# New Piper PA-46-310P

- Type: Aircraft model (FAA registry)
- Registry codes: 7104612, 7104603
- Manufacturer (registry): NEW PIPER AIRCRAFT INC
- Model: PA-46-310P
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Turbo-prop
- 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: 1
- Page: https://openairdocs.org/model/new-piper-pa-46-310p

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. The FAA lists this model under more than one registry code, usually for different spellings of the maker. This page covers them all.

## 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 2023-09-09](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 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 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 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 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 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
- [AD 88-25-08](https://openairdocs.org/ad/88-25-08): Engine Cooling System · Piper PA-46-310P. Effective Jan 3, 1989
- [AD 87-04-01](https://openairdocs.org/ad/87-04-01): Air Valve Linkage · Piper PA-46-310P. Effective Feb 24, 1987
- [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

Historical (superseded or no longer in force):

- [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) (6)

- [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018
- [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 ACE-99-03](https://openairdocs.org/saib/ACE-99-03): . Issued Oct 21, 1998

## Registered aircraft (1)

- [N350BR](https://openairdocs.org/aircraft/N350BR): [Mmhc Logistics LLC](https://openairdocs.org/faa-owner/MMHC%20LOGISTICS%20LLC), [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis), S/N 4608001

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (119, newest 50)

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

- [SDR 2025FA0000670](https://openairdocs.org/sdr/2025FA0000670), Sep 12, 2025: PUMP. LEAKING. DURING A PLANNED FLIGHT FROM FORT WORTH MEACHAM (KFTW) TO KENOSHA, WI (KENW), THE PILOT OF A PIPER PA-46-310P MALIBU EXPERIENCED A FUEL SYSTEM ANOMALY. APPROXIM
- [SDR 2015FA0000604](https://openairdocs.org/sdr/2015FA0000604), Oct 15, 2015: SELECTOR VALVE. FAILED. PILOT REPORTED LANDING GEAR WOULD NOT EXTEND. TROUBLESHOT, FOUND THAT THE HYDRAULIC POWERPACK WOULD CYCLE 5 TIMES, THEN SHUTOFF. ACCORDING TO THE MM THIS IS NOR
- [SDR DGCA2015042800163](https://openairdocs.org/sdr/DGCA2015042800163), Apr 23, 2015: EXHAUST PIPE. BROKEN. PILOT STATED LOSS OF PRESSURIZATION AND DECREASED MANIFOLD PRESSURE. EXHAUST PIPE BROKEN.
- [SDR 2014FA0000662](https://openairdocs.org/sdr/2014FA0000662), Nov 18, 2014: LOCK NUT. DETACHED. THE LOCKNUT ON THE TURBO COMPRESSOR SHAFT CAME OFF. THE NUT CAUSED DAMAGE TO THE COMPRESSOR FAN BLADES. THE INTER-COOLER WAS REPLACED AS A PRECAUTIONARY MEASURE
- [SDR H6MR2014121745546](https://openairdocs.org/sdr/H6MR2014121745546), Nov 9, 2014: CYLINDER. SEPARATED. AFTER TAKEOFF ACFT WAS CLIMBING THROUGH 8000' WHEN OWNER/PILOT EXPERIENCED A "POP" FOLLOWED BY IMMEDIATE ENGINE ROUGHNESS. PILOT REDUCED POWER AND RETURNED TO D
- [SDR C41R2014071500001](https://openairdocs.org/sdr/C41R2014071500001), Jul 15, 2014: RIB. CRACKED. ACFT WAS UNDERGOING AN ANNUAL INSPECTION AND SEVERAL RIVETS ON THE BOTTOM OF THE LT AND RT WING WERE FOUND SEEPING FUEL. ACFT WAS DEFUELED AND TANK SEALANT REMO
- [SDR CA140630009](https://openairdocs.org/sdr/CA140630009), Jun 18, 2014: UNKNOWN. UNKNOWN. (CAN) THE ACFT WAS CRUISING AT FL270 AND APPARENTLY DEVIATED FROM ITS ROUTE WHILE IN COMMUNICATION WITH ATC. THE AIRCRAFT THEN CRASHED IN AN OPEN FIELD. SEVERE 
- [SDR C41R201307030001](https://openairdocs.org/sdr/C41R201307030001), Jul 3, 2013: O-RING. MISSING. TROUBLESHOT ENGINE OIL CONSUMPTION AND LEAKAGE. FOUND OIL LEAK AFTER NUMEROUS ATTEMPTS TO NARROW OIL LEAK TO A CENTRAL LOCATION. DISCOVERED OIL LEAKING FROM AIR
