proper installation, corrosion and operation of controls and sufficient radiated signal. Battery expires June 2023. Complied with 12 month/ 200hr fuel return functional test in accordance with Piper AMM 767-617, Ch. 28-20-00. Complied with 12 month/ 100hr G3000 and Trim Annunciator checks in accordance with Piper AMM 767-617, Ch. 34-20-00. Complied with 12 month/ 100hr Avionics Cooling Fan Fail Annunciator check in accordance with Piper AMM 767-617, Ch. 34-20-00. Complied with 12 month Aspen EBO inspection in accordance with Piper AMM 767-617, Ch. 34-20-00. Complied with 90 day inspection of oxygen cylinder in accordance with Piper AMM 767-617, Ch. 35-10-00. Complied with 12 month pilot's oxygen mask test in accordance with Piper AMM 767-617, Ch. 35-10-00. Complied with Piper SB 1318A, fuselage station 144.25 rivet replacement Part II, by installing kit PN 88624-701 per SB instructions. Complied with Piper SB 1315, cabin door threshold rivet replacement by installing 6 ea. NAS1097KE4 fasteners, 2 ea. NAS1097KE5 fasteners, and fabricated access panel PN SB1315-1 per SB instructions. Adjusted A/C compressor drive belt tension to within limits in accordance with Piper AMM 767-617, CH. 21-50-00. Adjusted alternator drive belt tension to within limits in accordance with Piper AMM 767-617, Ch. 24-30-00. Adjusted LH and RH MLG wheel toe-in/ toe-out as required to eliminate excessive tire wear in accordance with Piper AMM 767-617, Ch. 32-10-00. Installed new seals PN 187-628, 485-082, and 484-797 in LH and RH MLG shock struts in accordance with Piper AMM 767-617, CH. 32- 10-00. Serviced struts with nitrogen and hydraulic fluid per Piper AMM 767-617, Ch. 12-10-00. Removed surface scratch in co-pilot's windshield using Optica 4 Scratch Removal System PN 51-860 per Piper AMM 767-617, Ch. 56-00- 00. ----- Continued on next page (1 of 2) ----- Al RC RAFT LOG Date Aircraft Time Recorder This Date Total Reading Maintenance llrl'1,,.r...t -- Continued from previous page (2 of 2) -- Fabncated and installed airframe interface kit model PN BM-AIK2 for BatteryMINDer charging system using MIL-W-22759/16 wire, 10A inline fuse. and SBS0 plug ,n accordance with AC43-13/1 B Removed LH MLG tire PN 185F88-6, SN 63622349 and installed new t,re PN 185F88-6, SN 80872087 In accordance with Piper AMM 767- 617, CH 32-40-00 Removed RH MLG tire PN 185F88-6, SN 63582346 and installed new tire PN 185F88-6, SN 80852306 In accordance With Piper AMM 767- 617, CH 32-40-00 Repaired minor nick in cabin door seal using RlV 157 as required, ref Piper AMM 767~617, Ch 52-10-00 Removed and replaced with new, center elevator static wick base PN 452-124 in accordance with Piper AMM 767-617, Ch 23~0-00 AdJUSted NLG and LH MLG squat switches to Within limits in accordance with Piper AMM 767-617, Ch 32~0-00 AdJusted NLG steenng arm clearance to w1th1n limits in accordance with Piper AMM 767-617, Ch 32-20-00 Serviced vapor cycle cooling system with R134A refrigerant as required In accordance with Piper AMM 767-617, Ch 21-50-00 Removed debns from and cleaned AFT evaporators and evaporator drams Accomplished all required operational and functional checks with satisfactory results I certify that this Aircraft has been inspected in accordance with an Annual InspectJon and Is determined to be in an airworthy condition Pertinent de I are n fil u der the above work order Signed ~~~~6£..VL----- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C •·•·•·• ·········~.•.•················· Total To :::::::~:::~:::::::::::::::::::::::::: Carry Forward =.==.==.===== .. ======================~=~=r .. .............. - and Remarks Airframe N39NG Model: PA....S-600TP SIN: 4698039 Date: 5 July 2018 Registration No. ___________ _ Signature I~C. Certificate No. Hobbs Time: 114.6 Total Time: 114.6 Landings: 112 Work Order: S-18-00216 Compiled with Piper SB 1327 by venfy1ng the Clearance on the cable guard per the service bulletin instructions, no defects noted Compiled with Piper SB 1328 by replacing control yoke aileron cable guards per service bulletin instructions and Piper drawing 46F44A701 rev A Installed new #3 decal on LH ·N· numbers and 2 new eo• h anniversary decals after paint was touched up by Aircraft Refinishing Corp Ac:compllshed all required operational and functional checks with satisfactory results The Aircraft identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Admin1strat1on and 1s approved for return to service Pertinent details are on file under the above work order Signed -~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Airframe ~ N39NG Hobbs Time: 287 .8 Model: PA-46-600TP I --C Total Time: 287.8 SIN: 4698039 -- ~ Landings: 280 Date: 17 July 2019 l<l'll'\e"" Clt:v Avll'l" 1 ",.. C"~"'""" Work Order: S-19-00176 A-19-00285 Complied with an Annual inspection using Piper PA-46-600TP AMM 767-617 ch 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. . Complied with 50hr oleo strut inspection per Piper AMM 767-617 ch 12-10-00. complied with 400hr / 12 month airframe lubrication items per Piper AMM 767-617 ch 12-20-00. Complied with 500hr cabin pressurization system test per Piper AMM 767-617 ch 21-30-00. Complied with 12 month GFC700 inspection per Piper AMM 767-617 ch 22-10-00. complied with 300hr starter generator inspection per Piper AMM 767-617 ch 24-30-00. Removed starter P/N 601-928 SIN 0047 and installed new starter/ generator PIN 601-928 S/N 0167 per Piper AMM 767-617 ch 24-30-00. Complied with 200hr 1120 day main battery capacity check (98%) per Piper /\MM 767-617 ch 24-30-00. complied with 30 day check of the fire extinguisher per Piper AMM 767-617 ch 767-617 ch 26-20-00. Complied with 12 month inspection of the fire extinguisher per Piper AMM 767-617 ch 26-20-00. Complied with 12 month 14 CFR 91.207(d) inspection of the ELT for proper installation, corrosion and operation of controls and sufficient radiated signal. Battery replacement due 6/2023. Complied with 90 day ELT system self-test per Piper AMM 767-617 ch 25-60-00. Complied with 500hr replacement of the elevator down spring by installing new spring P/N 46F40V001-001 per Piper AMM 767-617 ch 27- 30-00. Complied with 200hr I 12 month fuel return system test per Piper AMM 767-617 ch 28-20-00. Complied with 500hr landing gear warning switch tast. Complied with 500hr / 2 year inspection of the fuel strainerl:. and fuel probes per Piper AMM 767-617 ch 28-10-00. Complied with 90 day check of the hydraulic fluid level per Piper AMM 767-617 ch 12-10-00. Complied with 6 month cleaning and application of Age Master #1 in accordance with manufacturers' instructions. Complied with 90 day brake reservoir check per Piper AMM 767-617 ch 12-10-00. Complied with 12 & 24 month inspection5 of the Aspen EBO stand by instrument per Piper AMM 767-617 ch 34-24-00. Complied with 90 day inspection of the oxygen cylinder per Piper AMM 767-617 ch 05-30-00. Complied with 300 hour inspection of the oxyge!1 cylinder per Piper AMM 767-617 ch 35-10-00. Complied with 12 month mspection of the Pilots 02 mask per Piper AMM 767-617 ch 35-10-00. Complied with 400hr / 24 month fuel purge system inspection per Piper AMM 767-617 ch 71-70-00. Complied with 24 month cal:bration of Garmin GAE43 per Piper AMM 767-617 ch 34-25-02. Complied with 500hr inspection of Garmin G3000 per Piper AMM 767-617 ch 34-25-01. Complied with 24 month magnetometer calibration per Piper AMM 767-617 ch 34-25-01. Complied with 12 month inspection of the engine mount to fuselage bolts per Piper AMM 767-617 ch 05-30-00. Complied with AO 2019-12-12. effective date 12 July 2019, para (h)(1) by performing the rivet replacement per Piper SB 1332A part Band para (h)(2} by r~moving the AFM revision and ground limitations placards. No further action required. A!> 2018-14-01, effective date 25 July 2018, previously complied with by incorporation of Piper SB 1318A part 2 and installation of kit 88624-701 at 114.3 AFTT, 26 June 2018. Per Piper SB 13188, no further action is required if the aircraft was already in compliance with SB1318A part 2 at the time of rPv1sioi'\. No further action required. A02018-21-!.!, effective date 27 Mar 2019, not applicable by PIN of installed mask (MC1 0-16-105). No further action required. -----Continued next page (1 of 3)----- = -----CoNtnued from previous page--- Complled wtth Piper SB 1326A by m001fymg the propeller heat sensor wlrmg per the service bulletin Instructions Complted wtth Piper SB 1332A part B by removing the engtne / engine mount assembly, replacmg the required nvets and remstal~ng the enoine I mouAt assembly per the instruction m part 8 of the service bulletin Comolted Witt, Piper SB 1333A by Installing new boits PIN NAS1160-9-200, washers PIN MS2199C10 and NAS1149F1063P, MS2129-9-9, 407-601 and 690-633 to achieve the proper gaps m the left and nght forward wmg fittings per the servace bulletln instructions ComP'+ed w~ Piper SB 1334A by relocattng El panel and 'Mndshleld heat relay ground wiring per service Wletin instructions Compiled with 100hr I 12 month aHeron sector bearing Jubricabon per Piper SL 1131 A Compiled with Piper SL 1228A by lnstatting additlonal clamps on el\~ne winng harness per seMce letter instructions Complied with Piper SL 1231 by mstaMmg Fhghtstream 510 card PIN 011-03595-05 SIN 590001236. Comp{1ed with Piper SL 1244 commun1cat1on w1nng ground ~mprovements per service letter instructions Complied wfth Piper SL 1247 inspection of hyd-rautlc hoses tnstalled new mner and 01Jter hoses PIN 566-670 on the left and right mam gear actuators per Piper AMM 767-617 ch 29-00-00 Complied with Piper SL 1249 by lnspeot1ng control cokJmn for bmdmg, no discrepancies noted Complted With Piper Sl. 1259 by instalt.ng Garmin G3000 software version 2039 15 per service letter instructions Aspen MSB S02018-01 not apphcable by current software version (2 6 3 lnstalled) Piper Specfal Advisory 46-28 not appf~e by senal number Tested and mspected #1 Garmin ADC PIN 011-00882-10 SIN 20624188 from -1,000ft to 30,000ft as r~1.11red by FAR91 411(a)(1) and was found to comply with appendices E and F of FAR 43 Tested and mspected #2 Garmin ADC PIN 011-00882-1 O SIN 20624193 from -1,000ft to 30,000ft as required by FAR91 411 (a)(1) and was found to comply with appendices E and F of FAR 43 Tested and msp~ed standard att.irMter PIN 910-00001-501 SIN 24364 from -1,ooon to 30,000ft as required by FAR91 411(a)(1) and was found to oomply with appendix E of FAR 43 Tested and inspected transponder #1 P,N 011-00779-3-0 SIN 89130597 as required by FAR91 413(a) and was found to comply With appendix F of FAR 43 Tested and inspected transponder #1 PIN 011-00779-30 SIN 89135129 as required by FAR91 413,(a) and was found to comply wrth appendlx F of FAR 43 Tested an<il inspected atroraft static system to 3'J.OOOtt as ,requlfed by FAR91 ~11(a)(1) and was found to comply Wlth appendices E and F of FAR 43 Removed t.ft transducer assem~y PIN C-5507-2 SIN 172223-03 and in~ modified assembly PIN C-5507-2 SIN 172223-05 per Ptper A.MM 767-617 ch 27-30-00 UM mo<Med by Safe Fhght tnstrument Corp FM CRS# QA1R419K on WIO 51026 Performed albtude data caltbraoon on the Aspen EBO per Aspen A\•lonlcs Tech Note 2009-09 Rev D Adjusted attemator beU dnve tenStOn per Piper AMM 767-617 ch 24-30-00 Adjusted A/C compressor belt drive teflston per P,1per AMM 767-617 ch 21-50-00 lnstatled new LH lightning dlverter stnp PIN 272-226 USfflQ "Jt PIN 88559-003 per Piper drawmg r.