# New Piper PA-32R-301

- Type: Aircraft model (FAA registry)
- Registry code: 7104307
- Manufacturer (registry): NEW PIPER AIRCRAFT INC
- Model: PA-32R-301
- 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: 6
- Page: https://openairdocs.org/model/new-piper-pa-32r-301

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 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 99-05-09](https://openairdocs.org/ad/99-05-09): Induction Air Filter · Piper PA-23-235, PA-23-250, PA-23-250 (Navy UO-1) and 20 more. Effective Mar 19, 1999
- [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 (6)

- [N1030N](https://openairdocs.org/aircraft/N1030N): [Dcaw Aviation LLC](https://openairdocs.org/faa-owner/DCAW%20AVIATION%20LLC), [Advance, NC](https://openairdocs.org/faa-place/NC/Advance), built 2006, S/N 3246242
- [N239ST](https://openairdocs.org/aircraft/N239ST): [N239st LLC](https://openairdocs.org/faa-owner/N239ST%20LLC), [Peachtree City, GA](https://openairdocs.org/faa-place/GA/Peachtree%20City), built 2006, S/N 3246239
- [N241SE](https://openairdocs.org/aircraft/N241SE): [Carrie Chad Michael](https://openairdocs.org/faa-owner/CARRIE%20CHAD%20MICHAEL), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 2006, S/N 3246241
- [N31241](https://openairdocs.org/aircraft/N31241): [Hotel Charlie Aero LLC](https://openairdocs.org/faa-owner/HOTEL%20CHARLIE%20AERO%20LLC), [Marshville, NC](https://openairdocs.org/faa-place/NC/Marshville), built 2006, S/N 3246234
- [N643MA](https://openairdocs.org/aircraft/N643MA): [Pritchetts Point LLC](https://openairdocs.org/faa-owner/PRITCHETTS%20POINT%20LLC), [New Castle, IN](https://openairdocs.org/faa-place/IN/New%20Castle), built 2006, S/N 3246243
- [N727GR](https://openairdocs.org/aircraft/N727GR): [Parth Aviation LLC](https://openairdocs.org/faa-owner/PARTH%20AVIATION%20LLC), [Terre Haute, IN](https://openairdocs.org/faa-place/IN/Terre%20Haute), built 2006, S/N 3246238

## NTSB investigations (1)

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 NYC07FA083](https://openairdocs.org/ntsb/NYC07FA083), Mar 24, 2007: Piper PA-32R-301 (N324ST), Jacksonville, MD, destroyed, 3 fatal. Probable cause: The pilot's failure to maintain control of the airplane which was a result of spatial disorientation after takeoff into instrument conditions with an operationally degraded electronic primary flight…

## FAA accident and incident reports (2)

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.

- [Incident 20211104018929I](https://openairdocs.org/incident/20211104018929I), Nov 4, 2021: New Piper Aircraft Inc PA-32R-301 (N241SE), New Castle, DE, Minor damage. Upon level off pilot noticed gear was not up and locked and three green lights not displayed. Noticed landing gear control circuit breaker tripped. Selected…
- [Accident 20070324004519A](https://openairdocs.org/incident/20070324004519A), Mar 24, 2007: Piper PA32R301 (N324ST), Jacksonville, MD, Destroyed, 3 fatal. (-23) Aircraft took off from harford county airport in churchville (0W3). People in the area did not see the aircraft crash but heard the impact. Aircraft…

