# New Piper PA-32R-301T

- Type: Aircraft model (FAA registry)
- Registry code: 7104308
- Manufacturer (registry): NEW PIPER AIRCRAFT INC
- Model: PA-32R-301T
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 7
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A3SO](https://openairdocs.org/tcds/A3SO) (OpenAirDocs)
- Holder: Piper Aircraft Inc.
- Registered aircraft: 18
- Page: https://openairdocs.org/model/new-piper-pa-32r-301t

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2024-14-03](https://openairdocs.org/ad/2024-14-03): Autopilot System · Garmin GFC 500 Autopilot (STC SA01866WI). Effective Aug 20, 2024
- [AD 2023-09-09](https://openairdocs.org/ad/2023-09-09): Exhaust Turbine System (Recip) · Aerostar PA-60-600 (Aerostar 600), PA-60-601 (Aerostar 601), PA-60-601P (Aerostar 601P) and 292 more. Effective Jul 17, 2023
- [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022
- [AD 2017-14-04](https://openairdocs.org/ad/2017-14-04): Engine Oil · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Aug 15, 2017
- [AD 2013-02-13](https://openairdocs.org/ad/2013-02-13): Stabilizer Control System · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Mar 11, 2013
- [AD 2010-15-10](https://openairdocs.org/ad/2010-15-10): Control wheel shafts · Piper PA-28-140, PA-28-150, PA-28-151 and 33 more. Effective Aug 31, 2010
- [AD 2010-13-07](https://openairdocs.org/ad/2010-13-07): Engine Exhaust. · Piper PA-32R-301T and PA-46-350P. Effective Jul 28, 2010
- [AD 2009-05-05](https://openairdocs.org/ad/2009-05-05): Primary Flight Displays · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 3, 2009
- [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2004-14-12](https://openairdocs.org/ad/2004-14-12): Control wheel attaching hardware · Piper PA-28-161, PA-28-181, PA-28R-201 and 8 more. Effective Aug 10, 2004
- [AD 2001-23-17](https://openairdocs.org/ad/2001-23-17): GNS 430 units · Cessna 172, 182, 206 and 209 more. Effective Dec 28, 2001
- [AD 98-21-21 R1](https://openairdocs.org/ad/98-21-21-R1): Electric Inflatable Door Seals · Cessna 17-30, 17-30A, 17-31 and 267 more. Effective May 1, 2000
- [AD 98-25-02](https://openairdocs.org/ad/98-25-02): Top-mounted Antenna · Bell Helicopter Textron Canada 407, 172, 172A and 243 more. Effective Dec 22, 1998
- [AD 98-14-03](https://openairdocs.org/ad/98-14-03): Transponders · Cessna 172, 172A, 172B and 230 more. Effective Aug 16, 1998
- [AD 96-10-03](https://openairdocs.org/ad/96-10-03): Flap Handle Attach Bolt · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jun 14, 1996
- [AD 93-05-10](https://openairdocs.org/ad/93-05-10): Nose Landing Gear · Piper PA-32R-300, PA-32R-301 (HP), PA-32R-301 (SP) and 3 more. Effective Apr 30, 1993
- [AD 87-08-08 R3](https://openairdocs.org/ad/87-08-08-R3): Lower spar cap · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective May 22, 1989
- [AD 86-17-01](https://openairdocs.org/ad/86-17-01): Ammeter Replacement · Piper PA-28-150, PA-28-160, PA-28-180 and 20 more. Effective Aug 21, 1986
- [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986
- [AD 81-24-07](https://openairdocs.org/ad/81-24-07): Nose Landing Gear Modification · Piper PA-32R-300, PA-32R-301 (SP), PA-32R-301T and 2 more. Effective Nov 20, 1981
- [AD 80-14-03](https://openairdocs.org/ad/80-14-03): Bendix, King or Narco Transmitters · Piper PA-28-161, PA-28-181, PA-28-201T and 16 more. Effective Jul 1, 1980
- [AD 79-26-05](https://openairdocs.org/ad/79-26-05): Oil and Fuel System Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 28 more. Effective Jan 3, 1980

Historical (superseded or no longer in force):

- [AD 2008-06-28 R1](https://openairdocs.org/ad/2008-06-28-R1) (historical): Primary Flight Displays (PFDs) · Avidyne Primary Flight Displays, 441, LC41-550FG and 22 more. Effective Apr 10, 2008
- [AD 2008-06-28](https://openairdocs.org/ad/2008-06-28) (historical): Primary flight display · Avidyne Primary Flight Display (S-TEC STC SA09543AC-D or 2 others). Effective Apr 10, 2008
- [AD 95-26-13](https://openairdocs.org/ad/95-26-13) (historical): Inspect Oil Cooler Hoses · Piper PA-28-140, PA-28-150, PA-28-151 and 22 more. Effective Feb 5, 1996

## Information bulletins (advisory) (15)

- [SAIB 2022-20](https://openairdocs.org/saib/2022-20): Wing Spar. Issued Oct 19, 2022
- [SAIB AIR-21-10](https://openairdocs.org/saib/AIR-21-10): Wing, Attach Fittings (JASC 5740). Issued Jun 29, 2021
- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [SAIB CE-11-12R1](https://openairdocs.org/saib/CE-11-12R1): Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Dec 2, 2015
- [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014
- [SAIB CE-11-42](https://openairdocs.org/saib/CE-11-42): Flight Controls: Control Cable/Pulley Inspections. Issued Jun 29, 2011
- [SAIB CE-11-14](https://openairdocs.org/saib/CE-11-14): Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-13](https://openairdocs.org/saib/CE-11-13): Wings - Piper PA-28, PA-32, PA-34 Forward Spar Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-12](https://openairdocs.org/saib/CE-11-12) (historical): PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach Fitting. Issued Jan 5, 2011
- [SAIB CE-11-11](https://openairdocs.org/saib/CE-11-11): Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting Corrosion. Issued Jan 5, 2011
- [SAIB CE-11-10](https://openairdocs.org/saib/CE-11-10): Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and Ribs. Issued Jan 5, 2011
- [SAIB CE-11-01](https://openairdocs.org/saib/CE-11-01): Stabilizers -Horizontal Stabilator   Turnbuckle. Issued Oct 4, 2010
- [SAIB CE-09-23](https://openairdocs.org/saib/CE-09-23): Fuel: Piper PA-28, PA-32, PA-34. Issued Apr 7, 2009
- [SAIB CE-09-12](https://openairdocs.org/saib/CE-09-12): Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 Installations. Issued Feb 11, 2009
- [SAIB CE-08-13](https://openairdocs.org/saib/CE-08-13): Electrical Power. Issued Feb 27, 2008