-umber 88559 Re-appi,ed edge seater to aut01I de-l~r boots In~ new TB22 and TB23 terminai blocks P:N 475-~44 per P•per AMM 767-617 ch 91-28-40 and cat1brated fuel tank gauges per Peper AMM 767-617 ch 28-40-00 Touched up extenor pamt as requued Trimmed lower cabin door skm a~ comer to prov•de proper olearance to fus~age skm ----Co,1tAnued next page (2 of 3)---- --Continued from previous page (3 of 3)-- lnstatled new should harness tnm covers PIN 594-016 at the pilot. copilot #1 passenger and #2 passenger seat positions Sealed minor nicks in cabin door seal with R1V1 57 Pohshed light surface scratches from pilot's side window and #1 passenger side cabin window per Piper AMM 767-617 ch 56-00-00 Installed new LH & RH aileron gap seals PIN 46W-430047-001, -46W430068-001 and 46W430067-001 per Piper AMM 767-617 ch 57-50- 00 Installed new cabin drain placard PIN 656-250 on fuselage belly skin Installed new LH and RH MLG brake shims PIN 068-0-4100 per Piper AMM 767-617 ch 32-40-00 Installed new o-nng PIN •e•-eoe on brake reservoir cap Installed new grommet P/N 217-30653 on NLG wheel half per Piper AMM 767-617 ch 32-40-00 AdJusted aileron, pitch and yaw servo cable tensions per Piper AMM 767-617 ch 22-10-00 AdJusted elevator tnm cable tension per Piper AMM 767-617 ch 27-30-00 AdJusted elevator primary cable tension per Piper AMM 767-617 ch 27-00-00 Adjusted rudder cable tens10n per Piper AMM 767-617 ch 27-20-00 Adjusted aileron cable tension per Piper AMM 767-617 ch 27-10-00 Blended hght surface scratches on lower fuselage skins Adjusted nap jack screw ngging per Piper AMM 767-617 ch 27-50-00 Accomplished all required operatJonal and functional checks with satisfactory results I certify that this Aircraft has been inspected In accordance with an Annual inspection and Is determined to be in an airworthy condition Pertinent details are on file under the above work order Signed ---,.r-7-;;i __,.,.t:?~------- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C ·•••••••••·•••••••·•••·•••·•••·•·•·•·•·•· Total To :::::::::::::::::::::::::::::::::::::::: ···········--··················· •·•·• Carry Forward :::::::::::::::::::::::::::::::::~:::::; - - Airframe N39NG Model: PA..-6-600TP SIN: 4698039 Date: 1 November 2019 Resecured Pilot's PFD with existing hardware Bled brakes per Piper PA◄ 6-600TP AMM 767-617 chapter 32 ◄ 0-00 Hobbs Time: 337.7 Tout Time: 337.7 Landings: 328 Work Order: 5-19-003"8 Reset Fuel Flow Transducer K factor In the G3000 system per Piper PA◄ 6-600TP AMM 767-617 Ch 3'4-25-02 Complied with Piper SL 1236 by mspecllng and tnmmmg upper channel flange adjacent to nose gear trunnion per Piper SL Instructions Complied With Piper SB 1339~ Generator Relay (K303) Replacement Installed SB Kit PIN 86-46-002 per SB mstructlons Removed left wheel, deflated tire, removed tire PIN 185F88-6, SIN 83-40205'4 and mstalled new tire PIN 185F88-6, SIN 83362021, and 0- ring PN MS28775-261 Serviced and reinstalled wheel per Piper AMM 767-617 Ch 32--40-00 Removed nght wheel, denated tire, removed tire PIN 185F88-6, SIN 83392237 and mstalled new tire PIN 185F88-6, SIN 83-412275 and 0- nng PIN MS28775-261 Serviced and reinstalled wheel per Piper AMM 767-617 Ch 32--40-00 Aligned mam wheels per Piper PA-'46-600TP AMM 767-617 chapter 32-10-00 Performed Lightning Strike mspectlon per Piper PA-'46-600TP AMM 767-617 Ch 5-50-00 Adjusted alignment of propeller deice brushes by adding two shims P/N 1E1157 per Piper AMM 767-617 Ch 30-60-00 Inspected R/H and UH elevator spar per Piper SL 1272 No d1screpanc1es noted Performed Op Check of Traffic and ADS-B operation as per G3000 Pilots Guide Removed Emergency Bieeda1r valve PIN 592-657 SIN 0717 and replaced with new PIN 592-657 SIN 08'47 per Piper PA-'46-600TP AMM 767-617 Ch 21-20-00 Accomplished all required operational and functional chc-cks with satisfactory results The Aircraft 1dent1fied above was repaired and inspected m accordance with current Regulations of the Federal Aviation AdministratJon and 1s approve~retum lo service Pertinent details are on file under the above work order Signed /2---- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Airframe -.~c. N39NG Hobbs Time: 355.3 Model: PA-46-iOOTP Total Time: 355.3 SIN: 4698039 Landings: 346 Date: 3 February 2020 ~ c.:y .... -.riabon Cena,,- Work Order: S-19-00420 Compiled W\th an Annual inspection using Piper PA-46-600TP AMM 767-617 ch 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D Complied with 50hr oleo strut mspectJon per Piper AMM 767-617 ch 12-10-00 Complied with 90 day check of the hydraulic fluid level per Piper AMM 767-617 ch 12-10-00 Complied with 90 day brake reservoir check per Piper AMM 767-617 ch 12-10-00 Complied with 400hr / 12 month airframe lubncation items per Piper AMM 767-617 ch 12-20-00 Complied W\th 12 month GFC700 Inspection per Piper AMM 767-617 ch 22-10-00 Complied with 300hr starter generator Inspection per Piper AMM 767-617 ch 24-30-00 Complied wtth 200hr / 120 day main battery capacity check (96 1%) per Piper AMM 767-617 ch 24-30-00 Comphed with 30 day check of the fire extinguisher per Piper AMM 767-617 ch 767-617 ch 26-20-00 Compiled with 12 month Inspection of the fire extinguisher per Piper AMM 767-617 ch 26-20-00 Complied with 12 month 14 CFR 91 207(d) inspection of the ELT for proper installation, corrosion and operation of controls and sufficient radiated signal Battery replacement due 6/2023 Complied With 90 day EL T system self-test per Piper AMM 767-617 ch 25-60-00 Comphed With 36 month replacement of the Aspen EBO battery by removing battery PIN 409-00003-001 SIN 164800082 and installed new battery PIN 409-00003-001 SIN 193700110 per Piper AMM 767-072 ch 34-24-00 Tested and inspected aircraft static system to 20,000ft as required by FAR91 411 (a)(2) and was found to comply with appendices E of FAR 43 Compiled with 36 month inspection of the GSA ex servo per Piper AMM 767-617 Ch 22-10-00. Complied with 12 month inspection of the Aspen EBO stand by instrument per Piper AMM 767-617 ch 34-24-00. Complied With 200hr / 12 month fuel retum system test per Piper AMM 767-617 ch 28-20-00 Complied with 6 month cleaning and application of Age Master #1 in accordance With manufacturers' instructions Complied With 90 day Inspection of the oxygen cylinder per Piper AMM 767-617 ch 05-30-00 Complied with 12 month inspection of the Pilots 02 mask per Piper AMM 767-617 ch 35-10-00 Complied with 12 month inspection of the engine mount to fuselage bolts per Piper AMM 767 -617 ch 05-30-00 Comprled with 100hr I 12 month aileron sector beanng lubncation per Piper SL 1131 A Complied with SIL 1272 by visual Inspection of elevator spar flanges per S/L lnstruct1on No defects noted Recurring inspection due in 100hra of operation. AdJusted alternator dnve belt tension to be within limits per Piper AMM 767-617 Ch 24-30-00 Complied wrth serviceab1hty check on windshield heat system per Piper AMM 767 -617 Ch 30-40-00 Removed and replaced wiper PN 187-628, o-nng PN 484-797, and backup seal PN. 485-082 tn left matn strut Serviced strut Work performed tn reference to Piper PA-46-600TP AMM PN 767-617 chapters 32-10-00 and 12-10-00 Removed and replaced wiper PN 187-628, o-nng PN 484-797, and backup seal PN 485-082 in nght main strut Serviced strut Work -- performed 1n reference to Piper PA-46-600TP AMM PN 767-617 chapters 32-10-00 and 12-10-00 -(Continued on next page 1 of 2)-- ~ == - - - - -(Continued from previous page 2 of 2)-- Removed one static wick from elevator and replaced with new PIN 767-617 per Piper AMM 767-617 ch 23-60-00 Serviced hydraulic reserv01r per Ptper M600 AMM 767-617 Ch 12-10-00 Accomplished all required operational and functional checks with satisfactory results I certify that this Aircraft has been inspected m accordance with an Annual inspection and Is determined to be In an airworthy cond1t1on Pertinent details are on file under the above work order Signed 0--- Olathe KS 66062 (913) 782-0530 FAA Repacr Station #AMYR171C Airframe I~C. N39NG Hobbs Time: 374.2 Model: PA--'6100TP Total Time: 374.2 SIN: 4698039 Landings: Date: 10 April 2020 ~ Cit¥ A"4aaon Cane-- Work Order: A-20-00155 .. Removed #2 AOC PIN 011-00882-10, SIN 20624193 and installed overhauled #2 AOC P/N 011-00882-10, SIN 20609728 per Piper AMM 767-617, Ch 34-25-01 Installed ADC overhauled by Garmin lntemat,onal, CRS #G6XR582Y on W/0 15080547 Leak checked to 12,700 fl as per Piper PA--16-600TP M600 AMM 767-617 Ch 34-10-00 and Tested as required by FAR 91 411(a)(3), and was found to comply with paragraph (c). appendix E of FAR 43 Unit was inspected and tested as per requirements of 14 CFR Part 91 411 up to 55000 ft by repair facility Accomplished all required operational