# New Piper PA46-350P - Type: Aircraft model (FAA registry) - Registry code: 7104607 - Manufacturer (registry): NEW PIPER - Model: PA46-350P - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 6 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A25SO](https://openairdocs.org/tcds/A25SO) (OpenAirDocs) - Holder: Piper Aircraft Inc. - Registered aircraft: 9 - Page: https://openairdocs.org/model/new-piper-pa46-350p 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 2023-25-02](https://openairdocs.org/ad/2023-25-02): Control Column Section · Piper PA-46-350P, PA-46-500TP and PA-46-600TP. Effective Dec 19, 2023 - [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 2021-09-02](https://openairdocs.org/ad/2021-09-02): VACUUM SYSTEM · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Apr 16, 2021 - [AD 2015-13-09](https://openairdocs.org/ad/2015-13-09): Cabin Pressure Control System · Piper PA-46-350P and PA-46-500TP. Effective Jul 13, 2015 - [AD 2013-13-01](https://openairdocs.org/ad/2013-13-01): Fuel Storage · Piper PA-46-310P, PA-46-350P, PA-46-500TP and 1 more. Effective Jul 10, 2013 - [AD 2011-06-10](https://openairdocs.org/ad/2011-06-10): Engine Indicating · Piper PA-46-310P, PA-46-350P and PA-46R-350T. Effective May 6, 2011 - [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 2009-07-08](https://openairdocs.org/ad/2009-07-08): 35-amp and 250-amp current limiters · Piper PA-46-350P and PA-46R-350T. Effective May 5, 2009 - [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 2008-26-11](https://openairdocs.org/ad/2008-26-11): Stall vane heater · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Jan 28, 2009 - [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 2001-12-01](https://openairdocs.org/ad/2001-12-01): Inboard Flap Drive Bellcrank Assemblies · Piper PA-46-310P, PA-46-350P and PA-46-500TP. Effective Jun 29, 2001 - [AD 2001-10-09](https://openairdocs.org/ad/2001-10-09): Automatic Flight Control Systems · Aerostar PA-60-700P (Aerostar 700P), 208, 208B and 15 more. Effective Jun 15, 2001 - [AD 99-16-06](https://openairdocs.org/ad/99-16-06): Wing Attach Fittings · Piper PA-46-350P. Effective Sep 24, 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 98-04-26](https://openairdocs.org/ad/98-04-26): AFM - Limitations Section - Icing · Piper PA-46-310P and PA-46-350P. Effective Mar 13, 1998 - [AD 96-12-22](https://openairdocs.org/ad/96-12-22): Full Flow Engine Oil Adapter · Bellanca CH-300 Pacemaker, 120, 140 and 361 more. Effective Jul 31, 1996 - [AD 95-23-12](https://openairdocs.org/ad/95-23-12): Placard - Manifold Pressure Limits · Piper PA-46-350P. Effective Jan 8, 1996 - [AD 92-18-08](https://openairdocs.org/ad/92-18-08): Flight Control Systems · Piper PA-46-310P and PA-46-350P. Effective Oct 2, 1992 - [AD 92-15-14](https://openairdocs.org/ad/92-15-14): Air-Driven Attitude Gyro · Piper PA-46-310P and PA-46-350P. Effective Aug 22, 1992 - [AD 92-13-07](https://openairdocs.org/ad/92-13-07): Empennage Countersunk Rivets · Piper PA-46-310P and PA-46-350P. Effective Aug 21, 1992 - [AD 92-13-06](https://openairdocs.org/ad/92-13-06): Elevator Guide Tube · Piper PA-46-310P and PA-46-350P. Effective Aug 21, 1992 Historical (superseded or no longer in force): - [AD 2021-04-07](https://openairdocs.org/ad/2021-04-07) (historical): VACUUM SYSTEM · Piper PA-46-350P, PA-46-500TP and PA-46R-350T. Effective Mar 30, 2021 - [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 99-15-04 R1](https://openairdocs.org/ad/99-15-04-R1) (historical): Turbine Inlet Temperature System Calibration · Piper PA-46-310P and PA-46-350P. Effective Jul 28, 2000 - [AD 99-15-04](https://openairdocs.org/ad/99-15-04) (historical): Turbine Inlet Temperature System Calibration · Piper PA-46-310P and PA-46-350P. Effective Aug 31, 1999 ## Information bulletins (advisory) (10) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-17-02](https://openairdocs.org/saib/CE-17-02): Cabin Altitude Encoder Alternative Method of Compliance (AMOC) to Airworthiness Directive (AD) 2015-13-09; Terminating Action. Issued Dec 13, 2016 - [SAIB CE-15-18](https://openairdocs.org/saib/CE-15-18): WING SPAR Main Spar Lower Cap Cracks. Issued Jun 15, 2015 - [SAIB CE-14-23](https://openairdocs.org/saib/CE-14-23): Powerplant; Air Intake. Issued Aug 6, 2014 - [SAIB