## Service difficulty reports (82, newest 50)

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

- [SDR 2026FA0000828](https://openairdocs.org/sdr/2026FA0000828), Oct 12, 2026: ARM. BROKEN. THIS PART CONNECTS THE RUDDER TRIM ACTUATOR TO THE RUDDER BAR ASSEMBLY. THE PART HAS TWO ARMS WELDED TO IT. ONE CONNECTS TO THE RIGHT RUDDER CABLE AND THE OTHER
- [SDR 2025FA0000207](https://openairdocs.org/sdr/2025FA0000207), Oct 17, 2024: INTAKE DUCT. INCORRECT. AIRCRAFT DEPARTED AIRPORT AND AFTER APPROXIMATELY 10 MINUTES INTO FLIGHT, AIRCRAFT HAD LEVELED OUT AT CRUISE ALTITUDE OF 7,000 FEET. AIRCRAFT EXPERIENCED A LOSS
- [SDR 2023FA0000840](https://openairdocs.org/sdr/2023FA0000840), Dec 10, 2023: LIMIT SWITCH. BROKEN. AIRCRAFT N2542W WAS COMING IN FOR LANDING AT KSUS ON 10 DECEMBER 2023. PIC SELECTED LANDING GEAR HANDLE TO EXTEND POSITION. RIGHT MAIN AND NOSE GEAR DOWN AND LO
- [SDR 2022FA0000290](https://openairdocs.org/sdr/2022FA0000290), Jun 13, 2022: NONE. BYPASSING. THIS AIRCRAFT MADE AN EMERGENCY LANDING AT FORT LAUDERDALE EXECUTIVE AIRPORT AFTER SEVERAL ATTEMPTS THE RIGHT MAIN WOULD NOT FREEFALL, THE AIRCRAFT WAS BROUGHT 
- [SDR 2022FA0000322](https://openairdocs.org/sdr/2022FA0000322), Jan 4, 2022: MAGNETO. FAULTY. ENGINE FAILED TO START WHEN HOT! NEW MAGNETO FAILED TO START MULTIPLE TIMES AND STRAINED PILOT! INSTALLED ANOTHER NEW MAGNETO AND ENGINE STARTED NORMALLY AND NO
- [SDR 2021F00275](https://openairdocs.org/sdr/2021F00275), Aug 17, 2021: MAGNETO. MALFUNCTIONED. WHILE IN CRUISE FLIGHT EXPERIENCED ABNORMAL ENGINE NOISES AND SURGES. SUSPECTED MAG ISSUE DUE TO JUST INSTALLED SUREFLY ELECTRONIC MAG. DECLARED AN EMERGENCY AN
- [SDR 17GR2019031901](https://openairdocs.org/sdr/17GR2019031901), Mar 18, 2019: STRUCTURE. CRACKED. CRACK IN WING ON LT AND RT SIDE OUTBOARD AFT WHEEL WELL BOX CORNER. ABOUT 3 INCHES RADIATING FORWARD AND OUTBOARD.
- [SDR 2013FA0000489](https://openairdocs.org/sdr/2013FA0000489), Aug 13, 2013: VALVE. BROKEN. OPERATOR WAS COMPLAINING OF HIGHER THAN NORMAL OIL TEMPERATURES. FOUND VERNATHERM VALVE TO HAVE BROKEN. THE NUT THAT HOLDS THE SEATING VALVE HAD BROKEN OFF THE 
- [SDR CA121114001](https://openairdocs.org/sdr/CA121114001), Nov 13, 2012: HINGE BRACKET. CORRODED. (CAN) DURING THE REMOVAL OF THE RT SIDE AILERON FOR PAINTING, THE AME DISCOVERED SEVERE CORROSION ON THE INSIDE HINGE. THE CORROSION REDUCES THE HINGE BRACKET T