and functional checks wcth satisfactory results The Aircraft 1denbfied above was repaired and inspected In accordance with current Regulations of the Federal Aviation Admcmstration and Is approved for etum o s Pertinent details are on file under the above work order Signe Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Airframe N39NG Hobbs Time: 385.2 Model: PA-46-iOOTP SIN: 46989039 I~C. Total Time: 385.2 ====-. Date: 9 June 2020 Landings: Work Order: S-20-00150 AdJusted NG to be withm ltm1ts IAW Piper AMM 767-617 Ch 71-00-00 Acx:ompf1shed all requrred operational and functional checks with satisfactory results !he Aircraft Identified above was repaired and mspected m accordance with current Regulations of the Federal Aviation Administration and 1s approved for return to seMce Pertinent details are on file under the above work order Signed ~ '2---- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C 1 Airframe I~C. N39NG Hobbs Time: 392.0 Model: PA-46-iOOTP Total Time: 392.0 SIN: 4698039 Landings: Date: 1 July 2020 ~OevA-c.nllDI- Work Order: S-20-00174 Removed A/C compressor assy PIN 557-802 SIN 0561012680 and replaced with new P/N 557-802 SIN 0134311980 and new seals PIN 485-196 and PIN 485-198 at refngerant hose connecbons Serviced system with 2 75 pounds of 134a refngerant per Piper AMM 767-617 Ch 21-50-00 Removed accessory dnve pulley attaching hardware. inspected dnve shaft and pulley 1nstallat1on No defects noted Resecured pulley with new nut PIN AN310-8, new washer PIN NAS1149F0832P, and cotter pm P/N MS24665-285 per Piper AMM 767-617 Ch 72-60-00 Installed new a,r cond1tJoner dnve belt PIN 73965-024 per Piper AMM 767 -617 Ch 21-50-00 Installed new alternator dnve belt PIN 73965-023 per Piper AMM 767-617 Ch 24-30-00 Accomplished all required operat10naf and functional checks with satisfactory results The Aircraft identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Admm1strat1on and 1s approve~r return to service Pertinent details are on fife under the above work order Signed ~ r:2--- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C . •: •: •: •: •: •:•:•:•:•: •:• :•:•·• :• ........ Total To .......................... , •:•.•: •:•:•:. ••·•·•·•·•·•••·•·•·•·•·•·•·•·•·•·• ••• Corry Forward :~:~:~:~:~:~:~:~:~:~:~:~:~:f ~@t - - - - - - Airframe N39NG Model: PA'""6-600TP SIN: 4698039 Date: 16 September 2020 I<c C. ~ ~Avtatoan ~ Hobbs Time: 413.4 Total Time: 413.4 Landings: Work Order: A-20-00418 Removed #2 ADC PIN 011-00882-10, SIN 20609728 and installed overhauled ADC PIN 011-00882-10, SIN 206088CM per Piper AMM 767- 617, Ch ~-25-01 Installed unit overhauled and tested as required by FAR 91 411(a)(3} to comply with paragraph (c}, appendix E of FAR 43 by Garmin International, CRS #G6XR528Y on W/O 152636~ Accomplished all required operational and functional checks with satisfactory results The A1rcra was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and Is ap v,w.,_ ce Pertinent details are on file under the above work order Signe '-,&~~1£.{j~q--- ____ _ Olathe KS 66062 (913} 782-0530 FAA Repair Station #AMYR171C +MEAD • "c.••• ••""1c1, flllC KAN ■ A ■ C ITV 12931 W 151s1 STREET I OLATHE. KS 66062 j 620-960-7720 I MEADAIRCRAFT@GMAIL COM Airframe log entry 9-29-2020 N39NG PA46-600TP S/N 4698039 HM 418.1 hrs Installed new LH and RH brake linings and LH brake disc. Installed new LH and RH brake cylinder shims. Serviced tires and conditioned 11 g . Operations are satisfactory. Kevin Mea ~ A&P 443641987 9-29-2020 ~------------- Total Carry To +MEAD KANBAB CITY 12931 W 151" STREET I OLATHE KS 66062 I 620-960-7720 I MEADAIRCRAFT@GMAIL COM I Airframe entry 9-18:2020 7 N39NG PA46-600TP. S/N 4698039 HM 417.0 hrs Installed Tanis PN TSTPTGA-3057-115 engine preheater system on engine. Installed plug receptacle under RH clamshell door. The system is an independent AC ground operational minor alteration system. Weight and bal changes are negligible. Kevin Mead . A&P #443641987 9-18-2020 ~----___,......,._ ___ _ - •:::::::::::::::::::::::::::::::::::::::•••••••·•••••••·•••·•·•·•·•••·•·•·•·•·•· forward :::::::::•:•:•:•:::•:•:•:•:•:•:•:•:•:•:• .... ·•·•·•·•· ·•·•·•·•·•·•·•·•·•·•·•· •:•:•:•:•:•:•:•:•:•:•:•:•:•:•:•:•:•:•:•:• - - - - - - > Registration No. ___________ _ 2802 Old Tow.r Road Phoemx Arizona 85034 &02-217~70 Phone &02-217 ◄ 030 FAX LHi111t U1f lw111•ts, of A~tlOII FAA Rep,ilr Station No. EKGR571O Model PA ◄ 6.600TP Aircraft Maintenance Record Work Order No Hour Meter Aircraft Total Time Landi s 02M-12416 Serial No. Registration P e 4698039 N39NG 1 of 2 458.8 458.8 465 Ss-brdulrcf Ma,ntrnann or 1n,p«t1on, ... 1 • Complied with Annual Inspection per CFR Title 14 Part 91 409(a)(l) and CFR Title 14 Part 43 Appendix D usmg Paper PA-46-600TP MM 05-20-00 Events 1 & 2 as a gmde • Current re-.,1s1on for POH VB-2366 1s at Rev 4 1l1e POH for N39NG 1s current and at Rev 4 Dated December 17.2017 • CW 3 month check of brake reservoir for proper fluid level. leal..s, cond1t1on and secunty Reference Piper PA-46-600TP MM 12-10-00 • C/W 3 month check of fluid m hydraulic pump reservoir Reference Piper PA-46-600TP MM 29-10-00 • C/W 3 month v,sual inspection of oxy1,1cn C)'lmdt!r Reference Piper PA-46-600TP MM 35-10-00 • C/W 6 month capacity check of mam ship battery Battery passed capacity check at 90% Recharged and reinstalled battery Work perfonned m reference to Piper PA-46--600TP MM 24-30-00 and Concorde RG Sencs CMM 5.0171 • C'W 12 month cond1t1on check and charge of portable fire extmgmsher Placard mstalled Reference Piper PA-46-600TP MM 26-20-00 • C'W 12 month/ 200 hour functional test of fuel return system Reference Paper PA-46-600TP MM 28-20-00 • CIW 12 month test of Pilots OX)'gen ma~k S)stem Operational test good Reference Piper PA-46-600TP MM 35-10-00 • C/W 12 month mspcct1on and operational check of the ELT system per CFR title 14 part 91 207(d) Operational test tood. Reference Piper PA-46-600TP MM 25-60-00 • • • • • • • • • • • C/W 12 month mspect1on ofGFC 700 system m reference to Piper PA-46-600TP MM 22-10-00 CJW 12 month lubncat1on Reference Piper PA-46-600TP MM 12-20-00 C/W 12 month/ 100 hour mspecllon of the Gannm 03000 system with reference to Piper PA-46-600TP AMM section 34-25-01 C/W 12 month Aspen EBO standby instrument mspccllon Reference Piper PA-46-600TP AMM section 34-24-00 C/W 24-month test and mspcct1on of each ah1meter, static pressure system, automatic pressure reporting system. and ATC transponder's requmed by CFR Title 14 Part 91 411 and 91 413 ll1e integrated systems were found to comply with Appendices E & F of 14 CFR part 43. The ahnneters were tested to 30,000 feet C/W 24 month cahbrat1on of the GAE 43 / SAE 5-35 encoder Reference Paper PA-46-600TP AMM section 34-25.01 . C/W 24 month Reuhbrallon of magnetometers Operational tests good Reference Paper PA-46-600TP MM 34-25.0 I OW 50 hour check of oleo struts for proper extension and C\.1dence of fluid leakage Reference Piper PA-46-600TP MM 12• I 0-00 C.'W 300 hour mspecllon ofstarterlgeneralor brushes 75•;. hfc remammg Reference Paper PA-46-600TP MM 24-30-00 . C'W 400 hour lubncation reqmrements Reference Piper PA-46-600TP MM 12-20-00 C/W 500 Hour mspect1on of Ganmn O,000 system with reference lo Piper PA-46-600TP AMM section 34-25-01 FAA R r Stabon No EKGR571D - - > u,,,,., tllf a.isillfH of Av,etlOII 2I02 Old Tower Road Phoenix Arizona 85034 FM Repair Station No. EKGR571 D o;~crtoans:ia • Installed new carbon block PIN 968 29 11 375 Reference Piper PA-46-600TP MM Chapter 61-10-00 602-267-4070 Phone 602-217-4030 FAX • Installed new RH aileron outboard static wick base PIN 452-124. and a new static w1cl.. PIN 456-904 electrical bond 1s good Reference Paper PA46-600TP M M chapter 23-60-00 • • • Removed \\om 11re PIN I85F88-o SIN 83412275 from 1./H MLG wheel, disassembled wheel assembly PIN 40-483 SIN I 096. cleaned and perfonned vtsual inspection on wheel halves and boll with no defects noted Installed new tire PIN 185F88-o SIN 01420106 on LH mam wheel assembly Installed LH main wheel assembly Work pcrfom1cd m reference to Piper PA-46-o00TP MM 32-40-00 Removed wom 11re PIN I85F88-o SIN 83412275 from R/H MLG wheel. disassembled wheel assembly PIN 40-483 SIN I 096, cleaned and perfom1ed visual mspecllon on wheel halves and boll with no defects noted Installed new tire PIN 185F88-6 SINO 1400160 on RH mam wheel assembly Installed RH main wheel assembly Work performed m reference to Piper PA-46-o00TP MM 32-40-00 Removed nose wheel ttre PIN 505C0l-2 SIN 80302265 Disassembled wheel assembly P/N 40-77H SIN 1104. cleaned and inspected wheel assembl). no defects noted lnstalh:d new Inner tube PIN 302-013-400, and tire PIN 505C01-2 SIN 02970270 Reference Piper PA-46- 600TP MM 32-40-00 • Set elevator cable tensions and secured the tumbuckles with new locking claps PIN MS2 I 256- I Reference Piper PA-46-600TP M M Chapters 27-00-00. 