CE-09-13R1](https://openairdocs.org/saib/CE-09-13R1): POWERPLANT - ENGINE MOUNT Cracking at nose landing gear attachment and trunnion attachment. Issued Jul 14, 2014 - [SAIB CE-09-13](https://openairdocs.org/saib/CE-09-13) (historical): Landing Gear: Engine Mount-Nose Landing Gear Attach Section. Issued Feb 23, 2009 - [SAIB CE-08-13](https://openairdocs.org/saib/CE-08-13): Electrical Power. Issued Feb 27, 2008 - [SAIB CE-07-08](https://openairdocs.org/saib/CE-07-08): Avidyne Primary Flight display (PFD). Issued Oct 31, 2006 - [SAIB CE-01-30](https://openairdocs.org/saib/CE-01-30): . Issued Jul 11, 2001 - [SAIB ACE-99-03](https://openairdocs.org/saib/ACE-99-03): . Issued Oct 21, 1998 ## Registered aircraft (9) - [N3131M](https://openairdocs.org/aircraft/N3131M): [Air Service LLC](https://openairdocs.org/faa-owner/AIR%20SERVICE%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2006, S/N 4636382 - [N3151G](https://openairdocs.org/aircraft/N3151G): [Mtc Aviation LLC](https://openairdocs.org/faa-owner/MTC%20AVIATION%20LLC), [New Harmony, UT](https://openairdocs.org/faa-place/UT/New%20Harmony), S/N 4636390 - [N369ST](https://openairdocs.org/aircraft/N369ST): [Aero-Mobil Inc](https://openairdocs.org/faa-owner/AERO-MOBIL%20INC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2006, S/N 4636396 - [N379P](https://openairdocs.org/aircraft/N379P): [Visionary Holdings LLC](https://openairdocs.org/faa-owner/VISIONARY%20HOLDINGS%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 2006, S/N 4636379 - [N389ST](https://openairdocs.org/aircraft/N389ST): [Southgroup Aviation LLC](https://openairdocs.org/faa-owner/SOUTHGROUP%20AVIATION%20LLC), [Oxford, MS](https://openairdocs.org/faa-place/MS/Oxford), built 2006, S/N 4636389 - [N48HC](https://openairdocs.org/aircraft/N48HC): [Mirage Flight LLC](https://openairdocs.org/faa-owner/MIRAGE%20FLIGHT%20LLC), [Kalispell, MT](https://openairdocs.org/faa-place/MT/Kalispell), S/N 4636377 - [N747TH](https://openairdocs.org/aircraft/N747TH): [Philburto Consulting Ltd](https://openairdocs.org/faa-owner/PHILBURTO%20CONSULTING%20LTD), [Telluride, CO](https://openairdocs.org/faa-place/CO/Telluride), built 2006, S/N 4636392 - [N915ED](https://openairdocs.org/aircraft/N915ED): [Sqa Services Inc](https://openairdocs.org/faa-owner/SQA%20SERVICES%20INC), [Pls Vrds Est, CA](https://openairdocs.org/faa-place/CA/Pls%20Vrds%20Est), built 2006, S/N 4636397 - [N956AD](https://openairdocs.org/aircraft/N956AD): [Joel W Nikle](https://openairdocs.org/faa-owner/JOEL%20W%20NIKLE), [Fargo, ND](https://openairdocs.org/faa-place/ND/Fargo), built 2006, S/N 4636385 ## NTSB investigations (4) 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 CEN21WA059](https://openairdocs.org/ntsb/CEN21WA059), Oct 10, 2020: Piper PA46 (N369ST), Villingen-Schwenningen, Germany, substantial damage - [NTSB ERA15WA119](https://openairdocs.org/ntsb/ERA15WA119), Jan 26, 2015: New Piper PA46 350P (N369ST), Milan, Italy, substantial damage - [NTSB WPR14CA057](https://openairdocs.org/ntsb/WPR14CA057), Nov 23, 2013: New Piper PA46 350P (N3151G), Salt Lake City, UT, substantial damage. Probable cause: The pilot's failure to extend the landing gear before landing. Contributing to the accident was the pilot's improper use of the checklist. - [NTSB WPR09CA066](https://openairdocs.org/ntsb/WPR09CA066), Dec 22, 2008: Piper PA-46-350P (N379P), Idaho Falls, ID, substantial damage. Probable cause: The pilot's failure to maintain directional control during the landing roll. Contributing to the accident were the icy runway conditions and a snow bank. ## FAA accident and incident reports (6) 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 20170305001199I](https://openairdocs.org/incident/20170305001199I), Mar 5, 2017: New Piper PA46-350P (N3131M), Alexander City, AL, No damage. Pilot reported engine problem in flight and diverted to alx and landed safely without incident. Onsite mechanic removed left inoperative turbocharger and… - [Incident 20160225002109I](https://openairdocs.org/incident/20160225002109I), Feb 25, 2016: Piper PA 46-350P (N747TH), Manassas, VA, Substantial damage. This Piper PA46 landed on runway 34R. At the point of touchdown, the aircraft imediately pulled to the left, off of the runway into the grass. In the process… - [Incident 