Aircraft Log

AIRCRAFT LOG PIPER AIRCRAFT , INC. General Offices at Vero Beach, Florida U.S.A. Aircraft Registration number Part No. 230715 AIRCRAFf DESCRIPTION Registration No . NCO 0 '3 E Model: PA - 4' - (,00 i P Popular Name: M (, 00 Serial No.: 4('9 g IS (, Type CertifIc ate No. ____ _ ",,910\ Itl &4 S'".:). Colors: rnA'-"'T ER \\0 R N W H:I. JSI:E'E.L e,LU E q.. T:r TA Nl.lAM Engine Manufacturer : 1> RA T T + W H:r. , N E. Y Serial Numbers: Single PC £ - /?f{\ 0 qQ4 Left _______________ ___ Original Engi ne Model: 1', vA - 4) A Right _______________ _ Propeller Manufacturer : \-\ A T 2 &: L-L Hub or Serial Number :Single ____ Original Propell er Model: 5 1>3 - N 33 <l A \ Left _____________ _ Right ______________ _ Blade Numbers Left Right c. V 30;2 c 5359 C (,088 2020 MODEL c "0 II -- --- COMPLIANCE WITH FAA AIRWORTHINESS DIRECTIVES Time on Date of Signature and A. D. No. Method of Compliance (See log for Detail.) Aircraft Compliance and Date Certificate No. 3.8 IDEC 15 2020 All applicable Federal Aviation Administration Airworthiness Directives, through Bi-Weekly a0 ;1 0 - d 5 , have been complied with at the time of manufacture . A.D. 2020-16-08 Aspen Avionics, Inc ., Evolution Flight Display (EFD) EFD1000 Primary Flight Display , EFD1000 Multi-Function Display, and EFD1000 Emergency Back p Display is found NIA by Part Number 910-00001-501 Rev , SIN ';9 // 0 . ., . .., .,,--- ... M. . --- -- - - -- -- l Aircraft Time 1 Date This Date Total Brought DEC I 5 2020 ... Forward '" AIRCRAFT lOG Recorder Maintenance Reading = The Altimeter and Stati c Sy stem Test required by FAR 91.411 have been performed . Th e altimeter( s) have been tested: ! On (Pri) 1/ISI1.°at 55,000 ft. (Sec) CJ/1S/1...0at 55,000 ft. - i ........................................................................ .... ......... ............. ...... ' : The ELT is installed per FAR 91.207: " Battery Rep lacement date: 5 Ef 1. Db - ............................. ... .. .. ....................................................... ............. The ATC Transponder Tests and Inspection s required by FAR 91.413 were performed this date and found to comply with "FAR 43, Appendix F. _ _ 1. Make..Gm:min Model SIN 35912 . MakeJLJ:u:min Model SIN Jf o:lS' Details of this inspections are on File at this faci l ity under : AFT SI N 469815 " Date II/III, b 0].0 I The Automatic Pres sur e Altitude Reporting Equipment Te, by , FAR Part 91.217 have been performed this date : lilt I 0 , ...." .. " " .." ............" ,.....,., ... ,.. ... ,...." .... ,.. ,..." .........l ....,.l.., .." .. ,." .. " i The standby altimeter and static system test required by FAR Part 91.411 have been performt. The standby altimeter has been tested to 4Q,QQQ ft , on ' 2., J h'> &Q , -- I , ...... ... ..... ........... ......................... .... ... ............................................... I find that the aircraft meet, the requirement, for the certification request ed and have issued a Standard Airworthiness Certificate. Sig natur. Date: .DfC 1 5 202a M. 148315679 -- Total To Carry Forward 3.8 Registration No. f\f <g 0 E and Remarks p iper installed AMSAFE Aviation Inflatable Restraints for the Pilot and t o-Pilot Seats Per STC SA02276AK (Ref: Dwg. 46GOOAOOO Complete - PA-46-600TP and PC 206 PLR. ) Signed: 1-."'" . 14m7S6m Airframe N8023E Model : PA-46-600TP SIN : 4698156 Date : 18 December 2020 Signature Certificate No. 10'913\1 OilV' I.Ilvc:u:r.g\ Exp.: 12/22/2a22 ADC64 98(35 94381 Ifactivated; call the AFRCC at 1-888-851-3851 I I Hobbs Time 9.8 Total Time 9.8 Landings C. I<C Work Order A-20.Q0578 K",-....e Installed battery charger wiring provisions kit PIN BM -AIK1 in the engine compartment RH side per kit instructions This installation has been evaluated and determined to be a minor alterati on . Accomplished all requ ired 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 Olathe KS 66062 (913) 782-0530 FAA Repa ir Station #AMYR171 C AIRCRAFT lOG ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORAOO 80112 (303) 799-8386 N8023E Piper PA-46-600TP SIN: 4698156 Total Time: 27.7 20 February 2021 Hobbs: 27.7 Complied Piper Service Letter 12868 (Nose Landing gear Steering Components) per service letter instructions and the Piper Maintenance Manual Chapter 27-1-,27-20, 32-\ 0, 32-30. Adjusted nose roller clearance, both rods between the rudder pedals and steering bellcrank, steering bungee, rudder cable and yaw servo cable tensions. Removed one thin washer between each main gear center torque link and installed one thick washer to align the main landing. Checked rudder I aileron interconnect. Control system freedom of movement and stop check was good. Inst ed ne add' ional forward USB power outlet with a circuit breaker in the right circuit breaker ___ _ wlo 41997 I Airframe Model: SIN: Date: N2lG PA-46-600TP 4698156 19 March 2021 KC c.K."