27-10-00 fig 3, and 27-30-00 • Installed new LH brake insulator slum PIN 068-04100 SIN NI A Reference Piper PA-46-600TP MM 32-40-00 • Installed new left brake disk PIN 164-21000 on LH main "heel assembly Reference Piper PA-46-600TP MM 32-40-00 • Installed new nght brake disk PIN 164-21000 on RH main wheel assembly Reference Paper PA-46-600TP MM 32-40-00 Ainrnrrhinqs Dn::utht'S or S,nricr BuUrtjns • CIW Piper SL 1236 - Channel mod1fica11on for nose landmg gear trunnion clearance No action required Gap 1s 0 4 mm allowable as 0 06 • C!W P11)\.'f SL 1279 I hgh-s1de current monitor cahbrat1011 No defects noted Reference Piper SL 1279 • CIW Piper SL 1286 B - Nose Landing Gear stccnng components mspccllon and adJustment No discrcpa11c1es noted • CW Piper Mandatory SB 1308 - Wet-Wmg Fuel Access Cover lnspecuon, no defects noted • Piper Mandatory SB 1341 previously complied with Verified PIN of previously installed Lift Transducer PIN C-55007-2 Mod A No further maintenance action required Work performed m reference to SB 1341 • C/\V Piper Mandatory SB 1360A - AILERON DRIVE SECTOR INSPECTION No defects noted • C/W Piper Mandatory SBIJ64 - Fuel quantity capacitance probe check Operational test good Work performed in reference to Piper PA- 46-600TP MM 28-40-00 and SB 1364 • AD's reviewed through Biweekly 2021-05 The aircnft and for component identified above was repaired and Inspected In accordance with current federal aviation regulations and Is approved for return : •~::~Kped ;;?" performeZ2 "' on file 11 u,i, "'""' shllon. Kevin Reedy Date. MAR 18, 1011 FAA Re air Station No. EKGR5710 -- . - Airframe N39NG Model: PA-46-600TP S/N: 4698039 Date: 16 April 2021 . . Replaced fuse (F425) in Gen 2 voltage regulator voltage sense circuit with new PIN 461-684. Hobbs Time: 465.2 Total Time: 465.2 Landings: Work Order: S-21-00109 S-21-00105 Complied with 6 month cleaning and application of Age Master No.1 in accordance with the manufactures instructions. Removed NLG squat switch and squat switch bracket. Installed new switch PIN 87545-010 and bracket PIN 101711-002. Adjusted NLG squat switch per Piper AMM 767-617 Ch. 32-60-00. Accomplished all required operational and functional checks with satisfactory results. The Aircraft identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is approved for return to service. Pertinent details are on file under the above work order. Signed~ Model: SIN: Date: Airframe N39NG PA-46-600TP 4698039 13 January 2022 Olathe KS 66062 ...• (913) 782-0530 FAA Repair Station #AMYR171C Hobbs Time: Total Time: Landings: Work Order: 524.9 524.9 535 S-21-00442 A-21-00527 Complied with an Annual inspection using Piper PA46-600TP AMM 767-617 Ch. 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. Complied with 50 hour inspection of the strut extensions per Piper AMM 767-617 Ch. 12-10-00. Complied with 12 month lubrication per Piper AMM 767-617 Ch. 12-20-00. Complied with 90 day brake fluid reservoir fluid level check per Piper AMM 767-617 Ch. 12-20-00. Complied with 90 day hydraulic pump reservoir fluid level check per Piper AMM 767-617 Ch. 12-20-00. Complied with 100hr 112 month GFC 700 servo inspection per Piper AMM 767-617 Ch. 22-10-00. Complied with 100hr 112 month G3000 checks per Piper AMM 767-617 Ch. 34-25-01. Complied with 500hr G3000 checks per Piper AMM 767-617 Ch. 34-25-01. Complied with 12 month main battery capacity check per Piper AMM 767-617 Ch. 24-30-00. Battery passed with 92.0% capacity. Complied with 12 month 14 CFR 91.207(d) inspection of the ELT for proper installation, corrosion and operation of controls and sufficient radiated signal. Battery Expires June 2023. Complied with 90 day El T transmitter self-test per Piper AMM 767-617 Ch. 25-60-00. Complied with 12 month rechargeable (Gauged) fire extinguisher maintenance per Piper AMM 767-617 Ch. 26-20-00. Complied with 30 day fire extinguisher condition and weight check per Piper AMM 761-617 Ch. 26-20-00. Complied with 200hr 112 month fuel return system functional check per Piper AMM 767-617, Ch. 28-20-00. Complied with 600 hour airframe fuel filter replacement by removing filter and replacing with new PIN 601-820 per Piper AMM 767-617, Ch. 28-20-00. ----- Continued on next page (1 of 2) ----- -- Continued from previous page (2 of 2) ----- Performed deaning and apphcatlon of Age Master #1 on pneumatic de-ice boots in accordance with manufacturers' instructions Complied with 100 hour inspection of the prop heater system per Piper AMM 767-617 Ch 30-60-00 Comphed with 12 Month Aspen EFD inspection and battery check per Piper AMM 767-617, Ch 34-24-00 Comphed with 90 day Inspection of the 02 cylinder per Piper AMM 767-617 Ch 05-30-00 Complied with 300hr inspection of the 02 cylinder per Piper AMM 767-617 Ch 35-10-00 Complied with 60 month hydrostatic test of 02 cylinder by removing and re-installing inspected 02 cylinder PIN 800112-24, SIN sr32689 per Piper AMM 767-617, Ch 35-10-00 02 cyhnder inspected by Aerospace Turbine Rotables INC, CRS #NV2R045L on WI0 wo 17673 8 Complied with 60 month cvemaul of 02 cyhnder regulator by removing and re-installing overhauled regulator PIN 800114-22, SIN 4 C17010594 per Piper AMM 767-617, Ch 35-10-00 02 regulator overhauled by Aerospace Turbine Rotables INC, CRS #NV2R04SL 0 W/O WO1767~1 n Complied with 12 month 1nspect1on of the pilot's oxygen mask per Piper AMM 767-617 Ch 35-10-00 Comphed with 60 month FWD and AFT honzontal stab1hzer attach fittings inspection for corrosion per Piper AMM 767-617, Ch 55_ 10 _00 Complied with 60 month elevator trim tab push rods corrosion inspection per Piper AMM 767-617, Ch 55-20-00 Comphed with 60 month FWD vertical stabilizer attach fittings corrosion inspection per Piper AMM 767-617, Ch 55-30-00 Comphed wrth 12 month inspection of the engine mount firewall bolts per Piper AMM 767-617 Ch 71-20-00 Complied with 400hr/24 month Fuel Purge System Inspection and cleaning per ~r PA-46-600TP AMM 767-617, Ch 71-70-00 Complied with 100hr / 12 month aileron sector beanng lubncat1on per Plper SL 1131A. Complied with Piper SL 1135 Cable and Pulley Inspection by inspecting aileron control cables and pulleys per FAA Advisory Circular AC 43 13-1 B CHG 1, Chapter 7, Section 8 Complied with Piper SL 1238 AIieron Gap Seal Removal by removing aileron gap seals per Part I and Part II of the SB Comphed with Pipe SL 1272 Elevator Spar Inspection per SL instructions Complied with Piper SL 12858 by servicing tires and installing placards PIN 100700-164 and 100700-163 (2 ea) per SB instructions Complied with Piper SL 12860 nose Landing Gear Steenng Components Inspection and AdJustment Complied with Piper SB 1371 by applying 1dentificat1on markings to wing hfe hm1ted parts per SB Instructions AD 2020-16-0SC, effective date 17 Aug 2020, not applicable to aircraft model PA-46-600TP. AD 2019-01-02, effective date 7 Feb 2019, not appltcable to aircraft model PA-46-600TP Removed alternator dnve belt and installed new drive belt PIN 73965-023 per Piper AMM 767-617, Ch 24-30-00 Installed new wiper PIN 187-628, nng seal PIN 485-082, and O-nng PIN 484-797 tn LH MLG oleo strut assy per Piper AMM 767-617, Ch 32-10-00 Installed new wiper P/N 187-628, nng seal PIN 485-082, and O-nng PIN 484-797 in RH MLG oleo strut assy per Piper AMM 767-617, Ch 32-10-00 Installed new O-nng P/N 484-808 on brake reservoir cap Repaired passenger door weather seal using RTV157 Gray as required. Re-applied filet sealant around #1, 2, 3 and entry door cabin windows using PR1425B1-2 sealant as required Re-applJed bead sealant around LH and RH wing stall strips using PR1425B1-2 sealant as required Removed RH AFT elevator trim control rod and installed new elevator trim control rod PIN 102846-002 per Piper AMM 767-617, Ch 27-30- 00 Accomplished all required operational and functional checks with satisfactory results. I certify that this Aircraft has been Inspected tn accordance with an Annual inspection and 1s determined to be in an airworthy condition Pertinent de ils ar I under the above work order Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C - - Altitude correction Altitude correction Altitude correction # 1 PFO #2PFO ~ Stby Ind Airframe Actual Indicated Actual Indicated Actual Indicated N39NG -1000 ·1010 -1000 -1000 -1000Model: PA--16100TP SIN: 469 0 -10 0 0 0 Date: 10 January 2023 500 490 500 500 500 Complied with an Annual Im 1000 990 1000 1000 1000 the inspection requirements 1500 1490 1500 1500 1500 Complied with 50 hour inSPfl Complied with 50 hour mspE 2000 1990 2000 2000 2000 Compiled with 90 day ElT u Complied with 30 day fire e,- 3000 2990 3000 3000 3000 Complied with 12 month rec 4000 3990 4000 4000 4000 Complied with 90 day hydra• Complied With 90 day brake 6000 5990 6000 6000 6000 Compiled with 90 day mspe"' 8000 7990 8000 8000 8000 Performed cleaning and app Complied with 12 month ins~ 10000 9990 10000 10000 10000 Complied with 12 month lubr Complied with 400 hour lubn 12000 11990 12000 12000 12000 Compiled with 12 month ms~ 14000 13990 14000 14000 14000 Compiled with 200hr I 12 me Complied with 12 month 14 1 16000 15990 16000 16000 16000 radiated signal Removed El 011 per Artex ElT 1000 Mai 18000 17990 18000 18000 18000 Complied with 48 month Fut: 20000 19990 20000 20000 20000Tested and inspected stand; and was found to comply wit 22000 21990 22000 22000 22000 Tested and inspected encod 25000 24985 25000 25010 25000 and was found to comply wit Tested and inspected Trans~ 30000 29980 30000 30010 30000 Appendix F of FAR 43 35000 34980 35000 35015 3S000 Tested and inspected Trans 1 40000 N/A 40000 N/A 40000 Appendix F of FAR 43 45000 N/A 45000 N/A 45000 Complied with 100hr I 12 mo Compiled with 12 Month Aspen EFD inspection and battery check per Piper AMM 767-617, Ch 34-24-00. Complied with 24 Month Aspen EFD inspection per Piper AMM 767-617, Ch 34-24-00 Complied with 36 Month/ 2200hr Aspen EFD battery replacement per Piper AMM 767-617, Ch. 34-24-00 Hobbs Time: 597.9 Total Time: 597.9 Landings: 608 Work Order: S-22-00681 ts as a guide to comply with 20-00 rers' instructions 1 of controls and suffiaent : 452-6504-1 SN 396883- 1ired by FAR 91 411(a)(1), Jired by FAR 91 411(a)(1), found to comply with found to comply with 1 of 3 , Compiled with 24 month recaltbratIon of the GAE 43 per Piper AMM 767-617 Ch 34-25-02. Complied with 24 month check of the magnetometer per.a,er,Mtffit767-617 Ch. 34-25-02. complied with Piper SL 1135 Cable and Pulley Inspection by inspecting aileron control cables and pulleys per FAA Advtsory Circular AC 43.13-1 s CHG 1. Chapter 7i.