20140128000629I](https://openairdocs.org/incident/20140128000629I), Jan 28, 2014: New Piper PA46-350P (N841ST), Sabetha, KS, Minor damage. On January 28, 2014, at approximately 1600 local time (2200 UTC), a private pilot, with an instrument rating, was involved in an aircraft incident while… - [Accident 20131123022079A](https://openairdocs.org/incident/20131123022079A), Nov 23, 2013: New Piper PA46-350P (N3151G), Salt Lake City, UT, Substantial damage. The pilot stated that he landed the aircraft without lowering the landing gear. He had taken off for a local flight with one passenger on board with the… - [Incident 20100827045652I](https://openairdocs.org/incident/20100827045652I), Aug 27, 2010: Piper PA46-350P (N3151G), San Carlos, CA, Minor damage. While parked at the parking ramp with the engine operating and the PIC not in the pilot seat, the aircraft to taxi across the parking taxiway and struck an… - [Accident 20081221853589A](https://openairdocs.org/incident/20081221853589A), Dec 21, 2008: Piper PA46350P (N379P), Idaho Falls, ID, Substantial damage. On December 21, 2008 at approximately 18:26 local time N379P (PA46-350) veered off of the left side of runway 2 at Idaho Falls, ID (kida). The pilot stated… ## Service difficulty reports (229, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000805](https://openairdocs.org/sdr/2026FA0000805), Oct 1, 2026: BOLT. BACKED OUT. AFTER THE AIRPLANE WAS PUT AWAY, NOTICED THE LEFT ELEVATOR HINGE BOLT HAS BACKED OUT AND THE ELEVATOR WAS HANGING, DISCONNECTED FROM THE HORIZONTAL STABILIZER. - [SDR 2025FA0000649](https://openairdocs.org/sdr/2025FA0000649), Sep 17, 2025: SKIN. CRACKED. DURING EXTERIOR INSPECTION ON JANUARY 15 2025 AND AGAIN JULY 2, 2025, MULTIPLE CRACKS WERE OBSERVED IN THE WING UPPER SKIN PANELS OF BOTH THE LEFT AND RIGHT WIN - [SDR 2024FA0000728](https://openairdocs.org/sdr/2024FA0000728), Sep 19, 2024: VALVE. MULTIPLE FAIL. 5 MONTH OLD EMERGENCY EXTENSION VALVE FAILED OPERATIONAL CHECK, INSTALLED IN NEW CONDITION. RECEIVED AND INSTALLED NEW EMERGENCY EXTENSION VALVE, IN MANUFACTURE - [SDR 2024FA0000632](https://openairdocs.org/sdr/2024FA0000632), Aug 23, 2024: TRANSDUCER. FAILED. IN LATE JUNE 2023 AFTER LANDING AT WICK SCOTLAND ON A TRANSATLANTIC OUR FERRY PILOT NOTICED A SUBSTANTIAL AMOUNT OF OIL LEAKING OUT UNDER THE AIRCRAFT, TROUBLES - [SDR 2024FA0000293](https://openairdocs.org/sdr/2024FA0000293), Apr 5, 2024: TUBE. CRACKED. FLAPS GOT STUCK IN FULL DOWN POSITION ON APPROACH AND WOULD NOT RETRACT. AFTER INSPECTION BY MAINTENANCE, IT WAS FOUND THAT THE FLAP TUBE ASSEMBLY THAT ATTACHES - [SDR 2024FA0000334](https://openairdocs.org/sdr/2024FA0000334), Jan 11, 2024: LOCK FASTENER. LOOSE. AFT WING FITTING LOCK FASTENERS FOUND LOOSE ON LEFT AND RIGHT WING. ADDRESSED IN PIPPER SB820A BUT NOT APPLICABLE TO THIS MODEL AIRCRAFT AND SHOULD BE. - [SDR 2023FA0000746](https://openairdocs.org/sdr/2023FA0000746), Nov 1, 2023: MAGNETO. FAILED. I AM REACHING OUT BECAUSE WE HAVE HAD 3 MAGNETO FAILURES IN 20 HOURS TSMOH. IT’S A PIPER PA46-350P WITH LYCOMING TIO-540-AE2A. FAILURE 1) NEW SLICK 6363 MAGNETO - [SDR 2022FA0000532](https://openairdocs.org/sdr/2022FA0000532), Sep 20, 2022: PIPE. DEFORMED. A 12 MONTH / 250 HOUR INSPECTION OF THE EXHAUST SYSTEM SLIP JOINTS AND MARMON CLAMPS, IS WAS NOTED THAT THE CROSSOVER EXHAUST TUBES COULD NOT BE SEPARATED. THE - [SDR 2022FA0000362](https://openairdocs.org/sdr/2022FA0000362), Jul 20, 2022: SPARK PLUG. WEAK. PILOT REPORTED AIRCRAFT SEEMED TO BE SHORT ON POWER DURING CLIMB. AIRSPEED WAS SLIGHTLY BELOW EXPECTED. PILOT PERFORMED AN IN FLIGHT MAG CHECK AND NOTED THAT EN - [SDR 2022FA0000291](https://openairdocs.org/sdr/2022FA0000291), Jun 15, 2022: MAGNETO. WORN. OPERATOR REPORTED DIFFICULTY STARTING THE AIRCRAFT. UPON CHECKING THE MAGNETO TO ENGINE TIMING, IT WAS FOUND THAT THE RETARD BREAKER POINTS WERE OPENING VERY LA - [SDR 2022FA0000266](https://openairdocs.org/sdr/2022FA0000266), May 22, 2022: IGNITION SYS. DEFECTIVE. INSTALLED ELECTROAIR ELECTRONIC IGNITION 61000-5M TO REPLACE LH MAGNETO ON PIPER MIRAGE WITH LYCOMING TIO-540-AE2A ENGINE IN NOV 2018 PER STC FOR TURBOCHARGED L - [SDR 2022FA0000177](https://openairdocs.org/sdr/2022FA0000177), Mar 21, 2022: SQUAT SWITCH. SHIFTED. I DEPARTED RW 14 AT APPROXIMATELY 8 AM LOCAL TIME @ KDTS. IN THE CLIMB, I ATTEMPTED TO