Aircraft Record General Information

Aircraft Record General Information

Manufacturer ________________ Model _ -----------------

Serial Registration Number ____________ _

Date of Manufacture __________________________________ _

Engine(s) currently installed:

Manufacturer ___________ Model ---------- Serial __________ _

Manufacturer Model Serial -----------

Propeller(s) currently installed:

Manufacturer ________________ Model __________________ _

HUB Model ----------- - Serial ____ Serial -----------

Blade Model Serial ______ Serial ______ Serial-------

Blade Model Serial Serial Serial ______ _

Annual Inspection I Airframe 06-04-2014 1497.0 Hobbs Meter N918AS PA32R-301T SN 3257029 Aircraft TT -1497.0 Inspection Complete per FAR 43 Appendix 0- performed the following service work: Removed then Installed Engine after Major OH by Poplar Grove Airmotive - See Engine Log Removed then Installed Prop & Governor after Major OH by Maxwell Aircraft - See Engine & Prop Log Removed then Installed Turbo, Wastegate, Controller, & Pressure Relief Valve after OH by Main Turbo Replaced All (22) Engine hoses with identical Teflon TSO C53-A Type D assemblies See PHT Inc Listing Removed then Installed Alternator after OH by Aerotech Engine installed with new Lord Mounts & AN Hardware Lubed flight control & airframe hinge points & rod end ball joints - LPS Serviced fuel strainer bolNt screen - no contamination found Greased landing gear linkages - Shell #22 Lubed landing gear actuator attach points, down lock mechanisms, & nongreaseable joints - LPS Serviced brake reservoir - Aeroshell #4 Hydraulic Fluid (5606) Replaced EL T Battery - PN 110-4 Checked EL T per FAR 91 .207 - OK - Batteries due May 2017 Checked Airworthiness Directives through 2014-11 on airframe - None Due Ldgn Gear Operational Check, Emergency Ext & Anti Retract systems, Lights, Throttle Horn, Doors - OK Aircraft Operational Checks & Test Flight Performed - OK

/ CERTIFY THAT THIS A IRCRAFT HAS BEEN INSPECTED IA WAN

ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDlnON ISAAC DETERS A&P 2714038 IA

I I ACR ELECTRONICS, Inc.

Fort Lauderd1l1, Fl 33312 CAGE Code: 111560 __ -J__JC-..JC-J~4--l--'-~~~>-lLip:...!.._-r-....!.:~>..=..::::""""--><..:""-'-'c.:.__i"'""""~>.=.!...:..:....ARTEX PRODUCTS

BATT!RY PACK: ILT 110-4 PART NO: 452-0130 REV. M

S.N.:36291~56

EXP. DATE: MAY/2017 ENV CATC IA/00183/XXXXXXX88888 no C9l1

-YEAR TOTAL Current Weight and Balance Information 20 __ TIMEIN

DATE SERVICE Empty Weight Empty CG Useful Load

io-10- l~ \S-Oh .n ~-~ ' \....~h.\\t.~ Annual Inspection I Airframe 09-02-2015 1530.0 Hobbs Meter N918AS PA32R-301T SN 3257029 Aircraft TT-1530.0 -Inspection Complete per FAR 43 Appendix D- performed the following service work: Installed Vacuum Pump PN: 241CC-15 SN: 163018 (FAA/PMA'd for AH1A Engine) & Adjusted Regulator Replaced landing gear up pressure switch with new - Piper PN: 587-847 (Eaton 211C243-12) 1800 PSI Replaced turnbuckle barrels during compliance of AD2013-02-13-done in lieu of insp/reuse of old barrels

Turnbuckle PN: MS21251-B5S Safety Clip PN: MS21256-1 Removed then installed both Turn coordinators after OH by Kelly Instruments Inc. W0#135333 & 135334

Pilot Side - Mid Continent EGC - PN: 1394T100-7Z SN: 9709-467 Copilot Side - Mid Continent EGC - PN: 1394T100-7Z SN: 9710-350