..., Clt;y AI.AacoOn a.,t:at' Hobbs Time: Total Time: landings: Work Order: 29.9 29.9 5·21·00079 Installed new registration markings N2LG per the requirements of 14 CFR 45 Subpart C. Changed transponder settings to reflect new ta il number per Piper PA·46·600TP AMM 767·617 ch 34·25·03 . The ATC transponder system has been tested and inspected as required by FAR 91.413(b)&(c) and was found to comply with appendix E of FAR 43. Removed Artex EL T1000 SIN 387263·043 for tail number reprogramming . "El T not installed" placard installed in cockpit. 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 Olathe KS 66062 (913) 782·0530 FAA Repair Station #AMYR171C Registration __L"",-"q"f-____ _ 1 - • = ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD , COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Total Time: 34.1 24 April 2021 Hobbs: 34.1 Installed Artex 1000 EL T PIN: A3-06-2749-l Rev E, SIN: 323-00855 after reprogramming for registration c ange. Beacon ID ADC64 92499 9A6B 1. Functional check good after installation. Scott L. Utz A&P3442269 w/o 42206 ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA 46-600TP SIN: 4698156 Aircraft Total Time: 41.6 10 June 2021 Hobbs: 41.6 Completed )'t 50 Hour Inspection per Piper form 765-044. General inspection of aircraft per check list. Checked cable tensions . Adjusted the Roll Servo, Yaw Servo and Pitch Servo cable tensions as needed. Installed new grease fittings on the upper nose landing gear strut. Resealed pin in auto-throttle servo and completed servo functional check. Complied with Piper Service Bulletin 1364A (Fuel Quantity Capacitance Probe Check) by draining all fuel and checking individual probe values. All 10 probes checked good with values less than table 2 of the service bulletin. Completed fuel accuracy check, check was good. Serviced tires per Piper Service Letter 1285A. Completed servicing and lubrication per check list. Fire Extinguisher weight check at 2 pound ounc s. und run up and operational check good. AD's checked thorugh bi-weekly 2021-12. w/ 042317 - AIRCRAFT LOG Airframe N2LG Hcbbs Time: 43 .8 Model PA-46-600TP Total Time: 43.8 SIN 4698156 Landings: .Date 11 June 2021 K" n noo Cicy A v lQt;on Cfytu,r Work Order: 5-21-00175 Downloaded and cleared fault data ; Straightened upper passenger door seal rail and applied RTV to nicks in the door seal. Accomplished all required operationa l 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 Olathe KS 66062 (913) 782-0530 FAA Repair Station #AMYR171C Total To Carry Forward , Registration __________ _ .... . . ... - - cr,l - -'ificole No . INTERNATIONAL AIRPORT DE ::; MO i NE S PO BOX 35126 - DES MOINES, IOWA 50315-0302 TELEPHONE (515) 256-5300 - FAX (515) 256-5537 dmfs .com PIPER 6/16/2021 N2LG SN 46-98156 PA-46-600TP HOBBS: 44.7 Removed the auto-throttle servo , Garmin Part Number 011-03780-00 Serial Number 4JM003290 and installed a New auto-throttle servo, Garmin Part Number 011-03780-00 Serial Number 4JM004487 . Loaded software and configurations into the new servo in accordance with the Piper M600 Maintenance Manual. This aircraft , airframe, aircraft engine , propeller , or appliance identified above, was repaired, and inspected in accordance with current regulations of the Federal Aviation Agency and is approved for return to service . Pertinent details of the repair are on file at this agency under Work Order N9 21455 . @ Date Signed Des Moines Flying Service , Inc ., FAA CRS G9CR485J - [- INTERNATIONAL AIRPORT PO BOX 35126 - DES MOINES, IOWA 50315-0302 DE S M O I N ES ntenance TELEPHONE (515) 256-5300 - FAX (515) 256-5537 dmfs.com PIPER 6/16/2021 N2LG SN 46-98156 PA-46-600TP HOBBS : 44 .7 Calibrated the standby Aspen Air Data Computer in accordance with the Aspen Avionics Tech Note For Air Data Calibration, Tech Note 2009-09 Rev D, dated 04-07-2016. Complied with CFR 91.411. I certify that the air datas and static system tests required by FAR 91.411 have been performed . The air datas and altimeter have been tested to 30,000 feet. Date 6/16/2021 Pilots Air Data PIN: 011 -03734-00 SIN : 45S000369 Co-Pilot Air Data PIN: 011 -03734-00 SIN: 45S000386 and Standby Aspen Air Data PIN: 910-00001-501 MOD1 SIN: 29110 