- [SDR 2011FA0000085](https://openairdocs.org/sdr/2011FA0000085), Jan 26, 2011: STRUCTURE. CRACKED. WHILE PERFORMING MANDATORY SB 1216A OF AILERON RIB INSP, THE MECHANIC FOUND A CRACK ON THE RT OTBD L/E AT COUNTER WEIGHT ATTACH POINT.
- [SDR 2010FA0000583](https://openairdocs.org/sdr/2010FA0000583), May 14, 2010: BLADE. FAILED. ((ZY2R)) LOSS OF BLADE TIP IN-FLIGHT. IN FLIGHT, PILOT EXPERIENCED SUDDEN VIBRATION. AS HE WAS OVER AN AIRPORT, IMMEDATELY POWERED BACK AND LANDED THE ACFT APPR
- [SDR 2010FA0000032](https://openairdocs.org/sdr/2010FA0000032), Nov 26, 2009: MAGNETO. MISOVERHAULED. MAGNETO WAS O/H ALONG WITH ENTIRE ENG 150 HRS AGO, 5 YRS CALENDAR TIME. ON A SUCCESSFUL RUN UP, DEPARTING, ENG BEGAN RUNNING VERY ROUGH ABOUT 100 FT ABOVE RUNWA
- [SDR 2008FA0000618](https://openairdocs.org/sdr/2008FA0000618), Aug 19, 2008: TANK. LEAKING. THE ACFT OPERATOR DROPPED THE ACFT OFF WITH A COMPLAINT OF A FUEL LEAK IN THE LT WING. THERE WAS EXTERNAL STAINING AT THE IB AFT EDGE OF THE TANK ASSY WHERE IT 
- [SDR 2008FA0000409](https://openairdocs.org/sdr/2008FA0000409), Jun 7, 2008: ALTERNATOR. DAMAGED. 4 SCREWS THAT HOLD THE RECTIFIER PLATE INTO THE BACK CASE OF ALTERNATOR CAME LOOSE AND CONTACTED THE ROTOR, DESTROYED ALTERNATOR. (K)
- [SDR 2007FA0001103](https://openairdocs.org/sdr/2007FA0001103), Dec 20, 2007: BRACKET. CORRODED. AIR CONDITIONING CONDENSOR DOOR P/N 99271-000 FAILED IN FLIGHT WHILE DEPLOYED. THE SMALL EXTRUDED ANGLE BRACKET ON THE RT SIDE OF DOOR WHERE THE BEARING ASSY P/
- [SDR 2007FA0000997](https://openairdocs.org/sdr/2007FA0000997), Nov 5, 2007: BEARING. FAILED. WHILE IN FLIGHT THE NOSE GEAR RETRACT CYLINDER PISTON ROD END FAILED, CAUSING IMMEDIATE EXTENSION OF THE NOSE GEAR.
- [SDR 2005FA0000966](https://openairdocs.org/sdr/2005FA0000966), Jul 6, 2005: RIB. CRACKED. LEFT AILERON OUTBOARD HINGE HALF WAS CORRODED. AILERON WAS DISASSEMBLED TO REPLACE HINGE HALF. UPON REMOVING AN3 BOLTS AND HINGE HALF FROM NOSE RIB, THE LOWER B
- [SDR 2005FA0000620](https://openairdocs.org/sdr/2005FA0000620), Apr 13, 2005: GASKET. MISSING. ON INITIAL GROUND RUN, AFTER INSTALLING FACTORY REMFG, OIL WAS LEAKING FROM ACCY CASE UNDER FUEL PUMP. WHEN FUEL PUMP WAS REMOVED TO REPLACE GASKET, IT WAS FOUN