## Registered aircraft (18)

- [N1063C](https://openairdocs.org/aircraft/N1063C): [Jim Johnson Nissan Inc](https://openairdocs.org/faa-owner/JIM%20JOHNSON%20NISSAN%20INC), [Bowling Green, KY](https://openairdocs.org/faa-place/KY/Bowling%20Green), built 2006, S/N 3257440
- [N106L](https://openairdocs.org/aircraft/N106L): [Valiair Lc Trustee](https://openairdocs.org/faa-owner/VALIAIR%20LC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 2000, S/N 3257130
- [N213C](https://openairdocs.org/aircraft/N213C): [Levins Kenneth](https://openairdocs.org/faa-owner/LEVINS%20KENNETH), [Alameda, CA](https://openairdocs.org/faa-place/CA/Alameda), built 2006, S/N 3257436
- [N25CA](https://openairdocs.org/aircraft/N25CA): [White Dog Aviation LLC](https://openairdocs.org/faa-owner/WHITE%20DOG%20AVIATION%20LLC), [Portola Valley, CA](https://openairdocs.org/faa-place/CA/Portola%20Valley), built 2006, S/N 3257424
- [N28PZ](https://openairdocs.org/aircraft/N28PZ): [Asa Obion LLC](https://openairdocs.org/faa-owner/ASA%20OBION%20LLC), [Union City, TN](https://openairdocs.org/faa-place/TN/Union%20City), built 2006, S/N 3257418
- [N3120T](https://openairdocs.org/aircraft/N3120T): [Mcbride Matthew T](https://openairdocs.org/faa-owner/MCBRIDE%20MATTHEW%20T), [Eagle River, WI](https://openairdocs.org/faa-place/WI/Eagle%20River), built 2006, S/N 3257417
- [N3129B](https://openairdocs.org/aircraft/N3129B): [Raabe Craig A](https://openairdocs.org/faa-owner/RAABE%20CRAIG%20A), [West Hartford, CT](https://openairdocs.org/faa-place/CT/West%20Hartford), built 2006, S/N 3257415
- [N3140G](https://openairdocs.org/aircraft/N3140G): [Bynum Aviation LLC](https://openairdocs.org/faa-owner/BYNUM%20AVIATION%20LLC), [New Albany, MS](https://openairdocs.org/faa-place/MS/New%20Albany), S/N 3257433
- [N3143J](https://openairdocs.org/aircraft/N3143J): [Lyden Air LLC](https://openairdocs.org/faa-owner/LYDEN%20AIR%20LLC), [Walbridge, OH](https://openairdocs.org/faa-place/OH/Walbridge), built 2006, S/N 3257427
- [N3151H](https://openairdocs.org/aircraft/N3151H): [D S R D Investments LLC](https://openairdocs.org/faa-owner/D%20S%20R%20D%20INVESTMENTS%20LLC), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 2006, S/N 3257428
- [N382HP](https://openairdocs.org/aircraft/N382HP): [382 Hp LLC](https://openairdocs.org/faa-owner/382%20HP%20LLC), [Pt Pleasant Beach, NJ](https://openairdocs.org/faa-place/NJ/Pt%20Pleasant%20Beach), built 2006, S/N 3257411
- [N432LL](https://openairdocs.org/aircraft/N432LL): [Buckingham Aero LLC](https://openairdocs.org/faa-owner/BUCKINGHAM%20AERO%20LLC), [Buckingham, VA](https://openairdocs.org/faa-place/VA/Buckingham), built 2006, S/N 3257432
- [N477HP](https://openairdocs.org/aircraft/N477HP): [Williams Kerry Brent](https://openairdocs.org/faa-owner/WILLIAMS%20KERRY%20BRENT), [Seminole, TX](https://openairdocs.org/faa-place/TX/Seminole), built 2006, S/N 3257429
- [N551TT](https://openairdocs.org/aircraft/N551TT): [Southern Aircraft Consultancy Inc Trustee](https://openairdocs.org/faa-owner/SOUTHERN%20AIRCRAFT%20CONSULTANCY%20INC%20TRUSTEE), [Casper, WY](https://openairdocs.org/faa-place/WY/Casper), built 1997, S/N 3257026
- [N579HF](https://openairdocs.org/aircraft/N579HF): [Northstar Voyager Corp](https://openairdocs.org/faa-owner/NORTHSTAR%20VOYAGER%20CORP), [Lewes, DE](https://openairdocs.org/faa-place/DE/Lewes), built 2006, S/N 3257408
- [N616AR](https://openairdocs.org/aircraft/N616AR): [Centurion Flyers LLC](https://openairdocs.org/faa-owner/CENTURION%20FLYERS%20LLC), [Spokane, WA](https://openairdocs.org/faa-place/WA/Spokane), built 2006, S/N 3257423
- [N826MA](https://openairdocs.org/aircraft/N826MA): [Brown Thomas W](https://openairdocs.org/faa-owner/BROWN%20THOMAS%20W), [San Luis Obispo, CA](https://openairdocs.org/faa-place/CA/San%20Luis%20Obispo), S/N 3257435
- [N834HP](https://openairdocs.org/aircraft/N834HP): [Newman Aviation Services Inc](https://openairdocs.org/faa-owner/NEWMAN%20AVIATION%20SERVICES%20INC), [Tiffin, OH](https://openairdocs.org/faa-place/OH/Tiffin), built 2006, S/N 3257426