-§ectJon 8 Complied with Piper SL 12860 nose Landing Gear Steenng Components Inspection and Adjustment Complied with 100hr 112 month aileron sector bearing lubncatIon per Piper SL 1131A. Serviced tlres with nitrogen per Piper SL 1285C Complied with PIJ,tr SB 1369 Elevator Spar Inspection Part I Inspection per service bulletm instructions, no defects found Compiled with Piper SL 1314 Oxygen Generator Inspection per service bulletin Instructions, no defects noted Complied with AD 202l-11-10 effective date June 27,2022 Wing splice hfe l1m1t by incorporating section 4-00-00 of Ptper Aircraft Inc PA- 46-600TP, M600 AMM Airworthiness L1m1tations Page 1, dated August 31, 2021. Reducing the life limit of wing splice assembly PIN 46W57A100-001 to 3,767 hours, time-in-service. Performed composite repair of RH side of engine inlet duct extension with fiberglass mesh and f~ler as reqUtred Replaced brake reservoir cap o-nng with new PIN MS 28775-115 Re-bonded lower aft flap seal on UH wing as required using 1300L adhesive Re-torqued LH and RH MLG brake caliper piston bolts and bled brakes per Piper AMM 767-617 Ch. 32-40-00. Installed 4 ea new bushings PIN 453-781 and 2 ea new bolts PIN 691-315 on LH and RH MLG upper torque ~nk assy per Piper AMM 767-617 Ch. 32-10-00 Removed LH MLG tire PIN 185F88-6, SIN 01420106 and mst~led new tire PIN 185F88-6, SIN 21900106 per Piper AMM 767-617 Ch 32- 40-00 Removed RH MLG tire PIN 185F88-6, SIN 01400160 and installed new tire PIN 185F88-6, SIN 2190098 per Ptper AMM 767-617 Ch 32- 40-00 Installed new cam-loc receptacle PIN 584-219 on upper engine cowling. Serviced Hydraulic reservoir per Piper AMM 767-617 Ch CH 12-20-00. Removed and re-installed repaired Aspen EBO PIN 910-00001-501, SIN 24364 per P4per AMM 767-617, Ch 34-24-00 Installed EBO rep34red by Aspen Avionics, CRS #PT0999SW on WIO 7537143 This aircraft has been modified bv the following Installation: Removed sealed lead acid battery PlN RG-41, SIN 40878721 2 of 3 3 of 3 Installed new sealed lead acid battery PIN RG-41153, SIN 41245097 per Concorde Battery STC #SA01050DE and Concorde Battery STC OWG No 5-0692 Maintenance Requirements & Instructions for continued airworthiness: Ref Concorde Battery OWG No 5-0693 dated 11 Jun 2020 for instructions for continued airworthiness and Aircraft weight and balance updated Accomplished all required operational and functional checks with satisfactory results. maintenance requirements. I certify that this Aircraft has been inspected m accord th A Pert,nen'.?!:eu~der the above work orde~nce WI an nnual inspection and IS determined to be ,n an auworthy cond1bon Signed~-------- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C -- Airframe ~ N39NG Hobbs Time: 624.5 Model: PA~-600TP 1<CAc. Total Time: 624.5 SIN: 4698039 Landings: Date: 06 June 2023 K- OCVA~ Cantxw- Work Order: S-23.0035-1 Removed Aspen EDB PN 910-00001-501 SN 243S. Installed Repaired Aspen EDB pin 910-00001-501 sin 971464-4 Part was repaired by Aspen Avionics Installed Repaired unit IAW PA-46-600TP AMM 34-24-00 Accomplished all required operational and functional checks with satisfactory results The Aircraft 1dent1fied above was repaired and Inspected in accordance with current Regulations of the Federal Av1at1on Adm1n1strat1on and 1s approved for return to seMce Pertinent details are on file under the above work order Signed ,t..,. ,. [' t!) ~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Airframe N39NG Model: PA~-600TP SIN: 4698039 Date: 12 July 2023 Hobbs Time: 631.4 Total Time: 631.4 Landings: 645 Work Order: S-23-00454 Removed A/C compressor PIN 557-802 SIN 0134311980, and installed new compressor PIN 557-802 S/N 1611205280, and serviced A/C system per Piper AMM (767-617) Ch 21-50-00 Accomplished all required operational and functional checks with satisfactory results The Aircraft identified above was repaired and inspected m accordance with current Regulations of the Federal Aviation Administration and 1s approved fo retur Pertinent details are on file under the above work order Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Airframe ef N39NG Hoba,. Time; &75.3 Moct.l: PA-46-600TP l<4 C. Total Time: 175.3 SIN: 4698039 landings: 689 Date: 14 November 2023 ~°"YA~o.r-- Wort( Order: S-23-00781 Removed GTC#2 PIN 011-01924-10, SIN 1M8506771 and mstalled OVERHAULED unit PIN 011-01924-10, SIN 1M8506595 per Piper AMM 767-617 Ch ~-25-01 Unit OVERHAULED by Garmin International, FAA CRS #G6XR582Y on their WO #16418742 AccompJ1shed all required operational and functional checks with satisfactory results The Aircraft identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and 1s approved tor return ,!;!rvi~ Pertment details are on file under the above work order Signed .£ ■ e ( •di 1,-,. Olathe KS 66062 (913) 782-0530 FAA Repa" Si,obon #AMYR171C Total To .•:•;•;•;•;•;•··~·=•:•:•:•:•:::::•:::::: ·•·•·•·•·•·•·•·•·•·•·•·•·•·•· ..•... ·=·=·=·=·=·=·=·=·=•:•:•:•:•:•:•:•:•:•:•: Carry forward ::::::::::::::::::::::::::::::::::::::::,•••••••·•••••·•·•·•·•·•·•••·•·•·•·•·•·•· = = ! 12931 W 1s1•t STREET I OLATHE, KS 660821620·960•7720 I MEAOAIRCRAFT@GMAIL.COM KAN8A8 C ITV Airframe log entry (04-29-2024) N3 9NG PA46-600TP S/N: 4698039 HM and Aircraft Total Time: 699.3 hrs. Inspected aircraft per MAS PA46-600TP Meridian inspection guide. Performed ICA special inspections. Researched AO status through FAA biweekly 2024-08. Installed Unpaved field operations upgrade kit PN: 88705-701. Replaced Nose gear down spring PN: 487-399. Replaced all brake linings PN: 066-09100, PN: 066-09200 and shims PN: 068-04100. Replaced RH main gear tire PN: 18SF88-6 and rim 0-ring PN: M83461-1-261. Re-sealed RH main gear strut PN: 485-082 and 0-ring PN: MS28775-227. Re-torqued Upper actuator to engine mount attachment hardware. Re-torqued both Main actuator lower bolts and replaced safety wire. Replaced brake fluid reservoir cap 0-ring PN: MS28775-115. Re-sealed Hydraulic pump reservoir PN: 330385 25- GA, O-ring PN: MS28775-346 and seal PN: 600-0000-10. Flushed and serviced hydraulic powerpack. Performed landing gear retraction checks in normal and emergency operation. Operations are satisfactory. Performed Main ship battery capacity check passed@ 91.5%. C/W FAR 91.207(d) ELT inspection and test. Next battery replacement due: October 2028. Serviced AC system with 2.Slbs R134a refrigerant. Replaced Oil cooler deflector PN: 102611-002. Repaired Co-pilot recline mechanism. Repaired aft bench seat support bracket. Repaired mid seats Head rest internal frame. Replace·d Upper cabin door guide pin with new one PN: 84858-003. Resealed cuts in cabin door seal. De-ice boots treated. C/W Piper SL 1131 aileron sector lubrication. C/W Piper SL 1132 Fuel leak inspection, nothing abnormal noted. C/W Piper SL 1135 cable and pulley inspection, nothing abnormal noted. Piper SL 1183 Elevator bracket rivet inspection, nothing abnormal noted. C/W Piper SL 1286 Nose steering components inspection, nothing abnormal noted. C/W Piper SB 1369 elevator spar inspection, nothing abnormal noted. C/W Piper SB 1410A- Vertical Stabilizer Installation Improvement. Performed engine run-up and functional checks, operations are satisfactory. I certify that this aircraft has been inspected in accordance with an annual inspection and was found to be in airworthy condition. / ~ Randall Huelsman v! VZ,c_, ~ - IA 3021808 (04-29-2024) +-MEAD.. .. .. '"' . ,. 12931 W 151$1 STREET I OLATHE. KS 660621620-960-7720 I MEADAIRCRAFT@GMAIL • .COM KANSAS CITY Airframe log entry (05-08-2024) N39NG PA46-600TP S/N: 4698039 HM and Aircraft Total Time: 701.3 hrs. Troubleshooted and repaired LH pltot heat. Replaced relay PN: 584-442 J-D4N-300M. Corrected configuration Issue. Operational checked good. 1certify that the wor is aircraft has been completed in accordance with the aircraft maintenance manual. 1111111111 Randall Huelsman~~~f--.-£-,,;te..--,,.;__...,i!:::;;..._----------------- 'A 3021808 (0S-08-202 4) +MEADAUICIIIIAlllf' .... v,c ■ a.. tNC. 12931 W 151 st STREET I OLATHE, KS 660621620-960-7720 I KAN BAS C ITV Airframe log entry (06-04-2024) N39NG PA46-600TP S/N: 4698039 HM and Aircraft Total Time: 708.7 hrs. Replaced #3 fuel probe with new unit PN: 10891T07Y00 and left wing harness PN: 10891T07Y00. Operations are satisfactory. I certify that this propeller has been inspected in accorda with an annual inspection and was found to be in airworthy conditio~n~·----::~ Kevin Mead _____....t&,,e:;.2~~~~~----~------_~-4-L._:"' _______ IA 443641987 (06-04-2024) - Airframe ---4- • N39NG Hobbs Time: 710.5 Model: PA-46-600TP Total Time: 710.5 SIN: 4698039 - I<.CA.c. Landings: Date: 27 June 2024 ~c..v~,c.,._. Work Order: S-24-00418 Removed LH #2 wtng fuel probe PIN 481-501, SIN 33470 and installed NEW probe PIN 481-501, SIN OT~652U per Piper AMM 767-617 Ch 28-40-00 • Removed RH #3 wing fuel probe PIN 481-502, SIN DT5869O and installed NEW probe PIN 481-502, SIN OTCC199 per Piper AMM 767- 617, Ch 28-40-00 Performed fuel quantity 1nd1cat1on cahbratton per Piper AMM 767-617, Ch 28-40-00 Removed LH wing fuel probe wmng harness 46W24A018-001 and installed NEW fuel probe w1nng harness PIN 46W24A018-001 per Piper AMM 767-617, Ch 28-40-00 Accomplished all required operabonal and functional checks with satisfactory results The Aircraft 1denbfied above was repaired and Inspected in accordance wtth current Regulations of the Federal Av1at1on Adm1mstrat1on and 1s approv~~=-=nent detalls are on file under the above work order Signed Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Airframe N39NG Model: PA-46-600TP SIN: 4698039 Date: 14 August 2024 Hobbs Time: 721.8 Total Time: 721.8 Landings: 704 Work Order: S-24-00527 Removed UH #1 fuel quanbty probe PIN 481-500, SIN DT0483G and installed NEW probe PIN 481-500, SIN DTAJ931, removed R/H fuel quantity probe PIN 481-500, SIN OT0482G and installed NEW probe PIN 481-500 SIN DTAR741, and performed fuel quantity 1ndx:at1on calibration per Piper AMM 767-717 Ch 28-40-00 Removed mime fuel pump PIN 461-753 SIN 12BN45 and installed REPAIRED pump PIN 461-753, SIN 1BU5 per Piper AMM 767-617 Ch 28-20-00, pump repa1red by Parker Hannifin Corp. FAA CRS# H05R91 Mon their WIO# 51652, performed fuel system functional test per Piper AMM 767-617 Ch 28-00-00 Accomphshed all required operational and functional checks with satisfactory results The Aircraft Identified above was repaired and inspected in ac:cordance with current Regulations of the Federal Av1at1on Admin1strabon and Is approved for return to service ~:nent details are on file under the above work order Signed ~.,.,..... (' {r/ A.