- [SDR KBUY5052](https://openairdocs.org/sdr/KBUY5052), Feb 16, 2005: SWITCH. OPEN. PILOT REPORTED UNSAFE NLG ON FINAL. CYCLED AND INDICATION WAS SAFE. JACKED AC, RAN GEAR THROUGH RIG AND OPS CK. FOUND NLG DOWN LIMIT SWITCH WOULD NOT ACTIVATE P
- [SDR AUS20040441](https://openairdocs.org/sdr/AUS20040441), May 21, 2004: TRUNNION. CRACKED. (AUS) RT MAIN LANDING GEAR TRUNNION CRACKED.
- [SDR 2004FA0000144](https://openairdocs.org/sdr/2004FA0000144), Jan 12, 2004: TRUNNION. CRACKED. NOSE TRUNNION FOUND CRACKED AT ASSIST SPRING ATTACH BOSS. THIS WAS A NEW MFG TRUNNION WITH 16 MONTH AND 71 HOURS IN SERVICE. THE CRACK OCCURRED AT A POINT THAT 
- [SDR 2003FA0001097](https://openairdocs.org/sdr/2003FA0001097), Oct 23, 2003: LAMP. BURNED OUT. THESE BULBS ARE BURNING OUT AT A RATE OF AT LEAST 50 FLIGHT HOURS AND SOMETIMES AS LOW AS 20 FLIGHT HOURS. THE PILOT IS NOT LEAVING ON ALL THE TIME BUT RATHER O
- [SDR 2003FA0000970](https://openairdocs.org/sdr/2003FA0000970), Sep 24, 2003: BOLT. BROKEN. WHILE PERFORMING A NON RELATED MAINTENANCE GROUND RUN, ON THE TAXI BACK TO THE HANGER A VIBRATION OCCURED FROM THE RT MAIN LANDING GEAR. AFTER SHUT DOWN AN INSP
- [SDR AUS20031172](https://openairdocs.org/sdr/AUS20031172), Jul 25, 2003: RIB. CRACKED. (AUS) WING RIB LOCATED AT WS 49.25 CRACKED.
- [SDR AUS20031171](https://openairdocs.org/sdr/AUS20031171), Jul 25, 2003: RIB. CRACKED. (AUS) WING RIB LOCATED AT WS 49.25 CRACKED.
- [SDR SMT2003F00001](https://openairdocs.org/sdr/SMT2003F00001), May 12, 2003: DRIVE BELT. FAILED. AIRCRAFT HAS BEEN SUBJECT TO NUMEROUS ALTERNATOR AND AIR CONDITIONING COMPRESSOR DRIVE V BELT FAILURES. SOME WITH LESS THAN 10 HOURS TIME IN SERVICE WITH FIRST 
- [SDR 2001FA0000606](https://openairdocs.org/sdr/2001FA0000606), Dec 5, 2001: MOUNT. CRACKED. ENGINE TRUSS WELD ASSEMBY FOUND CRACKED AT STEERING ARM ATTACH POINT.
- [SDR 2001FA0000605](https://openairdocs.org/sdr/2001FA0000605), Dec 5, 2001: MOUNT. CRACKED. ENGINE TRUSS WELD ASSY FOUND CRACKED AT STEERING ARM ATTACH POINT
- [SDR 2001FA0000101](https://openairdocs.org/sdr/2001FA0000101), Jun 28, 2001: MUFFLER. CRACKED. UPON REMOVAL OF HEATING SHROUDS FOR INSPECTION, FOUND SIGNIFICANT DISTORTION OF MUFFLER CAN. THE MUFFLER WAS CRACKED AT UPPER LEADING EDGE WELD.
- [SDR AUS20010725](https://openairdocs.org/sdr/AUS20010725), Jun 24, 2001: BOLT. FAILED. (AUS) CYLINDER HOLDDOWN BOLTS FAILED.