Replaced Main Gyro Filter- Rapco RA D9-18-1 Replaced Vacuum Regulator Filter - RAB3-5-1 Lubed fl ight control hinge points & rod end ball joints - LPS Serviced fuel strainer bowl & screen - No contamination found Serviced struts, brake reservoir, shimmy damper, & hydraulic power pack - Shell Fluid #4 I Mil-H-5606 Greased landing gear service points with Shell #22 - Lubed rod ends & non-greaseable joints with LPS Greased all wheel bearings - Shell #22 Greased stabilator trim & flap jack screw - Shell #33MS Lubed A/C condenser door linkage - LPS Checked EL T per FAR 91.207 - OK - Batteries due May 2017 Checked Airworthiness Directives through 2015-17 on airframe CW AD2013-02-13 Stabilizer Controls per Piper SB1245 - No discrepancies found

Due again at 3530.0 Hrs or October 1, 2022 (2000 Hrs or 7 Year Inspection) Ldgn Gear Operational Check, Emergency Ext & Anti Retract systems, Lights, Throttle Horn, Doors - OK Aircraft Operational Checks - OK

I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED /AW AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRY>tORTHY CONDITION ISAAC DETERS A&P 2714038 IA

YEAR 20 _ DATE

RECORDING TACH TIME

TODAY'S TOTAL FLIGHT TIME IN

SERVICE

Description of Inspections, Tests, Repairs and Alterations y Entries must be endorsed with Name. Rating and Certificate Number of ~ Technician or Repair Facility. (See back pages for other specific entries.) 0

I certify that the altimeter, static system, transponder, and altitude reporter test required by FARs

91.41 1, 91 .413 & 91 .217 have been performed and found to be within the limits of FAR 43 apper

ces E & F and AC 43.6a TESTED TO 1St C ~ 0 fr

Altimeter Model 5't }'(f{}- ""J., #1 S/N t{c"{/ I{(, Model 'i"C, 1.J'{/1'3>#2 SIN O 9 ·757~

Transponder Model kr-/U. (,,. #1 SIN "!;>o(() Model-¥-#2 S/N-lL

Altitude Model .4-R.-~ #1 S/N / G 'ifLO Model-4-#2 S/N/L

SIGNED _ _ u_....._""'4,<ij_.4,_.,~...._'/;.._.~""'""-""-~-)----------North Star Aviation. Inc. Mankato.MN 56001 0-(

7 A

FAA CRS# NUTR521L W/O# ______ Q_ ' __ /! __ _

' -YEJ 20 DA

Annual Inspection I Airframe 01-10-2017 1583.3 Hobbs Meter N918AS PA32R-301T SN 3257029 Aircraft TT -1583.3 Inspection Complete per FAR 43 Appendix D- performed the following service work: Replaced throttle quadrant cover - H69669-44 Replaced RH wingtip nav light & lens (Aft Facing White)-Whelen A-508-28 & A615 Lubed flight control hinge points & rod end ball joints - LPS Serviced fuel strainer bowl & screen - No contamination found Serviced struts - Dry Nitrogen Serviced brake reservoir - Shell Fluid #4 / Mil-H-5606 Greased landing gear service points with Shell #22 - Lubed rod ends & non-greaseable joints with LPS Checked EL T per FAR 91 .207 - OK - Batteries due May 2017 Checked Airworthiness Directives through 2017-01 on airframe- none due Ldgn Gear Operational Check, Emergency Ext & Anti Retract systems, Lights, Throttle Horn, Doors - OK Aircraft Operational Checks - OK

I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED IAW AN ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDITION ISAAC DETERS A&P 2714038 IA