## NTSB investigations (3)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA20FA026](https://openairdocs.org/ntsb/ERA20FA026), Nov 1, 2019: Piper PA32R (N181AG), Paducah, KY, destroyed, 1 fatal. Probable cause: The pilot’s failure to fully seat the fuel selector in the proper tank position during the descent for landing, which resulted in fuel starvation and a total loss of engine power.
- [NTSB CEN15LA077](https://openairdocs.org/ntsb/CEN15LA077), Dec 12, 2014: New Piper PA 32R-301T (N3127R), Springfield, MO, substantial damage. Probable cause: The pilot’s decision to descend below the recommended altitude during approach for landing in night visual meteorological conditions, and his failure to see and avoid a lighted tower, which resulted…
- [NTSB NYC07IA199](https://openairdocs.org/ntsb/NYC07IA199), Aug 15, 2007: Piper PA-32R-301T (N3120T), Alton, IL, incident, minor damage. Probable cause: The component manufacturer's inadequate fabrication of the transient voltage suppressor.

## FAA accident and incident reports (4)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20191031017419A](https://openairdocs.org/incident/20191031017419A), Oct 31, 2019: New Piper Aircraft Inc PA-32R-301T (N181AG), Paducah, KY, Destroyed, 1 fatal. Aircraft was destroyed during a forced landing, resulting from complete loss of engine power. During landing, the aircraft impacted a tree, removing the outer…
- [Accident 20141212023099A](https://openairdocs.org/incident/20141212023099A), Dec 12, 2014: Piper PA-32R-301T (N3127R), Springfield, MO, Destroyed. The pilot conducted the ILS-14 at ksgf, then proceeded VFR at 1,700 MSL enroute to 3DW and struck a cellular antenna. The pilot then shut off the fuel valve…
- [Incident 20080407832679I](https://openairdocs.org/incident/20080407832679I), Apr 7, 2008: Piper PA32R301T (N3129B), Shabbona, IL, No damage. (-23) On 04/07/2008 Piper N3129B was approximately 20 miles west of aurora airport in aurora, Illinois when the engine "coughed for about 4-5 seconds, then…
- [Accident 20070815018269A](https://openairdocs.org/incident/20070815018269A), Aug 15, 2007: Piper PA32R301T (N3120T), East Alton, IL, No damage. (-23) On August 15, 2007 a Piper PA-32R-301T N3120T enroute from aurora municipal airport (karr) to spirit of st. louis (ksus) the pilot noticed smoke coming…