-____ Olathe KS 66062 (913) 782-0530 FAA Reoair Station #AMYR17H~ l ♦ I • • Transport Canada Transports Canada TC-1001185 1 ■ 11111111111111 05/2005 Engine Logbook TP 14182 (Revised 05/2005} Canada J Volume #: _ :J _____ _ Opened on: 1 8 FEB 2017 ENGINE DETAILS 1. Manufacturer ___ Pratt & Whitney Canada Corp. 2. Type/Model/Series_ E.T.C. E- :1-~ PT6A- f-~/1 8/S: LJ /:fl 3. Serial Number __ _ PCE- Rl'1 0 735 THIS ENGINE SERVICED WITH bp TURBO 2380 OIL AT THE PIPER FACTORY CYCLE COUNT AS OF HAY ! 3 20t7 ------=------- NUMBER OF CYCLES __ .J..7 ______ _ (i) ~ f. d f gine maintenance and elementary work Section 1: Recor o en Date Time since Time since Total cycles overhaul Details of task --/--/-- new 18 FEB 2017 0.0 NI/I 0 New engine final accepta ~ f inhibiting run compl t nce_fest ••d --- ~ d • • e ed satis,: - - an 1s 1n condition for s acto,.il - af e opera ti Y on. ~ (j 2 7~Pn 1.oll o.o NIA: ~ "Applied Procyon corrosion Inhibitor to - ~ compressor Inlet case Ptr Pratt & ~ --- Whitney Maintenance Manual PIN ~ 3021442 Chapter 12-00-00." I -- ~ ~ I ~ - Date· 5 - I I- I7 - Arcrlft SIN: qG 980 3 <-) Reg. Number: N3 9tJ G ---.... - -- - Ai'craft Engiie Model: PTIA-12A SIN: ece-R,(!)0735' - - TTE: ~ •" 'i Cycles: - Performed Engine w_, Wah per Pr.a & Whitney Maintenance j ' - Manual Part Number 3021442, c,..., Section 71.()()..()(), Power Plant a.....,,EnglfteW~::;r- - Signaue: a~ '""' - Name: B1111rtaantc A&P Certificate Number: AP113I007f0 - P1/e,-· PIPER AIRCRAFT, INC. -- ~ . - ·-~ - - - - Date:'5"°-\ &-\J - - Aircraft S/NH (;9 803~ Reg. Number: N39 NG - Aircraft Engiie Model: PTlkfZA SIN: PCE-Rf!\Ql3S - - TTE: 3. s Cyclea: s: P.rfonned Engine w_, Wah per Pren & Whitney Maineenanr.e - Manual Part Number 3021442, Chapw/ Section 71.()().00, Powe, Plant - =-~(7~1W~ - - \ Name: Ru11Wpw A&P Certlfecate Number. AP1131007fO '/ -- Pl,/,ir· PIPER AIRCRAFT, INC. - - ..__ AME ACA/AMO • SCA/AMO _, ___N_G_/...,.0-.. ~3~'.S-=-J~O-D-l~l~PM~,-at-~i-~5-0_S_H_P'-!/6~✓~0------+------+----~ Signature ITT Trim:_......3.....?t__\_.....5__C0 TS Trim Resistance: +'if', 7 Ohms 16- Engine ------4- N39NG Hobbs Time: 35.8 Model: PT6A..-2A I C. Total Time: 35.8 SIN: PCE-RM0735 Cycles: Date: 1 February 2018 K- City AvietlOn Cente<- Work Order: S-18-00033 Complied with 12 month/ 150 hour compressor performance recovery wash and turbine wash per P&\/1/C PT6A-42A EMM 71-00-00. Re-applied engine inlet case CPC per P&WC PT6A-42A EMM 71-00-00. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. The Engine identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is approved~ce. Pertinent details are on file under the above work order. Signed ~2 Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Engine ~N39NG Hobbs Time: 72.2 Model: PT6A-42A I<c C. Tach nme: 72.2 SIN: PCE-RM0735 Total nme: 63 Date: 06 April 2018 ~ City Avle<:lon c.ntar Work Order: S-18-00030 Complied with 1"1 50hr inspection in accordance with Piper Aircraft Warrantable 1•1 50hr Inspection Report PN 765-044. Performed compressor and turbine desalination wash and re-application of CPC in air inlet case after wash, in accordance with P&\/1/C PT6A-42 EMM 71-00-00. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. The Engine identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is approved f retu t s ice. Pertinent details are on file under the above work order. Signed ~~~ftl.../-~----- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Engine N39NG Model: PT6A-42A SIN: PCE-RM0735 Date: 26 June 2018 Hobbs Time: 114.3 Total Time: 110 Cycles: 110 Work Order: S-18-00036 Complied with an Annual Inspection using Piper AMM 767-617, Chapter 5-20-00 Event #1 and #2 forms as a guide to comply with the inspecilon requirements of FAR 43 Appendix D. Took engine oil and filter patch samples and sent them out for analysis. Performed engine compressor performance recovery and turbine wash per P&WC PT6A-42A EMM 71-00-00. Complied with 600 hour/ 12 month inspection of the of the reduction gearbox chip detector per P&\/1/C PT6A-42A EMM 72-00-00. Complied with 100 hour static operation check of the FCU MOR lever per P&WC PT6A-42A EMM 71-00-00. Complied with 12 month engine mount inspection in accordance with P&WC PT6A-42A EMM 71-20-00 and Piper AMM 767-617 Ch. 05- ~« ' Complied with air inlet case CPC application after compressor wash In accordance with P&\/1/C PT6A-42A EMM 71-00-00. Installed 2 new igniter plugs P/N CH34055 per Piper AMM 767-617, Ch 74-20-00. Adjusted engine Ng in accordance with Piper AMM 767-671, Ch. 76-10-00. Re-torqued lower torque transducer oll line, ref. Piper AMM 767-617, Ch. 71-00-00. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. I certify that this Engine ha been inspected in accordance with an Annual inspection and Is determined to be in an airworthy condition. Pertinent de ii are fil n er the above work order. Signed H~~.q,.lbq..,~..\----- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Page 1 Section 1 Oat - - I - - Engine -----✓-------- Model: SIN: N39NG PT6A-42A PCE-RM073517 July 2019 1 Hobbs Time: 287 8 Total Time: 287 :8 1< ... _ Cttv A,,._,.,,, c.~ • Cycles: 280 . . . Work Order· s 1 Compiled with an Annual lnspP.ct,on using Piper PA•48-600TP AMM 767-611 ch 05 . 20 _ 00 • • 9-00178 the inspection requirements or FAR 43 appendix D. event 1 & 2 checklisls 89 a ulde Complied with 100hr manual override static test per Piper AMM 767-617 ch 71-00-00 g to comply With Complied with 600hr 112 month RGB chip detector Inspection per P&WC PT6A-42A EMM 72 Complied with 150hr 112 month compressor and turbine wash per P&WC SIL PT6A. 206 R 2 -oo.oo. Inlet CPC. a nd PTeA-42A EMM 71-00-00 Re . Complied with 400hr borescope of the hot section components per P&WC PT6A-42A EMM 7 • -applied Complied with 400 hour fuel nozzles and manifold now check, replaced fuel nozzles With In 2 -oo.oo. Rocky Mountain Turbine Services CRS# 1 B6R708C on work order# R003465. Work perfor:ected and functionally tested nozzles Took engine oil and filter patch samples and sent out for analysis, results normal. ed per P&WC PT6A-42A EMM 73_ 11 .~ Installed 2 new ignlters PIN CH34055B per Piper AMM 767-617 ch 74-20-00. • Date: Compiled with 500 hour inspection of the accessory gearbox Internal scavenge screen per P&WC Accomplished all required operational and functional checks with satisfactory results. Ground rf PT 5 A-42A EMM 72-60-00. pe ormance run QOOd, no leaks noted. 1 certify that this Engine has been Inspected In accordance with an Annual Inspection and is deter I d Pertinent details ~re on file under the above work order. m ne to be In an airworthy COnditlon. Signed -.A~ Olathe KS 66062 (913) 782-0530 FM R ~ epair Station #AMYRHtC I I • 1 Engine N39NG Model: PT6A..-2A J Hobbs Time: 274.0 SIN: PCE-RM0735 Total Time: 274.0 Date: 10 Aprll 2019 ~ Ct11V•-. a.-· Cycles: . Work Order: S-19-00117 Performed engine compressor performance recovery and turbine wash per P&WC PT6A-42A EMM 71 0 required. • 0-00 and re-applied inlet CPC as Accomplished all required operational and functional checks with satisfactory results. Ground pert ormance run gOOd, no teaks noted. :n,e Engine identified above was repaired and inspected in accordance with current Regulations r th . . . . is approved for return to service. Pertinent details are on file under the above work order. 0 e Federal Aviation Admrn,stration and Signed ~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR 171 c ,-- J J Engine N39NGModel: PT6A-42ASIN: PCE-RM07!5 Date: 1 November 2019 Hobbs Time: 337.7Total Time: 337.7 Cycln: 328 Work Order: S-19-00348 -,~ --.J Performed unscheduled inspection for Propeller Electrical Leads Shorting and Lightning Strike per P&WC PT6A-42A AMM 72-00-00 page 651. No defects noted. Reinspect RGB chip detector, RGB oil screen, and main oil filter in the next 25 to 65 hours of operation. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. The Engine identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is approved for return to service. Pertinent details are on file under the above work order. Signed ~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Engine N39NG Model: PT6A-42A SIN: PCE-RM0735Date: 3 February 2020 Hobbs Time: 355.3 Total Time: 355.3 Cycln: 346 Work Order: S-19-00420 Complied with an Annual inspection using Piper PA-46-600TP AMM 767-617 ch 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. Complied with 200hr manual override static test per PT6A-42A EMM 71-00-00. Compl~ w~ 600hr / 12 month reduction and accessory gearbox chip detector inspection per P&WC PT6A..-2A EMM 72-~00. Complied with 150hr / 12 month compressor performance recovery and turbine wash per P&WC Sil PT6A-206R2 and PT6A__.2A EMM 71- 00-00. Re-applied inlet CPC. Performed follow up to lead shorted 0< lightning strike inspection of main oil filter RGB chip detector, and RGB oil screen per P&WC PT&- 42A EMM 70-00-00. ' Complied_ with _400hr bore&e0pe of the hot section components per P&WC PT6A-42A EMM 72-00-00. Took engine 0tl_and filter patch aamples and sent out for analysis. Removed both igmters and replaced with new PIN CH34055 per Piper AMM PIN 767-617 Ch. 74-20-00. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. 1 ~ th at th is Engine has been inspected in accordance with an Annual Inspection and 11 determined to be In an ailWOrthY conditiOn, Pertinent details are on file under the above work order. Signed C&J t"'2,_~--- Olathe KS 66062 (913) 782-01530 FM Repair StatiOn IAMYR171C ◄ AME Signature ACA/AMO ,.. SCA/AMO ---------+------+-----! > L,.411119 tht 111sl11n1 of Avtatto11 Model Serial No. Registration Engine Model PA-46-600TP 4698039 NJ9NG PT6A-42A En inc Serial PCE-RM0735 Scheduled Maintenance or Inspections 21Ul2 Old Towrr Rnwcl rhornll Arbona "~OJ4 FAA Rr11wlr Station No, EKC;R~7ll1 Engine Log Work Order No. I lour Meter Airernfl Total Time Engine TSN En •inc CSN 602-267-4070 Phont 602--267-4030 FAX 0lM-12416 458.8 458.8 458.8 465 • Complied with Minor Engine Inspection on Model PT6A-42A. Reference PWC PT6A-42A EMM 72-00-00 Table 60 I. • Complil.'d with 12 month compressor desalinization wash. Reference PWC PT6A-42/\ F-:MM 71-00-00. • Complied with 500 hour inspection and cleaning of engine oil scavenge screen in reduction gearbox. Reference to PWC PT6A-42A EMM 72-00-00 Table 60 I. Airworthiness Dirccti\·cs or Service Bulletins • AD's reviewed through Biweekly 2021-05. The aircraft a nd /or compo~ent i~entified above was repaired and inspected in accordance with current federal aviation regulations and is approved for return to service with respect to the work performed. Pertinent details are on file at this repair station. ~ ~ Signed: Engine N39NG Model: PT6A-42A SIN: PCE-RM0735 Date: 13 January 2022 FAA Rr air Station No. EKGR5710 Kevin Reedy Date: MAR 18, 2021 Hobbs Time: 524.9 Total Time: 524.9 Cycles: 535 Work Order: S-21-00442 Complied with an Annual inspection using Piper PA46-600TP AMM 767-617 Ch. 