RETRACT THE LANDING GEAR WITH NO SUCCESS (3 GREENS REMAINED LIT). I NOTIF - [SDR LF1RN20PT030422](https://openairdocs.org/sdr/LF1RN20PT030422), Mar 4, 2022: NONE. WORN. OWNER REPORTED THE MAG DROP ON THE LEFT MAGNETO WAS EXCESSIVE. PERFORMED A GROUND RUN AND CONFIRMED THE RPM DROP WAS OVER 150 RPM. CHECKED MAGNETO TO ENGINE TIM - [SDR 2022FA0000277](https://openairdocs.org/sdr/2022FA0000277), Feb 1, 2022: NONE. NONE. NOSE LANDING GEAR COLLAPSED ON ROLL OUT AFTER LANDING, AIRPORT PERSONNEL FOUND A BROKEN BOLT THAT HOLDS THE GEAR IN PLACE. - [SDR 2022FA0000250](https://openairdocs.org/sdr/2022FA0000250), Feb 1, 2022: BOLT. BROKEN. AIRCRAFT N35CM LANDED AT CRYSTAL RIVER AIRPORT ON A GRASS RUNWAY. THE PILOT STATED THAT WHEN THE AIRCRAFT WAS ALMOST TO S STOP AT APPROXIMATELY 10 KNOTS THE NOS - [SDR LF1RN725ED111221](https://openairdocs.org/sdr/LF1RN725ED111221), Nov 2, 2021: SQUAT SWITCH. OPEN. OPERATOR REPORTED "HYDRA PUMP ON" MESSAGE WHEN RETRACTING LANDING GEAR AFTER TAKEOFF. IT WAS ALSO NOTED THAT THE CABIN PRESSURIZATION WAS NOT PRESSURIZING INTER - [SDR 2021FA0000276](https://openairdocs.org/sdr/2021FA0000276), Oct 2, 2021: CRANKCASE. CRACKED. A PERSISTENT ENGINE OIL LEAK WAS TRACED TO THE RIGHT HAND SIDE OF THE ENGINE CRANKCASE IN FRONT AND BELOW THE VALVE ROCKER BOX COVER AN DRAIN FITTING. - [SDR LF1RJAN0820PT](https://openairdocs.org/sdr/LF1RJAN0820PT), Jan 8, 2021: SEAL. LEAKING. AIRCRAFT CAME INTO SHOP FOR A DOOR SEAL REPLACEMENT. AFTER REPLACING DOOR SEAL, THE FUSELAGE WAS PRESSURIZED PER THE PIPER PA-46-350P AMM. DURING TEST A LEAK WA - [SDR LF1R2020121000002](https://openairdocs.org/sdr/LF1R2020121000002), Dec 9, 2020: PITOT TUBE. LEAKING. OWNER REPORTED THE VERTICAL SPEED INDICATION WAS INTERMITTENTLY FLUCTUATING ON PILOT AND COPILOT SIDE IN CRUISE AND AIRSPEED SEEMED LOW. INSPECTED AIRCRAFT AND - [SDR KW7R20201116001](https://openairdocs.org/sdr/KW7R20201116001), Nov 12, 2020: SKIN. CRACKED. OWNER REPORTED EVIDENCE OF POSSIBLE CRACK ON THE LEFT WING TOP SKIN. INSPECTION REVEALED THE LEFT WING TOP SKIN CRACKED ALONG THE DOUBLE ROW OF RIVETS ALONG THE - [SDR FE6R20201009001](https://openairdocs.org/sdr/FE6R20201009001), Sep 25, 2020: TRANSDUCER. MALFUNCTIONED. THE OPERATOR OF THE THIS AIRCRAFT HAS REPORTED LOW MANIFOLD PRESSURE AND ASKED US TO LOOK INTO IT. WHILE PERFORMING THE BASIC AND DETAILED FUNCTION TESTS OF THE - [SDR 2019FA0000334](https://openairdocs.org/sdr/2019FA0000334), Oct 10, 2019: BEARING. WORN. FUEL CONTROL UNIT PROBLEMS ASSOCIATED WITH CONTROL ROD END BEARING WEAR. - [SDR 2019FA0000222](https://openairdocs.org/sdr/2019FA0000222), Jul 11, 2019: TUBE. FAILED. CUSTOMER REPORTED ON LANDING ROLL LEFT MAIN GEAR TIRE WENT FLAT. TIRES AT TUBES WERE INSTALLED JUNE OF 2018 WITH LESS THAN 30 HOURS ON THE AIRCRAFT SINCE INSTAL - [SDR 2019FA0000173](https://openairdocs.org/sdr/2019FA0000173), Jun 4, 2019: GASKET. IMPROPER PART. DISCOVERED DURING MAINTENANCE, TCM CONTINENTAL TURBO FLANGE GASKETS, P/N: 636465, INSTALLED ON THIS LYCOMING ENGINE. THE GASKETS WERE NOT IN FULL CONTACT WITH T - [SDR PAIR2018081074523](https://openairdocs.org/sdr/PAIR2018081074523), Aug 8, 2018: EXHAUST PIPE. SEPARATED. ENGINE EXHAUST CROSSOVER PIPING PARTIALLY SEPARATED CAUSING LOSS OF TURBOCHARGER BOOST, DAMAGING WIRING AND AIR CONDITIONER HOSES AT THE REAR OF THE ENGINE. ALS - [SDR 2018FA0000204](https://openairdocs.org/sdr/2018FA0000204), Jul 22, 2018: SCREW. FAILED. 10 HOURS AFTER ENGINE OVERHAUL THE SET SCREW FAILED TO HOLD THE PROP GOVERNOR IDLER GEAR SHAFT CAUSING THE SHAFT ITSELF TO TURN. THE ALUMINUM THREADING OF THE E - [SDR Q6MR201807180002](https://openairdocs.org/sdr/Q6MR201807180002), Jul 14, 2018: CLAMP. MISSING. PILOT REPORTED REDUCED ENGINE POWER AND LOSS OF MANIFOLD PRESSURE. MAINTENANCE INSPECTED AND FOUND A CLAMP MISSING FROM INTAKE OUTLET DUCT BETWEEN LEFT TURBO AN - [SDR 2016FA0000324](https://openairdocs.org/sdr/2016FA0000324), Jul 11, 2016: DIODE. SEPARATED. LANDED GEAR UP DUE TO AN PARTIAL ELECTRICAL FAILURE. WHILE CONDUCTING THE ACCIDENT INVESTIGATION, DISCOVERED THAT THE LEFT ISOLATION DIODE (RECTIFIER ASSY) FROM - [SDR 2016FA0000295](https://openairdocs.org/sdr/2016FA0000295), Jun 15, 2016: CONTROL HORN. MISINSTALLED. DURING ANNUAL INSPECTION, MECHANIC NOTICED LATERAL PLAY IN THE ELEVATOR CONTROL HORN. ELEVATOR