## Service difficulty reports (88, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR J4YR202512084112](https://openairdocs.org/sdr/J4YR202512084112), Dec 8, 2025: CONTROL ARM. BROKEN. PILOT NOTICED THAT THE RUDDER TRIM SYSTEM WAS UNRESPONSIVE WHEN RUDDER TRIM ADJUSTMENT WAS MADE. UPON CLOSER EXAMINATION THE ARM THAT CONNECTS TO THE RUDDER TRI
- [SDR 2023FA0000794](https://openairdocs.org/sdr/2023FA0000794), Oct 21, 2023: INTAKE VALVE. BROKEN. ENGINE LOST POWER ON TAKEOFF ROLL AND TAKE OFF WAS SAFELY ABORTED. FOUND NO COMPRESSION ON CYLINDER #6 AND DETERMINED THE ENTIRE INTAKE VALVE WAS MISSING. FOUND
- [SDR NA3R202008110001](https://openairdocs.org/sdr/NA3R202008110001), Aug 7, 2020: CABLE. BROKEN. FOUND RIGHT SIDE AILERON BALANCE CABLE BROKEN WHERE IT GOES OVER THE PULLEY IN THE RIGHT WING ROOT, LEFT AND RIGHT AILERON BALANCE CABLES ARE REVERSED.
- [SDR 2019FA0000117](https://openairdocs.org/sdr/2019FA0000117), Apr 11, 2019: WARNING SYSTEM. FALSE ACTIVATION. PILOT REPORTED THE FACTORY OIL TEMPERATURE SYSTEM GAVE WARNING THAT OIL TEMP WAS HIGH WHILE IN CRUSE. PILOT LANDED AT NEAREST AIRPORT AND CHECK OIL LEVEL WHICH 
- [SDR 2018FA0000292](https://openairdocs.org/sdr/2018FA0000292), Jul 25, 2018: DRAG LINK. BROKEN. NOSE GEAR FAILED TO EXTEND PROPERLY DURING LANDING.
- [SDR 2018FA0000457](https://openairdocs.org/sdr/2018FA0000457), Jul 9, 2018: BOLT. BROKEN. THE BOTTOM HALF OF THE BROKEN BOLT FELL OUT OF THE NOSE GEAR RETRACT CYLINDER ATTACH POINT WHILE PULLING THE ACFT OUT OF THE HANGAR. THE TOP HALF REMAINED IN PL
- [SDR 2017FA0000144](https://openairdocs.org/sdr/2017FA0000144), Jan 14, 2017: PUMP. INOPERATIVE. PRE-FLIGHT RUN-UP DISCOVERED LACK OF TAKE OFF POWER AND ENGINE VIBRATION. THE AIRCRAFT FLIGHT WAS ABORTED AND THE AIRCRAFT RETURNED TO THE HANGER. THE ENGINE WA
- [SDR 2016FA0000090](https://openairdocs.org/sdr/2016FA0000090), Feb 11, 2016: OIL SYSTEM. OVERTEMP. ON CLIMBOUT TO 9000 FT OIL TEMP WENT TO 240 DEGREES F AT 7500 FT. REDUCED POWER TO 20MAP AND TEMP KEPT CLIMBING TO 270. MADE A PRECAUTIONARY LANDING. GROUND TEM
- [SDR 2015FA0000511](https://openairdocs.org/sdr/2015FA0000511), Oct 27, 2015: MAGNETO. OUT OF ADJUST. THE PILOT REPORTED THAT HIS ENGINE WAS HARD TO START AND GETTING WORSE. THE ENGINE TO MAGNETO TIMING WAS CHECKED AND REVEALED THE TIMING ON BOTH MAGNETOS WERE A
- [SDR 2015FA0000252](https://openairdocs.org/sdr/2015FA0000252), May 29, 2015: AILERON. CRACKED. PERFORMED SB 1216B DISCOVERED CRACK AT AILERON ATTACH POINT ON BOTH THE LT AND RT AILERON.
- [SDR 17GR2015FA0000251](https://openairdocs.org/sdr/17GR2015FA0000251), May 29, 2015: TRUNNION. CRACKED. PERFORMED SB1161, FOUND CRACKING IN RADIUS BOTH LT AND RT WING AT LANDING GEAR SIDE STRUT ATTACH POINT.
- [SDR CA150303007](https://openairdocs.org/sdr/CA150303007), Jan 17, 2015: SETSCREW. DAMAGED. (CAN) IN FLIGHT FAILURE OF ENGINE DURING CRUISE. ENGINE DISASSEMBLY AND ASSESSMENT FOUND INCORRECT PROPELLER GOVERNOR GEAR SHAFT SET SCREW P AND INCORRECT SAFTE
- [SDR CA140823001](https://openairdocs.org/sdr/CA140823001), Aug 23, 2014: COUPLING. CRACKED. (CAN) DURING INSPECTION, FOUND ENGINE EXHAUST TO TURBOCHARGER WASTEGATE VALVE V-BAND COUPLING, CRACKED.
- [SDR 2014FA0000274](https://openairdocs.org/sdr/2014FA0000274), Apr 14, 2014: BOLT. FAILED. DURING FLIGHT, PILOT HEARD A LOUD BANG FROM THE FRONT OF THE AIRCRAFT. NOSE GEAR DOWN LIGHT ILLUMINATED. WAS UNABLE TO RETRACT NOSE GEAR. ELECTED TO LAND. DURIN
- [SDR 2013FA0000737](https://openairdocs.org/sdr/2013FA0000737), Nov 15, 2013: BREAKER POINTS. LOOSE. THE RIVET THAT HOLDS THE OPENING CONTACT POINT TO THE MOVEABLE ARM HAS LOOSENED ALLOWING THE ARM TO MOVE BUT THE POINTS DO NOT BREAK CONTACT. THE MAGNETO THEN D
- [SDR 2013FA0000738](https://openairdocs.org/sdr/2013FA0000738), Oct 10, 2013: BREAKER POINTS. LOOSE. THE RIVET THAT HOLDS THE OPENING CONTACT POINT TO THE MOVABLE ARM HAS SOOSENED ALLOWING THE ARM TO MOVE BUT POINTS DO NOT BREAK CONTACT. THE MAG THEN DOES NOT D
- [SDR 2PMR2014022800108](https://openairdocs.org/sdr/2PMR2014022800108), Jul 11, 2013: SHAFT. WORN. AIRCRAFT LANDED WITH NO OIL PRESSURE AND FUSELAGE INCLUDING WINDSCREEN TOTALLY COVERED IN OIL. PILOT REPORTED THAT 10,000 FT MSL, THE ENGINE STARTED LEAKING OIL