DMFS Seq No. 6145 . Complied with CFR 91.413 191 .217 on the #1 Transponder Garmin PIN: 011 -01215-30 SIN : 3EF023584 and the #2 Transponder Garmin PIN : 011-01217-30 SIN: 3EH028489 . I certify that the transponder and mode CIS data correspondence tests and inspections required by FAR 91 .217 and 91.413 have been performed in accordance with FAR 43 Appendices "E " and "F". Complied with Aeromech ICA for Piper PA-46-600TP Airplanes Qua lified for Operations Within RVSM Airspace, document no. AM0325-IC01 -05, dated 09/20/2019. This aircraft , airframe , aircraft engine, propeller , or appliance identified above , was repaired , and inspected in accordance with current regulations of the Federal Aviation Agency and is approved for return to service . Pertinent details of the repair are on file at this agency under Work Order N2 21454 . @T9 q 0,1, Sig,,,, Des Moines Flying Service, Inc., FAA CRS G9CR485J Airirame N2LG Hobbs Time Model: PA-46-S00TP I<C · C. Total Time SIN: 4698156 Landings Date: 20 October 2021 Keneell!"J Ctty A\I'I.!IItlon c.rmer Work Order 78.2 78.2 5·21-00289 Removed and replaced aircraft registry markings with new markings (N2LG). Aircraft registry has not changed. The Aircraft identified was repaired and inspected in accordance with current Regulations of the Federal Aviation Administration and Pertinent details are on file under the above work order. Olathe KS 66062 (913) 782·0530 FAA Repair Station #AMYR171C IS approved fof.l eturn)o ihfJIice. Signed '" - - - -AIRCRAFT lOG Aircraft Time Recorder Date 1 1 Maintenance Reading This Date Total Iii ARAPAHOE AERO 12760 EAST CON T ROL TOWER ROAD ENG L EWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 95.9 14 January 2022 Hobbs: 95.9 Landings: Event 1 I Event 2 I Annual Inspection completed this date using the Piper Inspection Event work sheets . Worksheets contain the scope and detail of FAR 43 Appendix D. Inspected and tested Artex ELT 1000 per manufactures service instructions, FAR 91.207 . WS Technologies beacon test report BTl OOA V triple /31951N2LG-12-10-1 on file. ELT battery expires September 2026 . Completed 30 day, 90 da y, 6 month , 12 month, 50 hour section inspe ction items . Installed a new strobe flasher PIN: 479-007 SIN : I 1499450003 in the right-wing tip. Fit and installed new left- and right-wing tip light lenses . Adjusted interior left side interior cover around pitot static drains for clearance . Installed a new flap indicator . potentiometer and adjusted . Installed a new emergency ex it seal. Reattached lower cabin step material as needed . Secured right wing outboard aft de-ice boot edge as needed . Applied sealant around the right-wing stall strip to seal edges . Secured hardware for the lower cabin door interior panel. Trimmed forward right- side panel under the instrument panel for better fit. Inspected both fuel tank vent valves. Adjusted the right valve so the hinge was on top. Put aircraft on jacks and ran landing gear retraction and extension checks . Checked rigging , indication , clearance and emergency extension system . Completed 100 hour I Annual lubrication schedule. Cleaned, inspected and serviced wheel bearings . Ran landing gear through at least 5 fault free cycles. A II land ing gear operations and indications were normal. Completed IOO-hour engine mount and firewall inspection , no defects noted. Complied with Piper SO 1369 (Elevator spar) by visual inspection , no defects found . Completed with Piper SO 1367 (Aft rib assembly rivets replacement) by II replacing protruding head rivets with flush rivets per service instructions. Complied with Piper SO 1370 (Inertial Separator Duct Shredder Angle) by visual inspection , no cracks or missing pieces noted. Installed reinforcement kit 88700-70 I per service instructions . Page I Registration No. ___________ _ and Remarks Signature Certificate No. ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 95.9 14 January 2022 Hobbs: 95.9 Landings: Complied with Piper Service Letter 1292A (Software update 2975 .22) by updatin g G3000NG system software from 2975.17 to 2975.22 per Piper drawing 88704 . Options loaded as follows : System ID 25EA09E3E, baseline PA-46-600TP, Emergenc y Autoland, Configuration A (GTX335, GTX345 , FS510, Enhanced AFSC Support, Flight Stream 510 , GDL 69A (SXM), GRA 55, WX-500 , Unlocks : Enhanced AFCS, Chartview, SVT , TAWS , TCAS I, SurfaceWatch , Ground Clutter Suppression & Turbulence Detection , Emergenc y Autoland Enablement, G WX 8000 Enablement (Auto, GCS, &TD, Service Spares Letter 514). Loaded CMC (M600.13). Completed system check out. All items checked good , no faults. Complied with Piper SB 1371 (Wing Assem bly Serialization Marking) by marking bo th wings per service instructions. Piper AD 2019-12-12 (Rivets) N/A by aircraft SIN. Piper AD 2018-14-01 (Skin Joint failure) NIA by aircraft SIN. Piper AD 2017-16-03 (Aft wing spar) NI A by aircraft serial number. Post inspection ground run up and system check was good . AD's checked through bi-weekly 2022-0 I. I CERTIFY THAT THIS AIRCRAFT HAS BEEN ;rED IN ACCORDANCE WITH AN EVENT 1 & 2 I ANNUAL INSPECTION (FAw WAS DETERMINED TO BE IN AIRWORTHY CONDITION . _____ _ r 131 w /o 42898 AIRCRAFT lOG ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 111.7 17 March 2022 Hobbs: 111.7 Complied with Piper Service Letter 1301 (Autothrottle Enablement) by applying Piper Service kit 88661-702. lnstalled autopilot mode controller GMC 711, SIN: 58K000594. Completed LRU software replacement per 34-25-03 and feature enablement (placed unlock card in card holder) Completed system check out of installation per 88661-702, 88704 and the Piper Maintenance Manual Chapter 34-25-03. Completed auto throttle potentiometer calibration (rigging). System checkout was good. Verified system software levels per Chapter 34-25-03 , Chart 40. Ground run up and operational check good. Placed new cockpit reference guide in aircraft . No weight and balance change per service instructions. lnstalled a new post light assembly on top of the oxygen cabinet. Complied with Piper SL 1296 (Flap Fail Module) by new part number check good. Adjusted both aft seat back recline button arms as needed. / Michael J Nigro A&P3443 131 w/o 43068 Total To Carry Forward i. Registration No. ___________ _ • ARAP AHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 180.3 I February 2023 Hobbs: 180.3 Landings: 110 Event I I Event 2 I Annual Inspection completed this date using the Piper In spection Event work sheets Chapter OS-20-00, OS-30-00. The checklist contains at least the scope and detail of FAR 43 Appendix D. Inspected and tested Artex ELT 1000 per manufactures service instructions, FAR 91.207 . WS Technologies beacon test report BTl OOA V triple/319SIN2LG-12-1 0-1 on file. EL T battery expires Septem ber 2026 . Completed 30 day, 90 day, 6 month , 12 month , 24 month special inspection items. Put aircraft on jacks and ran landing gear retraction and extension checks. Checked rigging, indication, clearance and emergency extension system . Completed 100 hour I Annual lubrication schedule . Installed three new landing gar tires . Disassembl ed all three wheel assemblies, cleaned, inspected and reassembled with new tires Left main 18SF88-6, SIN: 22800833, Right SIN: 27760734 and new seals. Nose tire SOSCO I-S, SIN : 11930071 with a new inner tube . Balanced all three assemblies. Cleaned , inspected and serviced wheel bearings. Serviced tires per SL 128SC. Serviced struts with nitrogen. Ran landing gear through at least S fau It free cycles . A 11 landing gear operations and indications were normal. Com plied with Piper SL 12860 (Nose Landing Gear Components), Adjusted Aileron , Rudder, Pitch Trim, Roll Servo and Pitch servo cable tensions. Completed I OO-hour engine mount and firewall inspection , no defects noted . Complied with Piper SL 1314 (02 generator) by inspection, no defects . Repaired wire between pulse light relay at pulse light switch. Tightened right navigation antenna in block on the vertical stabilizer. Completed Annual ICA for AmSafe crew air bag seat belt system, check was good. Post inspection ground run up and system check was good. Cleaned windows , vacuumed interior , treated de-ice boots. Piper AD 2022-11-10 (Wing Splice 46W57AI00-001) See Airworthiness Limitation section of the maintenance manual. Wing splice life limit 3,767 hours. AD's checked through bi-weekly 2023-03. I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN EVENT 1& 2 I ANNUAL D) AND WAS DETERMINED TO BE IN AIRWORTHY CON . . Michael Nigro A&P34431311A w/o 439S0 7 / I ARAPAHOE AERO AVIONICS 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SI N: 4698156 Aircraft Total Time: 189.5 10 March 2023 Hobbs: 189.5 Removed Aspen Remote Sensor PIN: 910-00003-503, SIN: 501007 and installed replacement unit as supplied by Aspen PIN: 910-00003-503, SIN: 501134. Completed calibration procedure and system check out per Aspen document 900-00003-00 I. Installed a new upper cabin door hydraulic cylinder. Piper Ser0ge l:.et!eJ-1284 no update required Aspen system software level is 2.10.2 . WIO A V-04862 . Scott L. Utz A&P3442269 CRS #ZLR6R006Y Total To Carry Forward Registration No.