CONTROL HORN REMOVED AND FURTHER INSPECTION SHOWED THAT THE HOLES - [SDR HPFR2016FA0000281](https://openairdocs.org/sdr/HPFR2016FA0000281), May 5, 2016: TURBOCHARGER. FAILED. PILOT REPORTED LOSS OF POWER, FOLLOWED BY PRESSURIZATION LOSS. DURING CLIMB, ENGINE KEPT RUNNING WELL, BUT POWER WAS LIMITED TO 19" HG INSTEAD OF 35" HG- PRIOR - [SDR 2016041400000181](https://openairdocs.org/sdr/2016041400000181), Apr 11, 2016: HORN. WORN. DURING SCHEDULED MAINTENANCE, MECHANIC NOTICED LATERAL PLAY IN THE ELEVATOR CONTROL HORN. ELEVATOR CONTROL HORN REMOVED AND FURTHER INSPECTION SHOWED THAT THE H - [SDR 2016FA0000025](https://openairdocs.org/sdr/2016FA0000025), Jan 20, 2016: DOUBLER. CRACKED. FORWARD AND AFT COMM ANTENNA DOUBLERS AND SKIN CRACKED. - [SDR 2016FA0000024](https://openairdocs.org/sdr/2016FA0000024), Jan 20, 2016: DOUBLER. CRACKED. SKIN AND DOUBLER CRACKING UNDER AFT COMM ANTENNA. FOUND DOUBLER TOO SMALL AND THIN. - [SDR 2015FA0000644](https://openairdocs.org/sdr/2015FA0000644), Dec 11, 2015: MOUNT. CRACKED. ENGINE MOUNT WAS AT A NEAR FAILURE STATE WHEN INSPECTED DURING NORMAL ANNUAL. - [SDR BQVD201505150001](https://openairdocs.org/sdr/BQVD201505150001), May 11, 2015: RELAY. FAILED. AIRCRAFT EXPERIENCED AN ELECTRICAL POWER SHUTDOWN & REBOOT. STARTER ENGAGED WARNING WAS OBSERVED. THE STARTER, STARTER SWITCH, STARTER CONTACTOR, AND STARTER RE - [SDR CA150525004](https://openairdocs.org/sdr/CA150525004), May 7, 2015: ENGINE. FAILED. (CAN) UNCONFIRMED REPORTS SUGGEST THE ACFT WAS ATTEMPTING AN EMERGENCY LANDING AFTER THE PILOT HAD REPORTED THE ACFT WAS SUFFERING ENGINE PROBLEMS. THE ACFT CAM - [SDR 2015FA0000144](https://openairdocs.org/sdr/2015FA0000144), Apr 10, 2015: MOTOR. FAILED. GROUND BLOWER FAILED, UNCERTAIN OF INSTALL DATE. MOTOR SHOWS MANUFACTURER DATE OF 5/26/2009. MOTOR FAILED AND DID NOT TRIP THE CIRCUIT BREAKER. MOTOR IS IN THE - [SDR HX1R2015033100001](https://openairdocs.org/sdr/HX1R2015033100001), Feb 17, 2015: EXHAUST PIPE. DAMAGED. DURING ANNUAL INSPECTION, CYLINDER NR 6 EXHAUST TRANSITION PIPE APPEARED TO BE STARTING TO BLISTER ON OUTSIDE, PHOTOS NR 3 & NR 4. TRANSITION PIPE WAS REMOVED T - [SDR C41R201405280001](https://openairdocs.org/sdr/C41R201405280001), May 27, 2014: CROSSOVER TUBE. CRACKED. FOUND PILOT'S RUDDER PEDAL CROSSOVER TUBE CRACKED AT WELD. MFG CONTACTED AND NOTIFIED OF SITUATION AND PROVIDED PHOTOS. POSSIBLE DUE TO INCORRECT WELD PROCESS. - [SDR 2014FA0000323](https://openairdocs.org/sdr/2014FA0000323), Apr 11, 2014: MOUNT. BROKEN. THE NLG DID NOT FULLY EXTEND AND CENTER DURING DOWN EXTENSION. ENGINE MOUNT IS BROKEN IN THE AREA, TO BE INSPECTED.. THE ENGINE MOUNT HAS AN INITIAL INSPECTION - [SDR 2014FA0000242](https://openairdocs.org/sdr/2014FA0000242), Apr 7, 2014: HORN. MISINSTALLED. DURING AN ANNUAL INSPECTION, MECHANIC NOTICED LATERAL PLAY IN THE ELEVATOR CONTROL HORN. ELEVATOR CONTROL HORN WAS REMOVED AND FURTHER INSPECTION SHOWED THAT TH - [SDR 2014FA0000241](https://openairdocs.org/sdr/2014FA0000241), Apr 7, 2014: HORN. MISINSTALLED. DURING AN ANNUAL INSPECTION, MECHANIC NOTICED LATERAL PLAY IN THE ELEVATOR CONTROL HORN. ELEVATOR CONTROL HORN REMOVED AND FURTHER INSPECTION SHOWED THAT THE HO - [SDR K5SR201404042365](https://openairdocs.org/sdr/K5SR201404042365), Mar 25, 2014: MAGNETO. FAILED. AT CRUISE POWER, ENGINE RAN ROUGH AND MISSED. RETURN TO DEPARTURE AND FOUND RT MAGNETO TO BE THE PROBLEM. MAGNETO WAS INSTALLED NEW IN THE ACFT ON 01/28/2014. T - [SDR M3VY20140109001](https://openairdocs.org/sdr/M3VY20140109001), Jan 8, 2014: SKIN. DAMAGED. DURING INSPECTION, SKIN WAS FOUND CRACKED AND TORN. - [SDR 2014FA0000237](https://openairdocs.org/sdr/2014FA0000237), Nov 6, 2013: PISTON RING. BROKEN. DURING IFR FLIGHT, VMC ON TOP, IMC BELOW, NORMAL CRUISE, EXPERIENCED DECLINING AND FLUCTUATING OIL PRESSURE ABOUT TWO HOURS AFTER TAKEOFF. NORMAL CRUISE OP IS A - [SDR 2013FA0000501](https://openairdocs.org/sdr/2013FA0000501), Sep 3, 2013: BOLT. BROKEN. ACFT CAME IN FOR A TIRE CHANGE. UPON REMOVAL OF THE NOSE WHEEL ASSY PN 40-77B, IT WAS NOTED THAT ONE WHEEL TIE BOLT WAS MISSING. THIS WHEEL HAS A TOTAL OF 3 TIE - [SDR C41R201307160001](https://openairdocs.org/sdr/C41R201307160001), Jul 12, 2013: TIMER. FAILED. OWNER REPORTED INOPERATIVE WING DE-ICE BOOTS. FOUND LOWER VACUUM PUMP COUPLING SHEARED AND BOTH