- [SDR 2012FA0000299](https://openairdocs.org/sdr/2012FA0000299), Apr 19, 2012: IMPULSE COUPLING. LOOSE. DURING 500 HOUR INSPECTION OF MAGNETO SB 1-86B IMPULSE COUPLING INSPECTION. FOUND A LOOSE RIVET.
- [SDR 2012FA0000242](https://openairdocs.org/sdr/2012FA0000242), Apr 17, 2012: HOUSING. WRONG PART. FUEL PUMP WAS RECEIVED FOR A FUNCTIONAL TEST DUE TO POOR OPERATION BELOW 1400 RPM WITH THE BOOST PUMP TURNED ON. WHEN TESTED, THE FUEL PRESSURE WAS SET 10 PSI L
- [SDR 2011FA0000580](https://openairdocs.org/sdr/2011FA0000580), Aug 15, 2011: POWERPACK. FAILED. LANDING GEAR HYD POWER PACK FAILED ON FIRST FLIGHT AFTER INSTALLATION. POWER PACK WAS O/H REF WO 3505.
- [SDR 2011FA0000514](https://openairdocs.org/sdr/2011FA0000514), Aug 11, 2011: SHAFT. BROKEN. DISCONNECTING YOKE SHAFT WHERE IT ATTACHES TO THE U JOINT ASSY WHICH IS HELD BY 2 THROUGH BOLTS AT 90 DEGREES. IN THE PROCESS THE U JOINT BROKE OFF OF THE SHAFT
- [SDR 2011FA0000245](https://openairdocs.org/sdr/2011FA0000245), Mar 22, 2011: WIRE. BROKEN. DURING ROLLOUT RT MLG COLLAPSED. PILOT REPORTED THAT THE MAIN GEAR INDICATION WAS DOWN AND LOCKED. DURING RETRACTION CHECK AND INSP, (2) WIRES WERE FOUND BROKEN
- [SDR O7TR201103251](https://openairdocs.org/sdr/O7TR201103251), Mar 9, 2011: TURBINE WHEEL. SEPARATED. MAJOR TURBO FAILURE DUE TO SEPARATION OF FACTORY NEW TURBINE WHEEL HEAD FROM SHAFT.
- [SDR 2010FA0000597](https://openairdocs.org/sdr/2010FA0000597), Jun 8, 2010: MAGNETO. BURNED. PILOT REPORTED ROUGH RUNNING ENGINE. AFTER INSPECTION OF BOTH MAGNETOS, IT WAS FOUND THAT THE INTERNAL PARTS WERE BURNED AND DETERIORATED. THIS CONDITION WAS FO
- [SDR 2010FA0000596](https://openairdocs.org/sdr/2010FA0000596), Jun 8, 2010: MECHANISM. BURNED. PILOT REPORTED ROUGH RUNNING ENGINE. AFTER INSPECTION OF BOTH MAGNETOS, IT WAS FOUND THAT THE INTERNAL PARTS WERE BURNED AND DETERIORATED. THIS CONDITION WAS FO
- [SDR 2010FA0001105](https://openairdocs.org/sdr/2010FA0001105), Apr 18, 2010: LANDING GEAR. DISTORTED. DAMAGE OCCURRED TO NLG SUPPORT STRUCTURE DURING THE RETRACT CYCLE OF MLG AFTER TAKEOFF. FULL (OR CLOSE TO FULL) RUDDER CONTROL IMPUTED DURING THIS CYCLE. A LOUD
- [SDR 2009FA0000901](https://openairdocs.org/sdr/2009FA0000901), Aug 28, 2009: RIB. CRACKED. DURING AN ANNUAL INSP, THE INSPECTOR FOUND WHAT APPEARED TO BE A CRACK EXTENDING FWD OF THE OTBD AILERON HING ATTACH BRACKET, LT AILERON, IN THE AILERON L/E RIB
- [SDR 2009FA0000613](https://openairdocs.org/sdr/2009FA0000613), Jul 7, 2009: MOUNT. BROKEN. UPON REMOVAL OF THE ENGINE FOR OVERHAUL, DISCOVERED THAT THE NOSE GEAR DRAG LINK ATTACH POINT WAS BROKEN. DISCOVERED THAT THE LWR RT ENGINE MOUNT MOUNTING BOLT 
- [SDR 2009FA0000625](https://openairdocs.org/sdr/2009FA0000625), May 6, 2009: WIRE HARNESS. BROKEN. AFTER GEAR EXTENSION, LF MLG DOWN LIGHT FAILED TO LIGHT. PROBLEM FOUND IN WIRING HARNESS AT LF MLG DOWNLOCK SWITCH. WIRE INSIDE THE CASING AT THE WIRING HARNESS
- [SDR 2009FA0000324](https://openairdocs.org/sdr/2009FA0000324), Apr 14, 2009: ATTACH BRACKET. LOOSE. THE NOSE GEAR ACTUATOR AFT ATTACH BRACKET WAS SHIFTING DURING GEAR FUNCTION CHECK. DISCOVERED THE BRACKET ATTACH ANGLE RIVETS HAD SHEARED, CAUSING THE NOSE GEAR
- [SDR 2008FA0000549](https://openairdocs.org/sdr/2008FA0000549), Aug 4, 2008: DOUBLER. CRACKED. UPPER COMM/NAV ANTENNA DOUBLER AND SKIN CRACKED FROM FWD SEAM ALONG BOTH ANTENNA MOUNT NUTPLATE LINES. CRACKS ARE APPROX 6 INCHES LONG WITH ADDITIONAL CRACKING 
- [SDR 2008FA0000548](https://openairdocs.org/sdr/2008FA0000548), Aug 4, 2008: SKIN. CRACKED. UPPER COMM/NAV ANTENNA DOUBLER AND SKIN CRACKED FROM FWD SEAM ALONG BOTH ANTENNA MOUNT NUTPLATE LINES. CRACKS ARE APPROX 6 INCHES LONG WITH ADDITIONAL CRACKING 
- [SDR 2008FA0000049](https://openairdocs.org/sdr/2008FA0000049), Jan 11, 2008: WIRE. FAILED. MAIN GEAR DOWN LOCK SWITCH WIRES PULL TIGHT ON STRUT ON RETRACTION AND PULL WIRE STRANDS APART TO BREAKING POINT. SILICONE TYPE WIRE COATING TENDS TO HOLD WIRE 
- [SDR 2008FA0000047](https://openairdocs.org/sdr/2008FA0000047), Jan 9, 2008: WIRE. FAILED. MAIN GEAR DOWN LOCK SWITCH WIRES PULL TIGHT ON STRUT ON RETRACTION AND PULL WIRE STRANDS APART TO BREAKING POINT. SILICONE TYPE WIRE COATING TENDS TO HOLE WIRE 