- [SDR 2001FA0000099](https://openairdocs.org/sdr/2001FA0000099), Jun 8, 2001: MUFFLER. CRACKED. UPON REMOVAL OF HEATING SHROUDS FOR INSPECTION, FOUND SIDNIFICANT DISTORTION OF MUFFLER WAS CRACKED AT UPPER LEADING EDGE WELD.
- [SDR FWRA2001002](https://openairdocs.org/sdr/FWRA2001002), Apr 28, 2001: SWITCH. WORN. THE CONTACTS INSIDE THE LANDING LIGHT SWITCH HOUSING WERE DIRTY AND WORN AND APPARENTLY CAUSED A HIGH RESISTANCE CONNECTION WHICH OVERHEATED AND BEGAN MELTING T
- [SDR 20000720SH031](https://openairdocs.org/sdr/20000720SH031), Jun 1, 2000: B-NUT. LOOSE. GEAR WOULD NOT EXTEND. CIRCUIT BREAKER TRIPPED. RE-SET, BUT NO HELP. GEAR FREE FALL FAILED TO LOCK ALL GEAR DOWN. RIGHT MAIN COLLAPSED UPON LANDING. FOUND B-NUT
- [SDR 20000622SH019](https://openairdocs.org/sdr/20000622SH019), May 13, 2000: ARM. BENT. DURING FLIGHT, THE STUDENT PILOT INADVERTENTLY SHUT THE FUEL OFF CAUSING AN EMERGENCY LANDING AND DAMAGE TO THE RIGHT WING. INVESTIGATION REVEALED THE FUEL SELE
- [SDR FWRA002](https://openairdocs.org/sdr/FWRA002), Apr 19, 2000: GEAR. DAMAGED. BROKEN DISTRIBUTOR GEAR TEETH ON RT HAND GEAR CAUSING INTERMITTENT RUNNING ON RIGHT MAGNETO. PART NUMBER ON GEAR 10-682016. (X)
- [SDR 20000426SH026](https://openairdocs.org/sdr/20000426SH026), Mar 24, 2000: TRUNNION. CRACKED. ON PRE-FLIGHT, PILOT NOTICED FLUID FROM MIDDLE OF STRUT. AFTER CLEANING, FLUID RE-APPEARED. AFTER INSP, FOUND STRUT HOUSING CRACKED BELOW AFT WEB ON STRUT HOUSI
- [SDR 20000417SH007](https://openairdocs.org/sdr/20000417SH007), Mar 2, 2000: STRUT. CRACKED. DURING AN ANNUAL INSPECTION, CRACKS WERE FOUND IN BOTH MLG STRUT ASSEMBLIES NEAR THE AXLE BOLT HOLES (BOTH TOP) NEAR BOLT HEADS. THE CRACKS ARE IN THE OUTSIDE W
- [SDR 2000ZZZX361](https://openairdocs.org/sdr/2000ZZZX361), Jan 17, 2000: CONTROL CABLE. BENT. NOSE GEAR FAILED TO EXTEND. FOUND THE ALTERNATE AIR CABLE (PIPER P/N 554051) NOT ROUTED CORRECTLY IN ENGINE COMPARTMENT AND TY WRAP BROKEN WHICH ALLOWED ALTERNA
- [SDR 99ZZZX3184](https://openairdocs.org/sdr/99ZZZX3184), Jul 1, 1999: BOLT. MISINSTALLED. NUT BOTTOMED OUT ON SHANK OF BOLT ALLOWING MOVEMENT IN THE VERTICAL FIN DURING FLIGHT. THE MOUNTING HOLES FOR THE VERTICAL FIN ATTACH BRACKET AND REAL BULKHEAD 
- [SDR AU990420](https://openairdocs.org/sdr/AU990420), Apr 6, 1999: TRUNNION. CRACKED. (AUS) LEFT AND RIGHT MAIN LANDING GEAR TRUNNION HOUSINGS P/N 67926-30 (LT) AND P/N 67926-31 (RT) BOTH CRACKED ON THE AFT SIDE AT THE LOWER END OF THE FILLET. FO