DEICE SOLENOID VALVES SEIZED IN CLOSED POSITION. DURING RUN UP P - [SDR CA130502004](https://openairdocs.org/sdr/CA130502004), Apr 28, 2013: OIL SYSTEM. LOW PRESSURE. (CAN) THE PILOT REPORTED AN OIL PRESSURE LOSS DURING TAKEOFF. OIL PRESSURE DROPPED BELOW 40 PSI AND OIL TEMPERATURE WAS AT 62 DEG. C. THE PILOT DECLARED AN EMER - [SDR CA130425003](https://openairdocs.org/sdr/CA130425003), Apr 25, 2013: MOUNT. CRACKED. (CAN) COMPLETING SB1103D, FOUND CRACK IN NOSE GEAR ACTUATOR MOUNT OF ENGINE MOUNT. - [SDR CA130425004](https://openairdocs.org/sdr/CA130425004), Mar 6, 2013: LANDING GEAR. MISINSTALLED. (CAN) - A/C LANDED WITH NOSE WHEEL STEERING HORN ASSY JAMMED IN ENGINE MOUNT TUBE CAUSING AIRCRAFT TO DEPART RUNWAY. IMPACT WITH SNOW BANK CAUSED FURTHER NOSE G All 229: https://openairdocs.org/model/new-piper-pa46-350p/reports.md ## STCs that may be installed (OpenAirDocs) (173, 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 SA01844WI](https://openairdocs.org/stc/SA01844WI): Installation of Garmin GFC 600 Automatic Flight Control System. Garmin International Inc - [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 SA04188NY](https://openairdocs.org/stc/SA04188NY): Installation of LAI CoolView Windshields and Windows. Lee Aerospace 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 SA01843CH](https://openairdocs.org/stc/SA01843CH): Replacement of certain Goodrich pneumatic deicer boots. SMR Aquisition LLC dba SMR Technologies Inc - [STC SA04734NY](https://openairdocs.org/stc/SA04734NY): Installation of LAI LH Heated Windshield. Lee Aerospace Inc - [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 SA03825AT-D](https://openairdocs.org/stc/SA03825AT-D): Installation of a Forward Vision EVS-100 and EVS-600 Infrared Camera System in the Piper PA-46-310P, PA-46-350P and PA-46-350T Models. Summit Aviation Inc - [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 SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics - [STC SA04586CH](https://openairdocs.org/stc/SA04586CH): Installation of Electroair Back Up Battery Panel System Control. Electroair Aquisition Corp - [STC SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA01834WI](https://openairdocs.org/stc/SA01834WI): Installation of a modified Climate Control System. Cutter Aviation Inc - [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 SA09856AC](https://openairdocs.org/stc/SA09856AC): Installation of BendixKing Aerowave 100 In-flight Data Link System for non-essential, non-required aircraft Cabin Systems & Equipments. Honeywell International Inc (Bendix King) - [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 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 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 - [STC SA01006WI-D](https://openairdocs.org/stc/SA01006WI-D): Installation of Bendix/King KMD 850 Multi-Function Display System and the optional Bendix/King KMH 980/KMH 880 Multi-Hazard Awareness Systems/KTA 870 Traffic Awareness System/KTA 970 Traffic Alert and Collision Avoidance System and KDR 510 VHF Datalink System. Honeywell International Inc - [STC SA00656WI-D](https://openairdocs.org/stc/SA00656WI-D): Installation of Bendix/King KFC 225 Automatic Flight Control System. Honeywell International Inc - [STC SA1778CE-D](https://openairdocs.org/stc/SA1778CE-D): Installation of KAP 100 single-axis, KAP 150 two-axis or KFC 150 two-axis flight control system with optional third (yaw) axis and opetional KAS 297B vertical speed and altitude selector. Honeywell International Inc - [STC SA01560WI-D](https://openairdocs.org/stc/SA01560WI-D): Installation of the Honeywell KFD 840 Primary Flight Display System. Honeywell International Inc - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA01750SE](https://openairdocs.org/stc/SA01750SE): Fabrication and Installation of Dahlia Doubler. Fliegen Works Inc - [STC SA01751SE](https://openairdocs.org/stc/SA01751SE): Fabrication and Installation of Panida Doubler. Fliegen Works Inc - [STC SA01752SE](https://openairdocs.org/stc/SA01752SE): Fabrication and Installation of Panida Doubler. Fliegen Works Inc - [STC SA04364NY](https://openairdocs.org/stc/SA04364NY): Installation of Wheels & Brake System. Beringer Aero S.A.S - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation All 173: https://openairdocs.org/model/new-piper-pa46-350p/stcs.md ## PMA parts (OpenAirDocs) (629, 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. - [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 - [AF89729-036-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199705809420251113202122.