- [SDR 2008FA0000050](https://openairdocs.org/sdr/2008FA0000050), Jan 4, 2008: WIRE. FAILED. MAIN GEAR DOWN LOCK SWITCH WIRES PULL TIGHT ON STRUT ON RETRACTION AND PULL WIRE STRANDS APART TO BREAKING POINT. SILICONE TYPE WIRE COATING TENDS TO HOLD WIRE 
- [SDR 2008FA0000048](https://openairdocs.org/sdr/2008FA0000048), Jan 4, 2008: WIRE. FAILED. MAIN GEAR DOWN LOCK SWITCH WIRES PULL TIGHT ON STRUT ON RETRACTION AND PULL WIRE STRANDS APART TO BREAKING POINT. SILICONE TYPE WIRE COATING TENDS TO HOLD WIRE 
- [SDR 2008FA0000046](https://openairdocs.org/sdr/2008FA0000046), Jan 4, 2008: WIRE. FAILED. MAIN GEAR DOWN LOCK SWITCH WIRES PULL TIGHT ON STRUT ON RETRACTION AND PULL WIRE STRANDS APART TO BREAKING POINT. SILICONE TYPE WIRE COATING TENDS TO HOLD WIRE 
- [SDR 2007FA0000933](https://openairdocs.org/sdr/2007FA0000933), Oct 19, 2007: SHUNT. BLOWN. COMPLETE ELECTRICAL FAILURE. WHEN BATTERY MASTER SWITCH WAS TURNED ON, NO POWER REACHED MAIN BUSS. FOUND BATTERY AMMETER SHUNT BURNED THROUGH. BATTERY AMMETER S
- [SDR 2007FA0000873](https://openairdocs.org/sdr/2007FA0000873), Aug 27, 2007: MAGNETO. DAMAGED. THIS AIRCRAFT HAD A SET OF MAGS INSTALLED AT APPROXIMATELY 400 HRS TT, AT 596 HRS TT, INSTALLED ANOTHER O/H MAG ON THE LT, DUE TO AN OVERHEAT SITUATION. IT APPE
- [SDR 2006FA0000965](https://openairdocs.org/sdr/2006FA0000965), Sep 2, 2006: PRESSURE SWITCH. FAILED. AT AN ANNUAL INSPECTION IT WAS NOTED THE MAIN GEAR FAILED TO CYCLE COMPLETELY BEFORE PUMP SHUT OFF. PUMP CYCLED ON AND OFF UNTIL MAINS WERE FULLY RETRACTED. PUM
- [SDR 4437811](https://openairdocs.org/sdr/4437811), Apr 18, 2006: AIR FILTER. DEBONDED. PN P560007-3, GASKET HAD SEPERATED FROM FILTER ON ONE SIDE AND WAS PULLED INTO THE AIR STREAM ON THE ENGINE SIDE OF THE FILTER. INSTALLED NEW FILTER.
- [SDR 2006FA0000407](https://openairdocs.org/sdr/2006FA0000407), Apr 14, 2006: HOSE. DETERIORATED. PARTIAL POWER LOSS, TWO CYLINDERS DROPPED OUT, CAUSED BY SMALL PARTICLES OF RUBBER HOSE FROM UPPER DECK AIR REFERENCE LINES FLAKING OFF AND OCCLUDING THE FUEL I
- [SDR ECW2006F00000](https://openairdocs.org/sdr/ECW2006F00000), Feb 3, 2006: POWERPACK. DEFECTIVE. NEW HYD LANDING GEAR POWER PACK WILL NOT EXTEND LANDING GEAR. ANOTHER NEW POWER PACK WAS ORDERED AND INSTALLED. LANDING GEAR WOULD NOT FULLY EXTEND. ONE OF THE 
- [SDR 2005FA0000459](https://openairdocs.org/sdr/2005FA0000459), Mar 21, 2005: MAGNETO. INOPERATIVE. AIRCRAFT ARRIVED AT HANGAR WITH ROUGH RUNNING ENGINE. FOUND DUEL MAG DEAD AND ON SIDE. REMOVED MAG FROM ENGINE. FOUND TEETH MISSING ON MAG GEAR. WAS TOLD BY OWN
- [SDR 2004FA0000881](https://openairdocs.org/sdr/2004FA0000881), Aug 5, 2004: DRIVE ASSY. LEAKING. PILOT REPORTED OIL LEAKING FROM ENGINE. THE DRIVE ASSEMBLY FOR THE TURBO SCAVENGE PUMP WAS FOUND LEAKING. THE PUMP WAS REMOVED FROM THE ENGINE, REPAIRED AND REI
- [SDR 2004FA0000691](https://openairdocs.org/sdr/2004FA0000691), Jun 11, 2004: RIB. CRACKED. A/C IS IN ANNUAL FOR USA CERT. DURING INSPECTION FOUND STAB LT OUTTER RIB CRACKING AT BALANCE WEIGHT ATTACHMENT POINTS. RIB HAS 3 CRACKS WORKING AFT FROM FORWAR
- [SDR T0438](https://openairdocs.org/sdr/T0438), May 4, 2004: DATA PLATE. DEPARTED. ENGINE DATA PLATE RIVETS ARE BECOMING LOOSE CAUSING THE DATA PLATE TO SEPARATE FROM ENGINE. WE ARE SEEING THIS ON SEVERAL ENGINES.
- [SDR 2003FA0001110](https://openairdocs.org/sdr/2003FA0001110), Oct 3, 2003: BOLT. MISSING. THE HARDWARE ATTACHING THE TURBOCHARGER SCAVANGE SUMP TO THE TURBOCHARGER BECAME LOOSE ALLOWING LARGE QUANITY OF OIL TO LEAK FROM THE ENGINE OIL SYSTEM. ONE BOL
- [SDR 2003FA0001143](https://openairdocs.org/sdr/2003FA0001143), Sep 9, 2003: TRUNNION. CRACKED. DURING AN ANNUAL INSPECTION THE NOSE TRUNION WAS FOUND TO HAVE A CRACK APPROXIMATELY ONE INCH IN LENGTH ON THE AFT SIDE. GREASE WAS SEEPING FROM THE CRACK WHICH
- [SDR AUS20030721](https://openairdocs.org/sdr/AUS20030721), Jul 19, 2003: CONNECTING ROD. CRACKED. (AUS) CONNECTING ROD CONTAINED A CRACK INDICATION ADJACENT TO THE LITTLE END. LENGTH OF CRACK APPROXIMATELY 6.35MM (0.25IN). CAP ON ANOTHER CONNECTING ROD CONTA