___________ _ and Remarks Signature Certificate No. N2LG Piper PA-46-600TP 6-9-2023 Academy Aero LLC SN:4698156 the 24 month certification of the # I /2 static pressure systems. The # 1/2 static pressure system tests and inspections. # 1/#2 Standby Altimeter, and automatic pressure altitude reportmg system tests required by Title 14 CFR Part 91.411 , and the # 1/#2 ransponder's tests and inspection required by Title 14 CFR Part 91.4 ,13 have been performed an found to comply with Title 14 Part 43 , Appendices E and F. the components listed below to RVSM standards I.A. W the Instructions for Continued Airworthiness found in the Aeromech Instructions for Initial and Continued Airworthiness for Piper Model PA·46-600TP (M600) Airplanes Qualified for within RVSM Airspace section 1.4.2 steps I-S. Customer to perform step 6 (In-flight altitude hold check) as required. of the RVSM 3D scarming test were submitted to Aeromech Incorporated and were found to PASS. I ADC GDC-72 PIN:0II-03734-00 SIN:4SS000369 . #2 ADC GDC-72 PN :OII-03734-00 , SN:4SS000386 Standby Altimeter EFD- PIN:91O-00001-S01 SIN :29 I 10 #1 Transponder GTX-33SR PIN:011-03301-00 SINJEF023S84. #2 Transponder GTX-34SR 11-03303-00 SIN:3EH028489 . above listed equipment, altitude reporting system data correspondence , and aircraft static system were tested to 30,000 feet on standby Aspen altimeter did meet the listed in ,91.411. Performed a calibrati.on of the Aspen the Aspen AVIOnICS Tech Note for Air Data CalIbratIon 2009-009 sectIon 14 & IS and found the altImeter to now be wlthm the cation listed herein in . above described repair or maintenance is approved for return to service. Pertinent details of this repair/maintenance are on file at repair station under Work Order #9RPLA . 4 / I /,.?' /V for Duncan Avionics; Englewood, CO 80112 Total Time: 220.1 Total Landings: AIRCRAFT lOG ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 801 12 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Log Entry 12 June 2023 Hobbs: 220.1 Replaced exterior window edge sealant on left and right side windows and the co-pilots windshield . Adjusted #5 seat back latch. Operational check good . ---:::;:> Aaron Peter Villery A&P 3224687 w/o 44376 Total To Carry Forward Registration No. ___________ _ ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 260.6 1 February 2024 Hobbs: 260.6 Landings: Event 1 1 Event 2 1Annual Inspection completed this date using the Piper Inspection Event work sheets Chapter 05-20-00, 05-30-00 . The checklist contains at least the scope and detail of FAR 43 Appendix D. Inspected 1Tested Artex EL T 1000 system according to applicable Aircraft and EL T manufacturer's instructions and found that it meets the requirement of section 91.207(d) . No defect noted , Beacon Test Report No. BTIOOAVtriple/3195 1 N2LG-0 1/03/2024 dated on file. ELT battery expires September 2026 . Completed 30 day, 90 day , 6 month , 12 month, 24 month special inspection items. 5-30-00 . Removed pilot side USB port PIN: TA202, SIN: A19-11430 and installed new port SIN : H22-13508. Applied Velcro to allow oxygen drawer to stay closed. Adjusted left rear seat spring . Installed new sealant for two lower left ' side passenger windows. Installed new white taillight assembly PIN : 01-0771774 V02, SIN: 661114. Installed new cabin door seal PIN: 88440-002 . Complied with 2 Year 1400-hour Fuel Purge System inspection and cleaned purged can, check valve, functional check good . Complied with Piper SL 1314 (02 Generator) by verifying removal of protective covers , condition of percussion caps. Complied with Piper SB 1369 (Elevator Spar) by visual inspection, no defects noted , Put aircraft on jacks and ran landing gear retraction and extension checks. Checked rigging, indication, clearance and emergency extension system. - Completed 100 hour ! Annual lubrication schedule. Cleaned, inspected and serviced wheel bearings. Serviced tires per SL 1285C. Complied with Piper SL 1310A (Unpaved Field Operations) by installing nose landing gear and wheel well modification kit PIN : 88705-70 I per Instructions 88705 Rev E. Complied with Piper SL 1286D (Nose Landing Gear Components) Serviced struts with nitrogen. Ran landing gear through at least 5 fault free cycles. All landing gear operations and indications were normal. Page I ------- ________________________________ L- __________ AI RCRAFT LOG ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 260.6 1 February 2024 Hobbs: 260.6 Landings: Completed Piper SL 1292C (Software version 2975.24) by updating system software from version 2975.22 to version 2975.24 per Piper Drawing 88704 Rev D. Options loaded as follows; PA46 Baseline, System ID 25EA09E3E , emergency Autoland plus autothrottle, Configuration A GTX335 , GTX345 with GTS and Flighstream, Enhanced AFCS Support, Flight Stream 510, GDL 69A (SXM) , GRA 55, WX-500 , Splash Screen Update, Unlocks ; Enhanced AFCS, Chartveiw , SVT, TAWS, TCAS-I , SurfaceWatch , Ground Clutter Suppression & Turbulence Detection, Emergency Autoland, GWX 8000, Normal use Autothrottle , CMC (M600 . 