- [SDR 99ZZZX624](https://openairdocs.org/sdr/99ZZZX624), Jan 19, 1999: SHAFT. MISINSTALLED. ALTERNATOR SHAFT NOT FULLY INSTALLED INTO ARMATURE/ALTERNATOR BODY. KEYWAYS NOT MATCHING UP. SHAFT TOO LONG. UNIT WAS OVERHAULED BY AERO ELECTRIC INC. NV2ROYSL.
- [SDR 98ZZZX3877](https://openairdocs.org/sdr/98ZZZX3877), Sep 22, 1998: VALVE. FAILED. REF: PA-32R-300 PARTS INDEX 53 1K7. THE ABOVE AIRCRAFT, SINCE NEW, HAD AN INTERMITTENT PROBLEM OF THE FUEL NOT SHUTTING OFF COMPLETELY AFTER ACTUATING THE DRAIN
- [SDR AU981576](https://openairdocs.org/sdr/AU981576), Sep 14, 1998: REGULATOR. MISINSTALLED. (AUS) AUTOMOTIVE TYPE VOLTAGE REGULATOR (BOSCH) FITTED INSTEAD OF THE CORRECT UNIT. INSPECTION ALSO FOUND THAT THE OVERVOLTAGE CONTROL UNIT HAD BEEN REMOVED AND
- [SDR 98ZZZX4557](https://openairdocs.org/sdr/98ZZZX4557), Sep 10, 1998: BALANCE CABLE. BROKEN. DURING AN ANNUAL INSPECTION, DISCOVERED A FLAT SHINEY SPOT ON THE BOTTOM OF THE RIGHT AILERON BALANCE CABLE. THE LOCATION OF THE CABLE IN QUESTION IS IN THE RIG
- [SDR AU981305](https://openairdocs.org/sdr/AU981305), Aug 22, 1998: TRUNNION. FAILED. (AUS) NLG TRUNNION TO DRAG BRACE ATTACHMENT FAILED ALLOWING THE NLG TO REST AGAINST THE DRAG BRACE IN A PARTIALLY EXTENDED POSITION. THE NLG FAILED TO FULLY EXT
- [SDR AU981020](https://openairdocs.org/sdr/AU981020), Jul 20, 1998: INLET VALVE. BROKEN. (AUS) NR 6 CYLINDER INLET VALVE HEAD SEPARATED FROM THE VALVE STEM. CRANKCASE CRACKED AND SEVERE INTERNAL DAMAGE TO THE ENGINE. PART TC: 4,097.
- [SDR 98ZZZX2455](https://openairdocs.org/sdr/98ZZZX2455), Jul 16, 1998: BELT. FAILED. REF: AIR CONDITIONING INSTALLATION DRIVE BELT SERVICE HISTORY: BROKEN AND REPLACED AT 135.7 TT 4/4/96. BROKEN AND REPLACED AT 213.4 TT 7/16/96. BROKEN AND REPLA
- [SDR AU980777](https://openairdocs.org/sdr/AU980777), Jul 6, 1998: DOWNLOCK. CRACKED. (AUS) NOSE LANDING GEAR DOWNLOCK ASSEMBLY BROKEN AT BUSHING AT PIVOT POINT. SUSPECT CRACK HAD BEEN PRESENT FOR SOME TIME. PART TOTAL CYCLES: 7,184.
- [SDR AU980827](https://openairdocs.org/sdr/AU980827), May 15, 1998: RIB. CRACKED. (AUS) AILERON NOSE RIBS CRACKED. FOUND DURING INSPECTION IAW PIPER SB 1011. PART TOTAL CYCLES: 1,879.
- [SDR AU980826](https://openairdocs.org/sdr/AU980826), May 15, 1998: RIB. CRACKED. (AUS) AILERON NOSE RIBS CRACKED. FOUND DURING INSPECTION IAW PIPER SB 1011. PART TOTAL CYCLES: 1,879.