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89744-0031](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199108920420251113202127.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89739-0096](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198919608620251113202126.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89729-036-14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197075050220251113202122.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89745-0023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194707167920251113202128.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89737-0025](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189278197720251113202123.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89746-0023](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID188812515620251113202129.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89729-036-09](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186805249320251113202121.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89745-0024](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182391011920251113202128.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89738-0026](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180924921220251113202124.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89745-0025](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180376562420251113202128.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89746-0024](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175092889220251113202129.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89729-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174361078120251113202116.0001): LH Fwd Mid Baffle Plate Assy. Airforms LLC · PMA PQ2644CE · Replaces 89729-004 · Sep 22, 2025 - [AF89739-0094A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170372758720251113202125.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89744-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170173131820251113202119.0001): LH Rear Inboard Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89744-002 · Sep 22, 2025 - [AF85593-002-WELD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170018203320251113202116.0001): Rocker Mount Bracket, Welded Assy. Airforms LLC · PMA PQ2644CE · Replaces 85593-002 · Sep 22, 2025 - [AF89743-0042](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167399951920251113202127.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89758-060-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166481056720251113202130.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89746-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164460349620251113202119.0001): Rear Center Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89746-002 · Sep 22, 2025 - [AF89731-011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163262322820251113202117.0001): RH Fwd Upper Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89731-011 · Sep 22, 2025 - [AF89746-0025](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160020811220251113202129.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89758-060](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159940146320251113202120.0001): RH Fwd Lower Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89758-060 · Sep 22, 2025 - [AF89729-036-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158404392420251113202122.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89737-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157639768220251113202117.0001): LH Rocker Cover Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89737-002 · Sep 22, 2025 - [AF89729-0044](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156817071220251113202121.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89744-0032](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156786673020251113202127.