ACll l!lfCTRONICS, Inc. -Fort u111derd•le, Fl. 3!312 CAGE Cod•: 18560

ARTEX PRODUCTS -Nw fL.\ ~ ... ~ BATTERY PACK: !LT 11C>-4

I PART NO: 452-0130 REV. N -~ tJt.>tt'?c, . S.N.:37'1915-019

EXP. DATE: SEP /2020 -ENV CATCWD0183/)000000(8BBBB TIO Cll.a

Annual Inspection I Airframe 03-10-2018 1617.5 Hobbs Meter N918AS PA32R-301T SN 3257029 Aircraft TI - 1617.5 Inspection Complete per FAR 43 Appendix D- performed the following service work: Replaced ELT Battery - 110-4 PN: 452-0130 Repaired alternator annunciator light fixture Air/Oil separator bowl repaired. Moisture pitting in bowl caused a leak that was welded by a local shop. Repaired rear seat intercom connection at quick disconnect plug Removed and discarded expired 02 bottle. Removed valve from bottle, sent valve for repair I testing Installed new bottle with original valve after repair I testing by C&L Aero WO# 010449 See 8130 Next hydrostatic test due December 2022 - Bottle Expires December 2032 02 Bottle serviced to 1700 PSI by Signature Flight Support RST Lubed flight control hinge points & rod end ball joints - LPS Serviced fuel strainer bowl & screen - No contamination found Serviced struts - Flushed, Serviced with Shell Fluid #4 (Mil-H-5606) & Nitrogen Serviced brake reservoir - Shell Fluid #4 Replaced Air Filter - Donaldson P-15-1936 (Replace Each 3 yrs, 5 Cleanings, or 500 hrs) Greased landing gear service points with Shell #22 - Lubed rod ends & non-greaseable joints with LPS Greased all wheel bearings - Shell #22 Checked shimmy damper action - found OK - no service needed Checked landing gear power pack hydraulic fluid level - found OK - no service needed Checked ELT per FAR 91 .207 - OK- Batteries due September 2020 Checked Airworthiness Directives through 2018-05 on airframe - none due AD 2017-14-04 Oil cooler hoses is NA. Hoses are Type D, no further action is required. Ldgn Gear Operational Check, Emergency Ext & Anti Retract systems, Lights, Throttle Horn, Doors - OK Aircraft Operational Checks - OK

~ -:r::-~ ~ I CERTIFY THAT THIS AIRCRAFT HAS BEEN INSPECTED JAW AN .. ANNUAL INSPECTION AND WAS DETERMINED TO BE IN AN AIRWORTHY CONDITION ISAAC DETERS A&P 2714038 IA

YEAR 20_ DATE

MAKE.~ MOOEL:l't.-S2R..S01T SIN. S2S7Q2t REG NO: N!l1 aAS WOAK OllllER: ~7-2018

Alrfnlme Entries

Bartelt Aviation, Inc.

13Cl1WMl~SIUlgll. Ml 4'0t1 --1-5431

DA TE: en1201 a AIC TSN: 1703.5 H011BS: 1703.S

Installed new high pressure line pin A285T168B8851 (Aviall Hose Shop Manufactured, see WO 1004288715) from the AJC compressor to the firewall. Utillzed new heat shield material to protect the line adjacent to lhe exhaust Setvlced the AJC Compressor oll to required level. Serviced the system with R134 coolant to 2 lbs, 2 oz's. Pelformed machine leak check and a sec:oodary leak check by visual bUbble check method. No leaks noted. Peiformed operational check. Alr-Conditioning system blows cold .... Installed a seMoeable El T Antenna pin 110-324 .... Torqued Stabilator Pivot Bearing botts.

Meintenwice RelttaSe

The einnll erd/ar ODIT1l)OfW'tl(a) on N918AS- repend 8l>d inspeded In~ with CUTW1I FAR• rules al the Federal Avlebon RagUlatlons 8l>d - IOt.lld PJrwontrf for r9ll.m a.vial. Pertinenl delalts ,..,_.. we on ftle unclW Work Order No BA~7-2018, Oated817/2018

DATE· 817/2018

t.W<E: Piper MODEL= f>A..32R-301T SIN: 3257029 REG. NO: N918AS WORK ORDER: BMlOS41-48-2018

Airframe Entries

SIGNED.

l<8ny All

~ Bartelt Aviation, Inc. 1301 WMI ~le 51191 Sturgis. Ml 49091 Phone: 269-651-5431

Order: BA-00538-07 -2018

•s and Alterations ertilicate Number of •ther specific entries.)

DATE: 8113/2018 /IJC TSH: 1704.5 HOB8S. 170'.5

R~ ~led AC Com_pn!SSOf' High Pressure Hose Assembly PIN A285T16888851. Hose returned back to Aviall Hose Shop for repai_rs. Reinstalled repaired Hose Assembly PIN A285T15888851 suppl"lfld by Aviall Hose Shop. Serviced AC Comiw-. ~ 2tgoodbs, 20Z. d R-134 coolant. Leak checked att8Ch fittings with no leaks noted. Engine run up and operational ctieck of ...,.,.,ng IS •

DATE: 8113/2018 SIGNED: Work Order. BA-00541-08-2018

KonyAllanH Printed by EBis 3 (datcomedia.oom)

YEAR 20 _ _

DATE

RECORDING YACH TIME

TODAY'S FLIGHT

TOTAL TIMEIN SERVICE

Description of Inspections, Tests, Repairs and Alterations Entries must be endorsed with Name, Rating and Certificate Number of Technician or Repair Facility. (See back pages for other specific entries.)