All 88: https://openairdocs.org/model/new-piper-pa-32r-301t/reports.md

## STCs that may be installed (OpenAirDocs) (262, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc
- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA02279AT](https://openairdocs.org/stc/SA02279AT): Installation of a Boom Beam bulb, starter, and ballast. Whelen Aerospace Technologies
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA01147WI](https://openairdocs.org/stc/SA01147WI): Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Concorde Battery Corporation
- [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA04075CH](https://openairdocs.org/stc/SA04075CH): Installation of Dynon EFIS-D10A EAA sales kit part number 102778-000. Dynon Avionics Inc
- [STC SA01005DE](https://openairdocs.org/stc/SA01005DE): Installation of a EarthX ETX900-TSO Lithium battery. EarthX Inc
- [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc
- [STC SA01120SE](https://openairdocs.org/stc/SA01120SE): Installation of Door Steward. Mountain View Aviation LLC
- [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA02532AT](https://openairdocs.org/stc/SA02532AT): Installation of subject Michelin tires on appropriate aircraft. For Michelin 5, 6, 8, and 10-inch rim diameter tires on General Aviation Aircraft. Michelin North America Inc
- [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc
- [STC SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA04400NY](https://openairdocs.org/stc/SA04400NY): Installation of the Integrated Back-up Battery System (IBBS). TCW Technologies LLC
- [STC SA01435LA](https://openairdocs.org/stc/SA01435LA): Installation of engines modified with Firewall Forward Technologies LLC modified camshaft. Centri-Lube Technologies LLC
- [STC SA04192NY](https://openairdocs.org/stc/SA04192NY): KFD 900 Primary Flight Display System Additional Functions. Honeywell International Inc
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA01038AT](https://openairdocs.org/stc/SA01038AT): Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28, -28R, -32, -32R, -34 series MODELS WITH CONSTANT-CHORD WINGS). Whelen Aerospace Technologies. Lists PA-32 Series
- [STC SA3254SO](https://openairdocs.org/stc/SA3254SO): Installation of main landing gear fairings. Whelen Aerospace Technologies
- [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp
- [STC SA00954WI](https://openairdocs.org/stc/SA00954WI): Installation of Concorde RG Series Batteries in Piper Single Engine Airplanes. Aero-Mach Wilco LLC
- [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC SA01675AT](https://openairdocs.org/stc/SA01675AT): Installation of composite wingtips with recognition lights under a lens. Whelen Aerospace Technologies
- [STC SA00029AT](https://openairdocs.org/stc/SA00029AT): Installation of 'Speed Splitter' flap bracket fairings. Whelen Aerospace Technologies. Lists PA-32 Series
- [STC SA00059AT](https://openairdocs.org/stc/SA00059AT): Installation of flap gap seals. Whelen Aerospace Technologies. Lists PA-32 Series
- [STC SA04231CH](https://openairdocs.org/stc/SA04231CH): Installation and activation of a TruTrak Vizion autopilot system. Honeywell International Inc
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [STC SA01875WI](https://openairdocs.org/stc/SA01875WI): BasicMed 6-Place Occupancy Restriction. Aeronautix LLC
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc
- [STC SA09902AC](https://openairdocs.org/stc/SA09902AC): Installation of BendixKing KFD 900 Flight Display System. Honeywell International Inc. (Bendix King)
- [STC SA11174SC PAGE 2](https://openairdocs.org/stc/SA11174SC%20PAGE%202): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King)
- [STC SA02265SE](https://openairdocs.org/stc/SA02265SE): Installation of a camera housing. Airborne Sensor LLC
- [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc
- [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation
- [STC SA02384CH](https://openairdocs.org/stc/SA02384CH): Installation of Flight Boss LTD SPA-32/34 Series Organizers. Flight Boss Ltd
- [STC SA04181NY](https://openairdocs.org/stc/SA04181NY): Installation of the KFC 230 Aerocruze Automatic Flight Control System. Honeywell International Inc
- [STC SA04182NY](https://openairdocs.org/stc/SA04182NY): Installation of BendixKing KA 310 Autopilot Adapter. Honeywell International Inc
- [STC SA02426AK](https://openairdocs.org/stc/SA02426AK): Approval of the FreeFlight FDL-978-TX ADS-B system installed. FreeFlight Systems
- [STC SA1310SW](https://openairdocs.org/stc/SA1310SW): Installation of stretcher in lieu of rear seats. Aviation Fabricators Inc
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation

All 262: https://openairdocs.org/model/new-piper-pa-32r-301t/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [MC67184-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183977842120260722151904.0001): Axle. Airforms LLC · PMA PQ2644CE · Replaces 67184-000 · May 6, 2026
- [SSV35-231765-1M](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142043761020260713144519.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 452-334, 452-357, M34-14, M34-14M · May 4, 2026
- [SSV35-231765-1F](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132699716920260713144519.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 131765-1F, 452-335, F34-14, F34-14… · May 4, 2026
- [SSV35-231765-L1F](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104549240720260713144520.0001): ROD END BEARING. McFarlane Aviation Inc. · PMA PQ3732CE · Replaces 452-336, FL34-14 · May 4, 2026
- [AFC301002-0103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172761002820260612142644.0001): Motor, Actuator. Airforms LLC · PMA PQ2644CE · Replaces 761-519761 519 · May 1, 2026
- [AFC301002-0103](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159550390120260612142643.0001): Motor, Actuator. Airforms LLC · PMA PQ2644CE · Replaces C145-200 · May 1, 2026
- [60-79445-80A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178118516920251125152237.0001): Rear Bulkhead Door. Texas Aeroplastics · PMA PQ03888SW · Replaces 79445-00,79445-000 · Nov 20, 2025
- [MDL TD 031851](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184021792220250508133546.0001): VA-1A( )AndAccessories. Electronics International Inc · PMA PQ0088NM · Modification part · Apr 10, 2025
- [MDL RR1-2-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188380771120250311133057.0001): Alternate Avionic SupportStrut Assemblies. Radiorax Aviation Systems LLC · PMA PQ00040WB · Modification part · Jan 17, 2025
- [LSM-200-700-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187312814920250417183925.0001): Hub Cap Assy. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Dec 10, 2024
- [20010A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193704377820250303152540.0001): Air-Oil Cooler. Boyd Niagara LLC · PMA PQ0872NE · Replaces 8535311 · Oct 30, 2024
- [MDL103216-000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186927414020240221143428.0001): SkyView HDX Instrumentation. Dynon Avionics, Inc. · PMA PQ05359NM · Modification part · Jan 26, 2024
- [TAU03323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194359759020240221143039.0001): AV/Cabin Heat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Dec 14, 2023
- [FS2-20](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187589568620250925194345.0001): Alternator. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces BC410-1 · Dec 6, 2023
- [10-50008-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197885936020231121213613.0001): SSUL-X Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50008-XFCCC · Nov 20, 2023
- [SG8916](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184210096520231121213704.0001): Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8916 · Nov 20, 2023
- [SG8995](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182943732920231121213647.0001): Flexible Overcarpet for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8995 · Nov 20, 2023
- [12-50003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174373804120231121213726.0001): Assembly: saf-Tglo® Exit (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50003 · Nov 20, 2023
- [10-50011-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169450321120231121213638.0001): SSUL-X11 Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50011-XFCCC · Nov 20, 2023
- [12-50007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162405995920231121213741.0001): Assembly: saf-Tglo® Supplemental Signage/Placard. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50007 · Nov 20, 2023
- [SG8996](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148229651320231121213656.0001): Flexible Overcarpet End Cap for SSUL with Tape. STG Aerospace, Inc. · PMA PQ00023CB · Replaces SG8996 · Nov 20, 2023
- [12-50009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143498653820231121213748.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50009 · Nov 20, 2023
- [12-50011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137095145120231121213755.0001): Assembly: saf-Tglo® Whiter Background EXIT Sign (USES). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50011 · Nov 20, 2023
- [10-50009-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131980607420231121213622.0001): SSUL-X Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50009-XFCCC · Nov 20, 2023
- [10-50010-XFCCC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127656014020231121213630.0001): SSUL-X11 Lateral Extension Track Assembly. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 10-50010-XFCCC · Nov 20, 2023
- [12-50005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID120858243120231121213733.0001): Assembly: saf-Tglo® Door Operation Sign. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50005 · Nov 20, 2023
- [12-50013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111712889720231121213802.0001): Assembly: saf-Tglo® Whiter Background Door Operation Signage. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50013 · Nov 20, 2023
- [12-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106138561720231121213720.0001): Assembly: saf-Tglo® Exit (Text). STG Aerospace, Inc. · PMA PQ00023CB · Replaces 12-50001 · Nov 20, 2023
- [30-50001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104107492420231121213712.0001): Scapa 5169 Filler. STG Aerospace, Inc. · PMA PQ00023CB · Replaces 30-50001 · Nov 20, 2023
- [A80564](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172675386920240730171257.0001): Pump. Aero Accessories LLC · PMA PQ1206CE · Replaces Griggs Aircraft Refinishing, LLC… · Oct 26, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [EA-26000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153703030520230105195523.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023
- [EA-26000-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106213955320230105195544.0001): EA-26000 Series EIS Back-up Battery System Panel. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Jan 3, 2023
- [8100-078](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199746210320240229155223.0001): 100 in-lb PMA Servo 12V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-078 · Nov 18, 2022
- [8100-065](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189478147320240229155225.0001): 60 in-lb. PMA Servo 24V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-065 · Nov 18, 2022
- [8100-064](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178963419020240229155224.0001): 60 in-lb. PMA Servo 12V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-064 · Nov 18, 2022
- [8000-174](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171620492620240229155221.0001): Vizion PMA 2 Inch. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-174 · Nov 18, 2022
- [8000-176](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160691672620240229155222.0001): Vizion PMA 3 Inch. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-176 · Nov 18, 2022
- [8100-079](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153716452420240229155223.0001): 100 in-lb. PMA Servo 24V. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8100-079 · Nov 18, 2022
- [8000-175](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151385150220240229155221.0001): VizionPMA Flat. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-175 · Nov 18, 2022
- [8200-146](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138369791020240229155220.0001): Piper PA32 Kit Parts. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8200-146 · Nov 18, 2022
- [8000-177](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132353197320240229155223.0001): PMA Link Sensor. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8000-177 · Nov 18, 2022
- [8225-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104685608220240229155225.0001): PA-28 / PA-32Wiring Harness Kit. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Replaces 8225-004 · Nov 18, 2022
- [8000356](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153658135320221130202600.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Harrison P/N:8535311Niagara20010A · Oct 21, 2022
- [ES-4003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166236091520220916174112.0001): Alternator Assembly. Hartzell Engine Technologies LLC · PMA PQ1383CE · Replaces Piper87415-5 · Aug 3, 2022
- [AAG5-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106659092420220811111804.0001): G5 Adapter Plate. Affordable Aviation LLC · PMA PQ05456NM · Replaces Garmin 115-02733-00 · Aug 2, 2022
- [OI7201](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132452596220230324134544.0001): Air Vent Assembly. Obvious Innovations LLC · PMA PQ00007CB · Replaces 65735-02, 65735-03, 65735-04… · Jun 24, 2022
- [01-0790906-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131226734520220706160203.0001): LED Landing Light. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · Jun 21, 2022
- [A764-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124553518720220901210306.0001): Elbow. Aerospace Welding Minneapolis, Inc. · PMA PQ2712CE · Replaces 764 501, EL025360-122 · May 18, 2022
- [8002945](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190972776320220615161414.0001): Engine Oil Cooler. Aero-Classics Heat Transfer Products Inc · PMA PQ2543NM · Replaces Piper Aircraft Inc.557-903Stewart… · Apr 29, 2022

All of them: https://openairdocs.org/model/new-piper-pa-32r-301t/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Piper PA-32R-301T](https://openairdocs.org/model/piper-pa-32r-301t): 502 registered aircraft, registry code 7103220
- [Piper PA-32R-301T](https://openairdocs.org/model/piper-pa-32r-301t): 34 registered aircraft, registry code 7103221

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