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89731-009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156166318020251113202117.0001): Baffle. Airforms LLC · PMA PQ2644CE · Replaces 89731-009 · Sep 22, 2025 - [AF89738-0027](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153270743820251113202124.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89758-0053](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152820246020251113202130.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89744-0030](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152095805120251113202127.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89729-036-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151612659620251113202122.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89738-0025](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151463051520251113202124.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89742-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148823187720251113202118.0001): LH Fwd Upper Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89742-002 · Sep 22, 2025 - [AF89758-0052](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146673178520251113202130.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89739-0098](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146225916320251113202126.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89739-0097](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145983280920251113202126.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89743-004](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144909033620251113202119.0001): RH Rear Inboard Baffle Assy. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89758-0573](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140640889720251113202130.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89729-036](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139492803420251113202117.0001): LH Fwd Lower Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89729-036 · Sep 22, 2025 - [AF89745-0026](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131701322020251113202128.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89739-009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130448545820251113202118.0001): LH Rear Outboard Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89739-009 · Sep 22, 2025 - [AF89737-0024](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129581274620251113202123.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89737-0026](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127797857720251113202123.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89758-005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125293023820251113202120.0001): RH Fwd Inboard Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89758-005 · Sep 22, 2025 - [AF89758-057](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124494510820251113202120.0001): Fwd Center Baffle Assy. Airforms LLC · PMA PQ2644CE · Replaces 89758-057 · Sep 22, 2025 - [AF89739-0094B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124249196820251113202125.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89729-0042](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123887575020251113202120.0001): Seal Plate. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 - [AF89738-0028](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122892190820251113202125.0001): Seal. Airforms LLC · PMA PQ2644CE · Modification part · Sep 22, 2025 All of them: https://openairdocs.org/model/new-piper-pa46-350p/pma.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Piper PA 46-350P](https://openairdocs.org/model/piper-pa-46-350p): 381 registered aircraft, registry code 7104620 - [Piper PA 46-350P](https://openairdocs.org/model/piper-pa-46-350p): 156 registered aircraft, registry code 7104619 - [Piper PA 46-350P](https://openairdocs.org/model/piper-pa-46-350p): 105 registered aircraft, registry code 7104627 - [Piper PA 46-350P](https://openairdocs.org/model/piper-pa-46-350p): 23 registered aircraft, registry code 7104618 - [New Piper PA-46-350P](https://openairdocs.org/model/new-piper-pa-46-350p): 7 registered aircraft, registry code 7104608 - [Piper/Hov-Aire PA 46-350P](https://openairdocs.org/model/piper-hov-aire-pa-46-350p): 0 registered aircraft, registry code 7104602 --- 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.