AVJET AVIONICS 253 Warbird L:ine Driggs, ID 83422

'.W8-354-3 I 87 - FAA C.R.S. 186R021 Y Nlll~As s. _32.~?o'J.q

3 - I --z.o-i. 1

I certify that the altimeter and static systcm tc-;ts requirt-d by 14 CFR part 91.411 and transponder tests, including dala corrcspondcncc, required by pa11 91 .413, have been pcrfonned and found to comply with 14 CFR pmt 43, nppcndix E and F.

4L1" l)l'\ . .wJ<"~:3~PD3 .s...i IOLir~ AltimclerModcl: Un.f!J ~<UyP0-3 Scr~al o. :$'1'?S/$'

Transponder Model: ~ KT J" '--- Senal No. --"3...,<>~1 o ___ _ EncoderModel: f\k.. rt:o AR,-S'SO ScrialNo. 1l:iS1D

Thi!" altimeter was tested to 2.o, ooo foct on 2 - (:, Z.c: 1C\ Encoder data correspondence was tl'Sted to '2v OtJu feet on Z-G ·2..0( 6\

The transponder was tested on 2. - (, - 2 O 1 "'1

Static system leak l~tcd on ~i~-~~~-=2.==0~1 r.~,~~~;:;;::::=::::~~ s~.------~ ~ ) ~ - - ,,ir.'\vjctAvmnrcs,C K.!>. roo~ ---~

ftfl-

YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests~ Repairs ~~d Alterations 20 __ TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Cert1f1cate ~.umbe~ of

DATE

-

-

-

TIME SERVICE Technician or Repair Facility. (See back pages for other specrfrc entries.)

,_,.~ ' A vjet Avionics Date- 2/22/2019 253 Warbird Lane Make-Piper N918AS

p. ·~ - Driggs, ID 83422 Model-PA32R-301 T ;::Qi ···~ - ~ 208-354-3 I 87 Hobbs-I 752.7

Removed and Overhauled King Horizon Gyro Flight Director Kl-256 PN 060-0017-00 sn 24220 with Berkshire Instrument work order #43643 dated 12 Feb, 2019. Reinstalled unit in aircraft. Ground test was performed. System test ok. AJso repaired Alternator Inop light by rewiring light input to unused spare light on light assembly. System check ok.

Updated King KLN-94 from system software 0104 to latest available software ver. 0106 to allow latest Nav Database upgrade. Nav Data was updated to latest cycle.

All equipment installed as per manufacturer's individual installation manuals and tested as per manufacturer's o erational manuals.

I certify that the repairs/ins ectioas identi ormed in accordance with current Federal Aviation Regulation · for

SigJle~~~~~~~~~~~~ CRS I86R021 Y

--

--

YEAR RECORDING TODAY'S 20 __ TACH FLIGHT

DATE TIME

TOTAL Description of Inspections, Tests, Repairs and Alterations TIMEIN Entries must be endorsed with Name. Rating and Certificate Number of SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

A vjet Avionics 253 Warbird Lane Driggs, ID 83422 208-354-31 87

Date- 2/27/2019 Make-Piper N918AS Model-PA32R-301 T Hobbs-1752.7

Removed and replaced Lamar Allemator lnop Switch PN A-00258-2-PMA with like part number sn 80R67804 (which is located under front baggage floor area). Alternator light was not extinguishing in flight but after replacing switch system check tested good during ground run.

All equipment installed as per manufac · ividual installation manuals and tested as per manufacturer's o erational manuals. I certify that the repairs/inspection e ere performed in accordance with current Federal Aviation Regulation

Sig ~~~z~~~~~~==;?L--CRS 186R02 l Y

YEAR 20 _

DATE

RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIMEIN Entries must be endorsed with Name. Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

-- --Piper Model: PA-32R-310T SIN: 3257029 Total Time= Hour Meter Time= 1,763 hours

Lycoming TI0-540-AHlA SIN L-9909-61A Hour Meter Time= Total Time= 1,763 hours Time since overhaul= 266 hours

ELT (Artex Tl 10-4, Part No. 452-0130 Rev N, Serial Number 374915-019) was inspected and tested in accordance with 14 CFR91.207 (d) and found to meet the criteria. ELT battery is dated Sep 2020.