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. Complied with 100 hour engine minor periodic inspections using P&WC PT6A-42A EMM 72-00-00, table 601. Performed engine compressor performance recovery and turbine wash per P&WC PT6A-42A EMM 71-00-00. Complied with 600 hour/ 12 month inspection of the of the reduction gearbox chip detectors per P&WC PT6A-42A EMM 72-00-00. Complied with 200 hour static operation check of the FCU MOR lever per P&WC PT6A-42A EMM 71-00-00. Complied with 600 hour inspection of the fuel inlet screen per P&WC PT6A-42A EMM 73-10-02. Complied with 600 hour replacement of the fuel outlet filter per P&WC PT6A-42A EMM 73-10-02. Took engine oil and filter patch samples and sent them out for analysis. Complied with Piper VSP 269 - P&WC SB 3501R1 by removing oil-to-fuel heater P/N 10585K S/N WA55037 and replacing with overhauled P/N 10994A SIN WA23848 per P&WC PT6A-42A MM 73-10-01. Unit overhauled by Meggitt (Troy), Inc. Cert No. S1WR141 N under W/O# 4504140479. Removed 2 ea. igniters and installed new igniters PIN CH34055 per P&WC PT6A-42A EMM 74-20-00. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. I certify that this Engine has been inspected in accordance with an Annual inspection and is determined to be in an airworthy condition. Pertinent~ a!/ ff er the above work order. Signed 114)_ ~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Engine N39NG Model: PT6A ◄ 2A SIN: PCE-RM0735Date: 10 January 2023 Hobbs Time: 597.9 Total Time: 597.9Cycles: 608 Work Order: S-22-00681 Complied with an Annual inspection using Piper PA46-600TP AMM 767-617 Ch. 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. Performed engine compressor performance recovery and turbine wash per P&WC PT6A-42A EMM 71-00-00. Complied with 100 hour static operation check of the FCU MOR lever per P&WC PT6A-42A EMM 71-00-00. Complied with 600 hr/ 12 month RGB chip detctor per Piper AMM 767-617 Ch. 5-20-00. Minor nick noted on first stage compressor blade during inspection has been evaluated and determined to be within acceptable limits without repair per P&WC PT6A-42A EMM 72-30-05. First stage compressor re-inspection due at 697.9 hrs. TT. Accomplished all required operational and functional checks with satisfactory results. Ground performance run good, no leaks noted. I certify that this Engine has been inspected in accordance with an Annual inspection and is determined to be in an airworthy condition. Pertinent details re on ,1 u the above work order. Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Page 2 Section 1: Record of engine maintenance and elementary work Date Time since Time since Total cycles Details of task --/--/-- new overhaul ~ l +~.~-~R 12931 W 1515 1 STREET I OLATHE, KS 66062 I 620-960-7720 I MEADAIRCRAFT@GMAIL.COM --........_ KANBAB CITY \ ------------------------------------,---- Engine log entry (04-29-2024) N39NG PT6A-42A S/N: PCE-RM0735 HM and Engine total time: 699.3 hrs ---- Inspected engine per MAS Meridian inspection guide. Checked both igniters, oil filter, and P3 filter. Cleaned and inspected fuel -..... inlet and outlet filters. Performed borescope inspection of first stage compressor, no defects noted. Performed 400 Hour Fuel -- nozzle flow check. Replaced #2 & #6 nozzles PN: 3019424, O-rings PN: AS3209-009, gaskets PN: MS9371-16. Performed 400 hour Hot Section Borescope (with nozzles removed). Found cracks beyond limits in combustion liner. Removed and re-installed - Engine Hot section components repaired by Standard Aero, Combustion Liner Outer PN: 3056143-01, SN: RWA17F109, WO: - RPR63517, PT Stator PN: 3076352CL05, SN: HLAB012, WO: RPR63517. Combustion Liner Inner PN: 3114842, SN: RWA14F728, - WO: RPR63517. Replaced accessory drive belts PN: 73965-024, PN: 73965-023. Performed engine compressor and CT wash. Performed engine exterior wash and lubrication. Completed engine run-up and operational creeks. Operations are satisfactory. I I certify that this e~gi s insi~ecte~m accor with an annual inspection and was found to be in an airworthy condition. I Randall Huelsman /. 7A IA 3021808 (04-29-2024) - v~ Engine -----4- I .. N39NG Hobbs Time: 760.9 Model: PT6A ◄ 2A I<c C. Total Time: 760.9 SIN: PCE-RM0735 Cycles:Date: 18 November 2024 ~ City Aviftelon Centor Work Order: S-24-00839 ,f t ~ Complied with 400-hour borescope inspection of engine hot section components in accordance with P&WC PT6A-42A EMM 3021442 chapter 72-00-00. • Accomplished all required operational and functional checks with satisfactory results. Ground performance run good. no leaks noted. . The Engine identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and 1s.approv1or retu~ ser. Pertinent details are on file under the above work order. Signed , - - ( c) Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C - - - ~ - ~ -- - 1 ~ HARTZELL PROPELLER LOGBOOK PROPELLER MODEL 5D3-N338A I PROPELLER S/N ______..S....._F_i+-=3::;..__ __ _ LOGBOOK# l rt»iWiNJ.@i#iPSMiiWA:Gi I 'IWri,,;4; I• Propeller NC Description of all operations pertaining to_ Airworthiness Directives, Date TSN TSO Hrs Service Documents, Overhaul, Major or Minor Repair, and Inspections. . f?rr@(?)®OO@rr lb@@ Date: 0 -I 1-f 7 Hobbs Time: ~ .tj I Aircraft SIN: ':f Ci9 &0 3~ Reg. Number: ~'3.2~G I PropMOdet:SD3-N33caa I SIN: ~f~3 I CL~~~~~~la~al I ~:ng v.ithl~=~; ~f aPJr~~=a:i:~~~~ng Flight I Signature: CT ~~ ~ II Name: Russwaaoec A&P Certificate Number: APjl3§0QZ6Q I P/,.r· - PIPER AIRCRAFT, INC. I - ~ - I • • --- --- ---- • • • Propeller 1<&.N39NG Hobbs Time: Model: 5D3-N338A1 Tach Time: SIN: SF43 Total Time:Date: 06 April 2018 ic.-c,,,,--.c.,,_. Work Order: Complied with 1 11 50hr inspection in accordance with Piper Aircraft Warrantable 1 11 50hr Inspection Report PN 765-044. Accomplished all required operational and functional checks with satisfactory results. 72.2 72.2 63 S-18--00030 The Propeller identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and is appr~v'Jff' r771J1ervice. Pertinent details are on file under the above work order. __ Signed ~ / Olath~ KS 66062 ~ 3) 762-0530 FAA Repair Station #AMYR 171 C Propeller 1<~c. N39NG Hobbs Time: 114.3 Model: 603-N338A1 Total Time: 110SIN: SF43D1w: 26 June 2018 ic-o...,-ow- Work Order: S-18-00036 Complied with an Annual Inspection usmg Piper AMM 767-817, Chapter 5-20-00 Event #1 and #2 forms as a guide to comply with theinspecbOn requ1remen11 of FAR 43 Appendix D. Complied with 12 month/ 400hr detailed propeller ln1pection in accordance with Hartzell Owner's Manual No. 486. Ch. 61-00-86. Complied with 60hr in1pect1on of the prop heat 1ystem per Piper 767-617 AMM 30-60-00. Complied with 12 month/ 400hr propeller lubncatton In accordance with Piper AMM 767-617, CH. 12-20-00. Accompl11hed all reqwed operattonal and functional check1 with 1att1factory r11ultI. I certify that thi1 Proper/lier~ ha1 been in1pected in accordance with en Annual inapectton and 11 determined to be In an airworthy condition. Pertinent d:, lire on leJfder the above work order. Signed _,U),M~U.,NfA~---- Olathe KS 86062 (913) 782-0530 FAA Repair Statton #AMVR171C I -v('"' ••• i - - - - - Page1 { - Datf Propeller N39NG Model: 5D3-N338A 1 SIN: SF43 Date: 17 July 2019 Hobbs Time: 287 .8 Total Time: 287 .8 Work Order: S-19-00178 Complied with an Annual Inspection using Piper PA-46-600TP AMM 767-617 ch 05-20-00 event 1 & 2 checklists as a guide 10 comply with the inspection requirements of FAR ◄ 3 appendix D. Complied with so prop heater Inspection per Piper AMM 767-617 ch 30-60-00. Complied with ◄ O0hr 112 month propeller lubrication per Piper AMM 767-617 ch 12-20-00. Complied with ◄ O0hr 112 month detailed Inspection per Hartzell manual 486 check 11st. Installed new beta block PIN A3026 per Piper AMM 767-617 ch 61-10-00. Applied sealer 0511 ◄ 1-5798 ◄ to de-Ice boots as required. Accomplished all required operational and functional checks with satisfactory results. I certify that this Propeller has been Inspected In accordance with an Annual inspection ond Is determined to be in an airworthy condition Pertinent details are on file under the above work order. • Olathe KS 66062 (913) 782-0530 Signed~) 1 - 1 I 1· FAA Repair Station #AMYR171C Propeller N39NG Model: 503-N338A1 SIN: SF43 Date: 7 October 2019 ~ l<4 C-Aviation- Hobbs Time: 337.7 Total Time: 337.7 Cycles: 328 Work Order: S-19-00348 Removed propeller assembly for repair. - Signed (,4.--- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C ------- • • • •I I I • . ,,· .. •. . ..· ;., ·;( ,: \1. ::·-.:t ·; :- '.·,;_""",,,,,,.,,., •.,. •£'Jtnfe~~~E.t.4f~·~ET ~RVl~E ~@- Prop Model Component Serial No. T.S.O. T.S.N. 503-N338A1 Propeller SF43 N/A 337.7 - Blade No. 1 B520S N/A 337.7 Blade Model Blade No. 2 B5207 N/A 337.7 78D01B Blade No. 3 B5200 N/A 337.7 Date: 10/30/2019 Blade No. 4 B5206 N/A 337.7 Blade No. 5 B5112 N/A 337.7 Disassembled propeller. #1 blade SIN 85205 was repaired by Hartzell Service Center (WO 16348). Painted remaining blades. Reassembled propeller using new seals and statically balanced 1/AJIN Hartzell Maintenance Manuals 496 rev. 2, 127 rev.13, 135F rev. 33, 159 rev. 68, 180 rev. 29, and 202A Vol. 1 rev57, Vol. 3 rev38, Vol. 6 rev35, Vol. 7 rev48, Vol. 8 rev33, and Vol. 11 rev36. Work performed in accordance with current Regulations of the Federal Aviation Administration and is approved for return to service. Details of repairs are on file with this Repair Station under W/O PROPa 3~ Signed /L,b= ~J'krv/,for INTERCONTINENTAL JET SERVICE CORP FAA Repair S ti6n # IZ2R916K Hangar 27-Tulsa, Oklahoma I I I s. Page2 I I Date Propeller N39NG Model: 5D3-N338A1 SIN: SF43 Date: 1 November 2019 Hobbs Time: 337 .7 Total Time: 337.7 Cycles; 328 Work Order: S-19-00348 Installed repaired propeller on Piper PA-46-600TP SIN 4698039 per Hartzell Owner's Manual No. 486 and piper PA-46~00TP AMM 767- 617 Ch. 61-10-00. Propeller was repaired by lntrcontenental Jet Service CRS# IZ2R916K under WO# PROP-1307. Dynamically balanced Hartzell Propeller Installed dynamic balance weight of 14.5g@ hol~ 8 and 26.6g ~ hole 9 c-,1 !'