15). Completed system checkout and autothrottle potentiometer rigging calibration. System check out was good. Complied with Piper SB 1230 A (G3000 Check List) by updating MFD checklist to VB-2793 RI3 per service instructions. Complied with Piper SB 1411 (AP Rigging) by verifying correct rigging on servos. Complied with Piper VSP 288 (Cable Retention Pins Garm in SB 22117) by installing new pins for the yaw, pitch trim and roll servo. Piper SL 1284A (Aspen EFD I 000 MAX Software) verified unit has current software 2.10 .2, no action required. Piper AD 2023-25- 02 (Control Column) N/A by serial number. Completed AnnuailCA for Am Safe crew air bag seat belt system, check was good. Post inspection ground run up and system check was good. Cleaned windows, vacuumed interior, treated de-ice boots. AD's checked through bi-weekly 2024-02 . I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IN ACCORDANCE WITH AN EVENT 1 & 2 I ANNUAL INSPECTION (FAR 43 APPENDIX D) AND WAS DETERMINED TO BE IN ff,hY' /ff Michael Nigro A&P3443131 IA wlo 44859 . - I:':':;:;:;:;:;:;:;:;:;:;:;:;:;::::::::::j Carry Forward:::::::::::::::::::::::::::::::::::::::: . Registration No. ___________ _ ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Piper PA-46-600TP SIN: 4698156 Aircraft Total Time: 288.8 8 May 2024 Hobbs: 288.8 Serviced all three struts with hydraulic fluid and nitrogen. Complied with Piper SL 1315 (Elevator Trim Tab Jw1fistalling new sealed PIN: 102846-005 control tubes. Serviced tires. w,./,/h-- Micheal NigroA&P3443131 w/o 44839 & 45189 ARAPAHOE AERO AVIONICS 12780 E Control Tower Rd Englewood, CO 80112 303.799.6289 N2LG Piper M600 SN: 4698156 ACTT: 288.8 May 8,2024 Owner reports Aspen EFD 1000 shuts down randomly for roughly 15 minutes in flight. Removed and sent Aspen EFD . 1000 MAX 910-00001-501 , SN:291 10 to Aspen Avionic s for evaluation and repair under RMA 39673 . They confirmed the reported issue and repl aced the main circuit board. Installed Aspen EFD 1000 MAX 910-00001-501, SN:29110 per Aspen EFDIOOO leA 900-00012-001 Rev AF. No defect s noted . The aircraft and/or component identified above have been inspected in accordance with the current maintenance rules of the Federal Aviation Re ula . nd is approved for return to service. FAA CRS ZL6R006Y AV-05063 - - Transport Transports TP 14182 Canada Canada (Rev ised OS/2005) 1+1 Engine Logbook TC -100 1185 I 11111111 1111 III 111111 11111 1m 1I11111111111111111111111111 Canada 0512005 Volume #: _ Opened on : 2 9 SEP 2020 ENGINE DETAILS 1. Manufacturer Pratt & Whitney Canada Corp. 2. Type/Model/Series 3. Serial Number E.T.C. E- /01.. PT6A- PCE- __ Kn1 oct.l Lf Lj;J..4 B/S: 1415 THIS ENGINE SERVICED WITH bp TURBO 2380 OIL AT THE PIPER FACTORY CYCLE COUNT AS OF DEC 1 5 2020 NUMBEROFCYCLES ______ __________ (il L -- -------- ---- I Section 1: Record of engine maintenance and elementary work Date Time since Time since Total cycles Details of task --/--/-- new overhaul 2 9 SEP 2020 0(0 /'Ilri 0 New engine final acceptance test and -- inhibiting run completed satisfactorily r L--- - and is in condition for safe operation. -f --- --r------ 1- ----- 0.0 1:3 OCi' NIIl 0 "Applied Procyon corrosion inhibitor to compressor iniet case per Pratt & Whitney Maintenance Manual PIN -t--- 3021442 Chapter 72-00-00." -- - I----- 1------ D".#Aircraft SIN: 4'981&' Reg. Number: N Aircraft Engine Model: PT6A-42A SIN: 9Z.-f Date:! Z/;3/?() , I Aircraft SIN: q,q ISC- Reg. Number: N80t..3E TIE: . i Cycl I Perlormed Engine water Was per;;,at! & ' .... i.no.. Unin'enance Manual Part Number 3021 2 P"" Cleaning, Engine Washing I s. Signature: / ... ..... , Aircraft Engine Model: PT6A-42A SIN : PCE- ko '1 z m3.£ Ii. 'I Perlormed Engine Water as pe'/f_rat! & Wh itney . ance MM"" PM P _ P"" Cleanmg, Engine Washin I . ns7 ""' . " .