Added small amount of hydraulic fluid (5606) to landing gear pump reservoir. Air cleaner was very clean and was not serviced. Topped off brake reservoir. Gear retract accomplished - no discrepancies. Operational check found all system functioning properly.

I have inspected this aircraft in accordance with the scope and detail of 14CFR43 Appendix D for an annual inspection and in accordance with the Piper PA-32R-301/301T inspection schedule and find it airworthy.

Lewis HART •25 15247 A&P

/~ 2~ay20l9 I I I

--

YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations 20 __ TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of

DATE TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

I

AVJET AVIONICS XPD(( I £NloDf3/l.. 253 Warbird Lane - Driggs, ID 83422 bf.IL~ r

208-354-3 187 - FAA C.R.S. 186R02 Ir ;V f3f-- I D {) t; N 9J6AS SIN '5,;;szoz '8 Y 2 . z

I certify lhat the altimeter and slatic system tests required by 14 CFR part 91.41 1 and I f · transponder tests, including data correspondence, required by part 91.413, have been pcrfonned and found to comply with 14 CFR part 43, appendix E and F. r

I Altimeter Model: - Serial No.

Transponder Model: ¥.~ irz.N't.g Serial No. .,[~J ~IS. '(L.,~ I Encoder Model: ~ · Serial No. J I 6

The altimeter was tested to feet on Encoder data correspondence was tested to al tjt!'O CJ feet on LL~·J7

The transponder was tested on // • £:::. .;9 Static sz_lrtc_:ed ~ I I~ · 19 Signatu :::::-~ ~ ·

< ~r Avjet Avionics, C.R.S. 186R021Y . r

I

YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations 20 _ TACH FUGHT TIME IN Entries must be endorsed with Name. Rating and Certificate Number of


Avjet Avionjcs 253 W arbird Lane Driggs, ID 83422 208-354-3187

Date-1 1/06/2019 N9 l 8AS Make- Piper Model- PA32R-301T Hobbs-1812.1

Removed Bendix King KT-76C Transponder PN 066-01156-0101 sn3010, Bendix King KLN 94 GPS PN 069-0 1034-0 IOI sn2518, Bendix King KA-92 GPS Antenna PN 071-01553-0200 snl6862, including associated trays and harnesses.

Removed Skywatch TRC-497 TAS PN 805-10800-001 sn85179, without tray and connectors. Installed Stratus Power PN 153010-000029 sn066096 on pilot s ide front panel, including K.Hxon breaker. Installed Garmin GNX-375 GPS/XPDR PN 011-04378-00 sn5GJ001854, GA-35 GPS/WAAS Antenna

PN 13-00235-00sn165101, including associated trays, wiring, coax, and Klixon breaker. GNX-375 system was interconnected to Garmin GMX 200 for traffic and Bendix King KFC 150 autopilot via Kl 525 HSI.

GNX-375 system was installed as per Garmin STC Number SA02636SE dated March 22, 2019 and IA W installation manual 190-02207-A4 Rev 4 dated July 2019 and GS installation manual 190-01112-10 Rev 20 dated August 2019. FAA Fonn 337 was completed and filed with the FAA. Aircraft flight manual supplement was placed into aircraft records. All associated wiring notes are on record at this repair station. Part 91 XPDR/Encoder certification com lete see attac · . · craft wei ht and balance records have been u dated 11 /05/2019. I certify that the repairs/i were perfonned in accordance with current Federal Aviation Regulation1_§s~~~~~~~ Si

CRS l86R021 Y

YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations 20_ TACH FLIGHT TIMEIN Entries must be endorsed with Name, Rating and Certificate Number of


A vjet Avionics 253 Warbird Lane Driggs, ID 83422 208-354-3187

Date- 11/06/2019 Make-Piper N918AS Model-PA32R-301T Hobbs-1812.21

Removed and Repaired (warranty) King Horizon Gyro Flight Director KI-256 PN 060-00 17-00 sn 24220 with Berkshire Instrument work order #44019 dated 2 I Oct, 2019. Reinstalled unit in aircraft. Ground test was performed. System test ok.