-FT spinn~r bulkhead tor total weight of 41.1g for final dynamic balance of .04 IPS@ 11 degrees, ground operation. Accomplished dy•;am,c balance in reference to Hartzell Owner's Manual No. 486. Accomplished all required operational and functional checks with satisfactory results. The Propeller identified above was repaired and Inspected In accordance with current Regulations of the Federal Aviation Administration and is a:::ed for return to service. Pertinent details are on file under the above work order. Signed~~ Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C I I I Propeller ~ N39NG Hobbs Time: 355.3 Model: 5D3-N338A1 l<4 C. Total Time: 355.3 SIN: SF43 Date: 3 February 2020 ~CloyA\llaClonc.,_, Work Order: S-19-00420 Cof'!lplied ~h an ~nual inspection using Piper PA-46-600TP AMM 767-617 ch 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. Complied with 50 prop heater inspection per Piper AMM 767-617 ch 30-60-00. Complied ~th 400hr / 12 month propeller lubrication per Piper AMM 767-617 ch 12-20-00. Complied with 400hr / 12 month detailed inspection per Hartzell manual 486 check list. Accomplished all required operational and functional checks with satisfactory results. I ce,:tify that th!s Propeller has been inspected in accordance with an Annual inspection and is determined to be in an airworthy condition. Pertinent details are on file under the above work order. Signed <: ...t:..--- Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C • • • • ~~11.J!!t? 2802 Old Tower Road 602-267....070 P1toee PhoeniK Arizona 150:W FAA Rtpair S1a1ion No. EKGR571 D 602-26740.)0 FA.'< Model PA-46-600TP Work Order No. 02M-12416 Serial No. 4698039 Hour Mc:ter 458.5 Registration N39NG Propeller log Aircraft Total Time 458.8 Propeller Model 5D3-N338AI PropdkrTSN 458.8 Prooeller Serial SF43 ProodkrCSN 465 ~lwlllwl MliDltDIDs:t SIC IDtlW:lillDI • C/W 12 month/400 hour lubrication. Reference Hanzel! Propeller Owner's Manual 61-00-47 . • C/W I2 monlh/400 hour periodic inspeclion of aircraft propeller. Reference Hanzel! Manual 147 . • C/W SO hour inspection check of propeller healer. Operational test good. Reference Piper PA-46-600TP MM 30-60-00 . PiKctRIPfia • Removed propeller for repairs. Reference Piper PA-46-600TP MM 61-10-00. See FAA Fonn 8130-3 from Ottosen Propdler and accc:i.sories. Inc. Dilled J 6/MAR/2021 for repairs. Reinstalled re1>aired propeller. Reti:rence Piper PA-46-600TP MM 61- I 0-00. Opet111ional checked sood . .&im:1rJbi11D1 11.ic.a:lit:a II[ Ho:i,t llulltliDI • Al>'• reviewed throusb U1weekly 2021-0S . The aircrlft and /o, component Identified lbovt w11 repllrtd and lnaptctld In accordance with cunent fed•II avlltioll rtgulalion1 and 11 approved tor rtturn to HMCt wiltl rtlplCI to tht wOftl pe,formed. Plltlnent dttlill 1r1 on flit It thl1 repair llltlon, Signed: .,r:: . ~ 11,U Kru1lr 8t1tioa No. t:l\(;115711> Ke,•/,, Rttt"1' Date: MAR 18, 2021 Page3 I I Date I I I I - Propeller A/C Description of all operations pertaining to Airworthiness Directives, TSN TSO Hrs Service Documents, Overhaul, Major or Minor Repair, and Inspections. • I. Arr,.n l,tJ C"h fl,\, IMH'n r AUTIIOIUZF,I) HELEASE CERTIFICATE J.,....,Tr,c•hlt- A1Nhorh) ll't,..,n,a 03162102 ~·AA'IJNITEI> STATES l'AA rmm ~130-3, AIRWORllllNE!l!I APPROVAL TAO ono.o;EN rRorr:LLER-c\ACTESSORIF.S~ INC. - .. . ... , Wmo.dff/C-~ol<•N•~- ~ 0n.,1,.,1or, N- ...i A.Urn,· CRS ZR2RJJJLI0J South 2Rrh ~'"~ • l'lk>tnl,, Arl1<Wla RJOU 111219 ~--7'-;;..:.~ ... ~... i. -~.;;-;.~~- - I" ... ;;;;.;- ·- II. . ·-·-- !11.r-,/Wort! -~ ~ ~RTttUrR~ELLER .• ~oj~~m~~ • ---- I : SFO --- RE,AIREO - -- U. ltnn""'" IIARTZELL PRO1'£1.LER MODEL: 5D3,Nl38A I SERIAL: Sl'"3 OLAl>E MOOEL: 780018 01.AOE SERIAL: I.OS20S 2.8$207 3.85200 ... 05206 S.0$112 OISASSEMBLE PROPELLER, REMOVE DEICER OOOT AND I.F.ADINO EIXJE OF #4 bl.Al>f.. INSTALL NEW LEAOfNO EOOF., FILL ANO 'AIN'T 131.ADE, INSTALL NEW l>F.ICER BOOT. OALANCF. 01.ADl:S, ASSEMBLE PROPELl.1:R, Sl'.T BLADE ANOLES, ANO BALANCF. PROPELLER: IN AC'C'ORDANCE WITII HARTZELL MANUAL "96 RF.V 3, r,9 REV 7... AND IIO REV 3'. ~ -~roe1 .... ,11 • ..,,,.,,,,,11,.;... - 14L 0 l'CFIUJ9Rttoono1es...1« 0°"'"'........,,.,,_.;11,,1;,._,1..., hi I cmdilklft r« ,.r, ~ ' . Cfflillft ,,,_ ...... .....,.,.. s,fflfd ir, _. 12, rlw - Wrwlif',c,d ill - II ~ ...., ,o llkd ll ,.., """"""isllH lo~""" Ttdc I~. Cock o( .,...ill<d hi 11 •I~•-• pon 4J lrl4 in ,..p<d,. ... •..t. lht - - _... ro, Mnitf. I lb. ''"""''""" S.,-: • .............__ I.le. ~..,-,..,,, No.: ti,· A~'ffll Si...-, I Uc. ,.,,..,....c'Cllif"lall< l'lo.: > '\,._ =::::::::::: • CKS ZR2RJSSL ~«Prirlw1: lk Dolr~))')'I: , ...... .__ ,rV«rr-,: He. Dole «.W->nY>: 00/00'00 ROY HENDERSON 16/MAR/2021 -- ~ - --- Usernnscaner Rnponsibililin - ~ i. ....,... .................. Gillctlctof .. 1.- ..... .,.. IIOl _iclll)'_M__,.IO ........... ;;;.....,.,,,..,,..,onidl . .,,._.,._,,......,.l'fflfflllS,.'Oll:ill-•Wlrlw•icNl ....... i<Mllof•_,........,~.iliW- __ ........,,_...,_.,._,,.__,.lfCdlWil'll!loct I. cis«k11ria!Nrr1w.,..,IUlall<r..,....,,.~is""..,..........,........., • ....,.......,..,....o-,.,,.,,1a1,rlllido111...,,..,..,.ontoillnt__,..,.,_,.,,.._.,_ ,_ -,.,81.x\a l)a ... l,lo.,.,,t_,.ilw......,,,ccnilicaiorl. .... _._ ...... ~ ....... - ....... ......._~.,_,il_...,•~lk ...,;.....i ,.,.,..k"1 II, ...... , ........ bdar, .. ai,<nft Ml)' II, n... ■ FM tMII SIJO.J 102-1~1 l>'SN: 00,~-4CM!ll-900$ .. . - -- - ... ----- -- - - • •Propeller N39NG Model: 503-N338A1 SIN: SF-'3 Hobbs Time: s2,.9 Total Time: 524.9 Work Order: S-21-0042 Date: 13 January 2022 Complied with an Annual inspection using Piper PA46-600TP AMM 767-617 Ch. 05-20-00 event 1 & 2 checklists as a guide to comply with the inspection requirements of FAR 43 appendix D. Complied with 400 hour/ 6 month propeller lubrication per Piper AMM 767-617 Ch. 12-20-00. Complied with 50 hr propeller heat inspection per Piper AMM 767-617, Ch. 30-60-00. Complied with 600 hour/ 12 month tap test of the erosion surfaces per Hartzell Owner's Manual No. 170, Ch. 61-13-70. Complied with 400hr/ 12 month detailed inspection of propelle~ per Hartzell Owner's Manual No. 486. 61-00-86. Accomplished all required operational and functional checks with satisfactory results. 1 certify that this Propeller has been Inspected in accordance with an Annual inspection and is determined to be in an airworthy condition. Pertinent o/!:-iJ./re on/)e/n;t3r the above work order. Signed .,.U/4c.ac..~-J-~..u.JL_~1/t.._ \...____ Olathe KS 66062 (913) 782-0530 FAA Repair Station tAMYR171C Model: SIN: Date: Propeller N3tNG 603-N338A1 8F43 10 January 2023 1<~c--. Hobba Time: Total Time: CyclM:WorkOrder: 597.t 597.t 808 S-22-00681 Complied with an Annual in1pectlon u1ing Piper PA46-600TP AMM 767-617 Ch. 05-20-00 event 1 & 2 checkliata as a guide to comply with the inlpection requiremenll of FAR '43 appendix o. Complied with 400hr/ 12 month detailed in1pectlon of propeller per Hartzell Owner'• Manual No. 486. 61-00-88. Com_plied with 400 hour/ 12 month propeller lubrication per Piper AMM 767-617 Ch. 12-20-00. Lubncated Propeller per Hartzell Propeller Owner'1 Manual 61-00-88, Reduce lubrlcatlon interval in accordance to Propeller Owner's Manual 81-00-86, to every 100 houri until grean leak i11ue l1 reaolved. Applied edge aealer to propeller de-Ice booll H required per Hartzell Propeller Ice Protection Manual No. 180. Replaced propeller de-ice wiring ty-rap1 with correct part number TY624MX per Hartzell aervice bulletin HC-SB-3~375. Accomplilhed all required operational and functional check• with 11t11flctory reaultl. I certify that thl1 Propeller ha1 been lnapected In accordance with an Annual lnapection and 11 determined to be In an airworthy condition. Pertin~re on J)nr the above work order. • Sigr::.(/ff) _ __.-" ■ .1-4"6M. 4 v-::-~i::;.._-======- Olathe KS 66082 (813) 782-0530 FM Repair Station tAMYR171C Page4 Propeller A/C Description of all operations pertaining to Airworthiness Directives, Date TSN TSO Hrs Service Documents, Overhaul, Major or Minor Repair, and Inspections. . 1+MEAD a1•c .. A•'r ■ e .. ,r1c••• ll'IIIC 12931 W 151 st STREET I OLATHE, KS 66062 1620-960-7720 I KAN8A ■ CITV Propeller log entry (04-29-2024) N39NG 5D3-N338A 1 S/N: SF43 HM and Prop TT: 699.3 Inspected Propeller per MAS Meridian inspection guide. Lubricated hub and dressed blades. Performed 600 hours Hartzell composite blade erosion shield Inspection, nothing abnormal --- ~ - --- noted. Repaired Inboard prop heat boots. Performed engine run-up and operational tests .. Operations are satisfactory. I certify that this propeller was inspected in accordance with an annual inspection and was found to be in an•~~~ Randall Huelsman ~ IA 3021808 (04-29-2024) - -- -- - - • • •Propeller 4- N39NG 1<e:A.c. Hobbs Time: 738.8 Model: 5D3-N338A1 Total Time: 738.8 SIN: SF43 Date: 08 October 2024 I<- C"'V"'-an 0-W Work Order: S-24-00718 Performed a minor repair to the trailing edge at the tip of the propeller blade per Hartzell Composite Propeller Blade Field Maintenance and Minor Repair Manual 170 Revision 21, Ch. 61-13-70. Ac.complished all required operational and functional checks with satisfactory results. The Propeller identified above was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration a~ i$ approved for retu~ serv~tt:ertinent details are on file under the above work order. Signed "44 iii!!! f • {J Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C -- -- ~ C Pages