-Name: David T Wallace Jr A&P Certificate Number: AP51627416 PIPER AIRCRAFT, INC. Signature: / ' " " Name: David T Wallace Jr A&P Certificate Number: AP 51627416 ! PIPER AIRCRAFT, INC. I - 'r - -- I - -- -- - ARAPAHOE AERO - 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 - N2LG Pratt & Whitney PT6A-42A SIN: 4698156 Engine Total Time: 41.6 10 June 2021 Hobbs: 41.6 - Completed )'150 Hour Inspection per Piper form PIN : 765-044. General inspection of engine and engine - components. Checked and lubricated engine control linkage . Checked belts tensions. Completed compressor and compressor tur wash per Pratt & Whitney service instructions. Ground run f- up operational check good -,/ Scott L. Utz A&P3442269 f- w/ o42317 .10_ -, ;r AME Signature ACAJAMO SCAJAMO 353a? RPM, at B:'JD SHP/frv0 1 ITT Trim: 30,7 co - 3Lf.tf T5 Trim Resistance: Ohms J J " ; F== ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD , COLORADO 80112 (303) 799-8386 N2LG Pratt & Whitney PT6A-42A SI N: PCE-RM0924 Engine Total Time: 95.9 14 January 2022 Hobbs: 95.9 Cycles: Event 1 I Event 2 I Annual Inspection completed this date using the Piper InspeCtion Event work sheets J Chapter 5-20-00 and Pratt & Whitney Maintenance Manual Table 60 I. Check list contain the scope and " detail of FAR 43 Appendix D. Completed minor and routine inspection and service items . Removed, "I' inspected, cleaned and reinstalled the oil tilter. Removed , inspected, cleaned and reinstalled the P3 tilter and P3 tilter housing . Checked the P3 tilter drain . Removed, inspected, cleaned and reinstalled the fuel inlet tilter. Installed a new fuel outlet tilter. Checked chip detector. Serviced control linkages. Secured fuel hose aft of air conditioning compressor as needed to gain clearance . Adjusted routing of fuel hose near manual override on fuel control to gain clearance. Completed CT wash and rinse. Added two quart of 2380 · turbine oil. Ground run up, leak check and operational check good. AD's checked through bi-weekly 2022- J 01. I CERTIFY THAT THIS ENGINE IN ACCORDANCE WITH AN J EVENT 1 & 2 INSPECTION (FAR AND WAS DETERMINED TO BE IN AIRWORTHY CONDTION. . Michael J . Nigro A& 443131 w/o 42898 ) ] 1! ARAP AHOE AERO J 12760 EAST CONTROL TOWER ROAD ENGLEWOOD , COLORADO 801 12 (303) 799 -8386 N2LG Pratt & Whitney PT6A-42A SIN: PCE-RM0924 Engine Total Time: 180.3 " I February 2023 Hobbs: 180.3 Cycles: 107 Event 1 I Event 2 I Annual Inspection completed this date using the Piper Inspection Event work sheets Chapter 5-20-00, 5-30-00 and Pratt & Whitney Maintenance Manual Table 60 I. Check list contain the J scope and detail of FAR 43 Appendix D. Completed minor and routine inspection and service items . 1 Removed, inspected, cleaned and reinstalled the oil tilter. Removed, inspected, cleaned and reinstalled the , P3 tilter and P3 tilter housing. Checked the P3 tilter drain . Removed , inspected , cleaned and reinstalled the fuel inlet tilter. Installed a new fuel outlet tilter. Checked chip detector. Serviced control linkages . 1 Completed CT wash and rinse. Added two quarts of2380 turbine oil. Ground run up, leak check and 'f operational check good . AD ' s checked through bi-weekly 2023-03 . I CERTIFY THAT THIS ENGINE HAS BEEN WITH AN EVENT I & 2 INSPECTION (FAR 43 · APPENDIX D) R D TO BE IN AIRWORTHY CONDTION. I Michael J. Nigro A&P3443131 w/o 43950 1 " I ; . 1 ..1 ! Page' · Section 1: Record of engine maintenance and elementary work Date --/--/-- Time since new Time since overhaul Total cycles Details of task ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD , COLORADO 80112 (303) 799-8386 N2LG Pratt & Whitney PT6A-42A SIN: PCE-RM0924 Engine Total Time: 260.6 I February 2024 Hobbs: 260.6 Cycles: Event I I Event 2 I Annual Inspection completed this date using the Piper Inspection Event work sheets Chapter 5-20-00,5-30-00 and Pratt & Whitney Maintenance Manual Table 60 I. Check lists contain at least the scope and detail of FAR 43 Appendix D. Completed minor and routine inspection and service items per Pratt & Whitney service instructions Table 60 I. Removed, inspected, cleaned and reinstalled the oil filter. Removed, inspected, cleaned and reinstalled the P3 filter and P3 filter housing . Checked the P3 filter drain . Removed, inspected, cleaned and reinstalled the fuel inlet filter . Installed a new fuel outlet filter. Checked chip detector. Serviced control linkages . Completed borescope inspection of 1'1 stage compressor and engine inlet, no defects noted. Installed two new oil seals for the air conditioner I alternator accessory drive. Completed CT wash and