All equipment installed as per manu ' individual installation manuaJs and tested as per manufacturer's o erational ma

1 certify that the repairs/ ins :e-perfoffiled in accordance with current Federal Aviation Regulations~~~~~~~~~ro

Sign~~2:!~~~~S:~~.---:--:~~-CRS 186R02 l Y

YEAR RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations 20_ TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of


Avjet Avionics 253 Warbird Lane Driggs, ID 83422 208-354-3187

Date- 04/09/2020 N9 l 8AS Make-PIPER Model- PA-32R-30IT

Removed faulty Narco AR-850Encodersn16810 and installed replacement Narco AR-850 Encoder sn35788. Checked system as per Part 91.41 I and found to comply with 14 CFR Part 43, appendix E and F.

Removed and Replaced Autopi lot Disconnect Switch on Pilot' s Yoke PN MS25089-3AR. System tested good and returned to service.

CRS 186R021Y

YEAR 20_ DATE

RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

Piper Model: PA-32R-310T SIN: 3257029 Total Time= Hour Meter Time= 1,763 hours

Lycoming TI0-540-AHlA SIN L-9909-61A Hour Meter Time= Total Time= 1,763 hours Time since overhaul = 266 hours

ELT (Artex Tl 10-4, Part No. 452-0130 Rev N, Serial Number 374915-019) was inspe<:ted and tested in accordance with 14 CFR91.207 (d) and found to meet the criteria. ELT battery is dated Sep 2020.

Added small amount of hydraulic fluid (5606) to landing gear pump reservoir. Air cleaner was very clean and was not serviced. Topped off brake reservoir. Repacked all wheel bearings. Gear retract accomplished - no discrepancies. Operational check found all system functioning properly.

I have inspected this aircraft in accordance with the Piper PA-32R-301/301T inspection schedule and the scope and detail of 14CFR43 Appendix. D for an annual inspection and find it in airworthy condition.

Lewis HART 251524 7 A&P

Likf~ 2 1May2019

----;

YEAR 20 _ DATE

RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations TACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

Piper Model: PA-32R-310T S/N: 3257029 Total Time= Hour Meter Time= 1,831 hours

Lycoming TI0-540-AHlA S/N L-9909-61A Hour Meter Time= Total Time = 1,831 hours Time since overhaul = 334 hours

ELT (Artex Tl 10-4, Part No. 452-0130 Rev N, Serial Number 374915-019) was inspected and tested in accordance with 14 CFR9l .207 (d) and found to meet the criteria. ELT battery is dated Sep 2020.

Replaced all brake linings (Cleveland 66-62). Retract check was satisfactory including lights and horn. Landing gear hydraulic reservoir was full. Brake reservoir was fuU. Lubed landing gear (Aeroshell 22).

I have inspected this aircraft in accordance with the Piper PA-32R-30l /30 1T inspection schedule and the scope and detail of J4CFR43 Appendix D for an annual inspection and find it in airworthy condition.

Lewis HART 2515247 A&P

6 A/-zol"'tt t_

,,,----

--

YEAR 20_

DATE

RECORDING TODAY'S TOTAL Description of Inspections, Tests, Repairs and Alterations YACH FLIGHT TIME IN Entries must be endorsed with Name, Rating and Certificate Number of TIME SERVICE Technician or Repair Facility. (See back pages for other specific entries.)

Piper Model: PA-32R-310T S/N: 3257029 Total Time = Hour Meter Time = 1,889 hours

Installed new battery ( 452-0130 Rev R) in EL T (Artex EL T 110-4). ELT was inspected and tested in accordance with 14 CFR91.207 (d) and found to be satisfactory. Battery is dated April 2023.

Replaced tires and tubes on both main gear. Balance was checked and found excellent. Tires are Goodyear Flight Custom ill, 8 ply and tubes are Goodyear Butyl Rubber

Removed Oildyne hydraulic pump 636029, serial number 108BI1 I 9SP-AL-l-VT and installed repaired (Power Packs Plus) hydraulic pump 38998-007 (Piper part number) serial number 122.

Lewis HART 2515247 A&P

i-~ 16 December 2020

Documents

Aircraft Record General Information