All 82: https://openairdocs.org/model/new-piper-pa-32r-301/reports.md

## STCs that may be installed (OpenAirDocs) (281, 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 SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [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 SA04568CH](https://openairdocs.org/stc/SA04568CH): Installation of the uAvionix tailBeaconX, a tail mounted position light with integrated Automatic Dependent Surveillance - Broadcast (ADS-B) Out and 1090MHz Mode-S transponder functionality. uAvionix Corporation
- [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 SA00953AT](https://openairdocs.org/stc/SA00953AT): Installation of a composite 'HOWL COWL,' mod comp engine cowling w/COWL FLAPS, full length nosegear close doors, belly fairing aft of firewall to streamline forward sec of exposed belly structures 'strakes' and large access doors on both sides of cowling. Whelen Aerospace Technologies
- [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 SA01820WI](https://openairdocs.org/stc/SA01820WI): Installation of a Lycoming IO-540-K1G5 Engine. Aeronautix LLC
- [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

All 281: https://openairdocs.org/model/new-piper-pa-32r-301/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
- [AF38738-05-LM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID193745621720250212132026.0001): Rear Center Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68031-07 · Feb 11, 2025
- [AF68833-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192669880320250212132036.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF99776-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192004731720250212132038.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF68831-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189063926120250212132035.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF38737-02-LCLM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188067793420250212132022.0001): RH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 38737-02 · Feb 11, 2025
- [AF68830-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185627863620250212132029.0001): Left Side Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68830-00 · Feb 11, 2025
- [AF38739-02-LCSM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182309329820250212132027.0001): LH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces AF38739-02 · Feb 11, 2025
- [AF68832-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181466344820250212132035.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF38738-024-LM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179971587820250212132034.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF87524-042](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175081475620250212132031.0001): LH Front Bracket. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF99769-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175075940020250212132032.0001): LH FWD Cover Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 99769-00 · Feb 11, 2025
- [AF99766-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169186930220250212132037.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF38737-02-LCSM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168461548720250212132022.0001): RH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 38737-02 · Feb 11, 2025
- [AF68030-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166022835820250212132023.0001): Rh Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68030-10 · Feb 11, 2025
- [AF87524-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165768764720250212132031.0001): LH Front Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 87524-04 · Feb 11, 2025
- [AF68029-093](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165553414520250212132034.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF38738-05-LM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165419685720250212132025.0001): Rear Center Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 38738-05 · Feb 11, 2025
- [AF38738-05-SM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163388751620250212132025.0001): Rear Center Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 38738-05 · Feb 11, 2025
- [AF99778-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156955953020250212132038.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF68029-09](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155761695920250212132028.0001): LH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68029-09 · Feb 11, 2025
- [AF38737-02-SCSM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152241652120250212132021.0001): RH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 38737-02 · Feb 11, 2025
- [AF87524-044](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150976343520250212132037.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF68031-052](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149174816120250212132035.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF68030-10-SCLM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137803500420250212132023.0001): Rh Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68030-10 · Feb 11, 2025
- [AF38737-02-SCLM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137697031920250212132022.0001): RH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 38737-02 · Feb 11, 2025
- [AF68830-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134344448020250212132035.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF99781-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134262577320250212132033.0001): RH Front Cylinder Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 99781-00 · Feb 11, 2025
- [AF68833-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134249311920250212132030.0001): Right Side Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68833-05 · Feb 11, 2025
- [AF38739-02-LCLM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134010491320250212132027.0001): LH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces AF38739-02 · Feb 11, 2025
- [AF99778-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133352470420250212132033.0001): RH Front Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 99778-00,99778-03 · Feb 11, 2025
- [AF68835-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128094161520250212132036.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF68832-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126106668920250212132029.0001): Left Side Front Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68832-00 · Feb 11, 2025
- [AF38739-026](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125358082120250212132034.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF87526-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121802705120250212132032.0001): RH Front Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 87526-02 · Feb 11, 2025
- [AF38738-05-SM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116342971620250212132026.0001): Rear Center Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68031-07 · Feb 11, 2025
- [AF68834-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115552264120250212132030.0001): Right Side Center Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68834-00 · Feb 11, 2025
- [AF68834-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112900601320250212132036.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025
- [AF38739-02-SCLM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109655947520250212132027.0001): LH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces AF38739-02 · Feb 11, 2025
- [AF99776-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108865865820250212132033.0001): RH Front Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 99776-00 · Feb 11, 2025
- [AF38739-02-SCSM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107069700020250212132026.0001): LH Rear Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces AF38739-02 · Feb 11, 2025
- [AF68835-00](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105176907820250212132031.0001): Right Side Front Baffle Assembly. Airforms LLC · PMA PQ2644CE · Replaces 68835-00 · Feb 11, 2025
- [AF99769-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID104853718320250212132038.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Feb 11, 2025

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

## The same model under other registry codes

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

- [Piper PA-32R-301](https://openairdocs.org/model/piper-pa-32r-301): 456 registered aircraft, registry code 7103218

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.