rinse . Added two quarts of2380 turbine oil. Complied with Pratt & Whitney SB 3522 (Ignition cable assembly) by inspection of ignition lead date codes 4L 19 and 4A20 are installed, no action required . Ground run up, leak check and operational check good. AD's checked through bi-weekly 2024-02. I CERTIFY THAT THIS ENGINE HAS BEEN INSPECTED IN ACCORDANCE WITH AN EVENT I & 2 INSPECTION (FAR 43 APPENDIX D) AND WAS DETERMINED TO BE IN Michael J. Nigro A&P3443131 w/o 44859 ;, 1 lJ1 I JI ·1 ' -e- ------ HARTZELL PROPELLER LOGBOOK PROPELLER MODEL 5 1)'3 - A/3 38 A I PROPELLER SIN SF' LOGBOOK # I Date Propeller Ale Description of all operations pertaining to Airworthiness Directives, TSN TSO Hrs Service Documents, Overhaul, Major or Minor Repair, and Inspections. [S@@ Date: Wo Hobbs Time: • (f Aircraft SIN : 0/,fBIS' Reg . Number: NZOa"3t. Prop Model: SOJ - "''3561. I SIN : .5F Z '" th P,"o""ed L,b,;",Uo" of Pmo by:WFI;,ht T"U", wllh NYCO GN3058 PC' I, " 0" Q:.'", - hours operation. Signature: '-- Name: David T Wallace JR A&P Certificate Number: AP51627416 Pi,!er' PIPER AIRCRAFT, INC. - .- -_.- c- . ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Hartzell 5D3-N338Al SIN: SF266 Propeller Total Time: 41.6 10 June 2021 Hobbs: 41.6 Completed pi 50 Hour Inspection per Piper fonn PIN: 765-044. General inspection of propeller, bulkhead and lubrication. Completed propeller heat inspection and operational test. /" Scott 1.. Utz A&P3442269 wlo 42317 P - ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Hartzell 5D3-N338Al SfN: SF266 Propeller Total Time: 95.9 14 January 2022 Hobbs: 95.9 Event 1 I Event 2 I Annual Inspection completed this date using Piper Inspection Event work sheets Chapter 5-20-00 as a guide . Check lists contain at least the scope and detail of FAR 43 Appendix D. Reference Hartzell Owner's Manual 486. Completed Annual Propeller Lubrication (Nyco grease). Completed propeller heat inspection. Checked hub, blades, spinner and bulkheads . Ground run up, operational check good. AD's checked through bi-weekly 2022-01. I CERTIFY THAT THIS PROPELLER HAS BEEN INPSECTED IN ACCORDANCE WITH AN EVENT 1 & 2 INSPECTlON D) AND WAS DETERMINED TO BE IN AIRWORTHY CONDITlON. Michael J. Nigro A&P34431331 wlo 42898 Page 1 ..I Date ARAPAHOE AERO n 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Hartzell SD3-N338AI SIN: SF266 Propeller Total Time: 180.3 = I February 2023 Hobbs: 180.3 Event I I Event 2 I Annual Inspection completed this date using Piper lnspection Event work sheets Chapter 5-20-00, 5-30-00 as a guide. Check lists contain at least the scope and detail of FAR 43 Appendix D. Reference Hartzell Owner's Manua'i 486. Completed Annual Propeller Lubrication (Nyco grease) . Completed propeller heat inspection. Checked hub, blades , spinner aod bulkheads. Hartzell HC-ASB-61- 396 (Propeller Hub) applies to this propeUer. Compliance time is the next overhaul November 2026 or 4000 hours. Ground run up, operational check good. AD's checked through bi-weekly 2023-03. I CERTIFY THAT THIS PROPELLER HAS BEEN INPSECTED IN ACCORDANCE WITH AN EVENT I & (FAR 43 APPENI)IX Dj AND W AS DETERMINED TO BE IN AIRWORTHY N. Michael J. Nigro A&P34431331 w/o 43950 / / I I I ARAPAHOE AE"RO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD, COLORADO 80112 (303) 799-8386 N2LG Hartzell SD3-N338Al SIN:SF266 Propeller Total Time: 181.7 2 February 2023 Hobbs: 181.7 Completed dynamic propeller balance using the Aces system . Beginning reading was . . 59 IPS. Added 23.6 and 23.6 at 185 degrees. Final reading was .05 IPS. Scott L. Utz A&P3442269 w/o 44023 - ARAPAHOE AERO 12760 EAST CONTROL TOWER ROAD ENGLEWOOD , COLORADO 80112 (303) 799-8386 N2LG Hartzell SD3-N338AI SIN: SF266 Propeller Total Time: 260.6 1 February 2024 Hobbs: 260.6 . .' Event 1 I Event 2 I Annual Inspection completed this date usmg PIper lnspectIOn .Event work sheets . Chapter 5-20-00 5-30-00 as a guide. Check lists contain at least the scope and detail of FAR 43 AppendiX D. Reference H;rtzell Owner's Manual 486. Completed Annual Propeller Lubrication (NYCO GN3058 grease). Installed six new harness assemblies in accordance with Manual 180, Rev 42, December 2023. Completed propeller heat inspection . Checked hub, blades, spinner and bulkheads. Ground run up, operational check good. AD's checked through bi-weekly 2024-02. I CERTIFY THAT THIS PROPELLER HAS BEEN INPSECTED IN ACCORDANCE WITH AN EVENT I & 2 INSPECTION (FAR 43 APPENDIX D) AND WAS DETERMINED TO BE IN AIRWORTHY ...... /':7/' Michael J. Nigro A&P3443131 w/o 44859 Page 2