- [SDR 2013FA0000131](https://openairdocs.org/sdr/2013FA0000131), Feb 27, 2013: CONTROLLER. MALFUNCTIONED. DURING CLIMB, THE PILOT REPORTED A LOSS OF TURBOCHARGING AND CABIN PRESSURIZATION. TROUBLESHOOTING REVEALED THE TURBO CONTROLLER HAD FAILED. THIS WAS THE 4TH FA
- [SDR C41R201201240101](https://openairdocs.org/sdr/C41R201201240101), Jan 23, 2012: MASTER CYLINDER. DAMAGED. ON LANDING ROLLOUT, PILOT HAD NO LT BRAKE. MX REMOVED LT MASTER CYLINDER AND DISCOVERED MASTER CYLINDER END GLAND HAD UNSCREWED ALL BUT 2 THREADS CAUSING FLUID 
- [SDR CA110830005](https://openairdocs.org/sdr/CA110830005), Aug 6, 2011: ENGINE. POWER LOSS. (CAN) ON AUGUST 6, 2011 AT APPROXIMATELY 1700 EDT, THE ABOVE REFERENCED AIRCRAFT EXPERIENCED A LOSS IN ENGINE POWER SOON AFTER TAKEOFF. THE PILOT REPORTED WHILE
- [SDR CA100819009](https://openairdocs.org/sdr/CA100819009), Aug 19, 2010: MOUNT. CRACKED. CRACK DETECTED IN ENGINE MOUNT ON JCAB REGISTERED ACFT. ENGINE MOUNT SWAPPED FOR MOUNT MODIFIED AND REINFORCED WITH TCCA RDC C-RA03-047. NOTE: ENGINE MOUNT REMO
- [SDR CA100812019](https://openairdocs.org/sdr/CA100812019), Aug 12, 2010: MOUNT. CRACKED. (CAN) ENGINE MOUNT DETECTED CRACKED BY AMO SENT IN FOR REPAIR. TWO PIECE FOOT STYLE MOUNT WITH CRACK IN TUBES ABOVE MLG ACTUATOR. ENGINE MOUNT WILL BE REPAIRED 
- [SDR CA100809010](https://openairdocs.org/sdr/CA100809010), Aug 6, 2010: MOUNT. CRACKED. (CAN) ENGINE MOUNT CRACKED AT 2 PIECE ATTACH FOOTING. CRACK IDENTIFIED BY VISUAL INSPECTION AS PER SB1103C. THIS IS THE 31ST ENGINE MOUNT WITH SUCH FAILURE THRO
- [SDR CA100809011](https://openairdocs.org/sdr/CA100809011), Jul 19, 2010: MOUNT. CRACKED. (CAN) CRACK AND CORROSION LEADING TO TUBE DETERIORATION IMMEDIATELY ABOVE THE LANDING GEAR ACTUATOR ATTACHEMENT POINT. NOTE: THIS IS THE "ONE PIECE" STYLE FOOT 
- [SDR CA100809013](https://openairdocs.org/sdr/CA100809013), Jul 7, 2010: MOUNT. BROKEN. (CAN) CUSTOMER MOUNT WAS SENT IN WITH CRACK IN LANDING GEAR ATTACHMENT. THIS IS THE 29TH ENGINE MOUNT WITH THIS DEFECT TO COME THROUGH OUR SHOP. REPLACEMENT ENG
- [SDR 2009FA0000907](https://openairdocs.org/sdr/2009FA0000907), Sep 14, 2009: TUBE. DETERIORATED. THE TUBING COVERING THE FUEL QUANTITY WIRING INSIDE THE WING HAS DETERIORATED. SOME SMALL PIECES WERE FOUND NEAR THE WING STRAINERS. THE CONDITION WAS FIRST DIS
- [SDR CA090505001](https://openairdocs.org/sdr/CA090505001), May 1, 2009: HINGE BRACKET. LOOSE. (CAN) AS PART OF A 500 HR AILERON BEARING INSP, IT WAS NOTICED THAT THE AILERON HINGES WERE LOOSE WHERE THEY ATTACHED TO THE BRACKETS THAT ATTACHED THEM TO THE 
- [SDR CA090310009](https://openairdocs.org/sdr/CA090310009), Mar 6, 2009: ROD BEARING. BROKEN. (CAN) ENG RECEIVED FOR CYL CHANGE, FOUND CAMSHAFT WITH SOME PITS. ON DISASSEMBLY OF ENG TO REPAIR CAMSHAFT FOUND NR 4 CONNECTING ROD BRG SHELL ON ROD END SPLIT 
- [SDR 2008FA0000097](https://openairdocs.org/sdr/2008FA0000097), Dec 26, 2007: CRANKSHAFT. BROKEN. CRANKSHAFT BROKE JUST AFT OF PROPELLER MOUNTNG FLANGE. (K)
- [SDR 2007FA0000948](https://openairdocs.org/sdr/2007FA0000948), Oct 24, 2007: CENTERING MECH. FAILED. UPON TOUCHDOWN AIRCRAFT VEERED LT ABRUPTLY AND DEPARTED RUNWAY SURFACE. GEAR EXTENSION AND INDICATION WERE NORMAL. INVESTIGATION REVEALED THAT UPON TOUCHDOWN TH
- [SDR R019692](https://openairdocs.org/sdr/R019692), May 19, 2006: ROD. WORN. THE AREA OF THE PITCH CHANGE ROD THAT IS GUIDED THROUGH THE ENGINE SIDE HUB HALF BORE HAS WORN THROUGH THE CHROME PLATING BEFORE FIRST OVERHAUL.
- [SDR 2005FA0001045](https://openairdocs.org/sdr/2005FA0001045), Jul 8, 2005: COLLECTOR RING. DEFECTIVE. THIS IS THE COLLECTOR THAT MOUNTS TO THE TOP OF THE LT TURBO. FOUND HOLES ON BOTH SIDES OF WELDS ON THE AFT END NEAR THE SMALL BALANCE TUBE. (K)
- [SDR 2005FA0001011](https://openairdocs.org/sdr/2005FA0001011), Jun 10, 2005: POINTS. BROKEN. CONTACT SPRING BROKNE IN 311.1 HOURS OF OPERATION. (K)
- [SDR 2005FA0001010](https://openairdocs.org/sdr/2005FA0001010), Jun 10, 2005: POINTS. BROKEN. CONTACT SPRING BROKEN IN 300.7 HRS OF OPERATION. (K)
- [SDR CA040326006](https://openairdocs.org/sdr/CA040326006), Mar 23, 2004: MOUNT. CRACKED. (CAN) ENGINE MOUNT CRACKED AT AREA DESCRIBED IN MFG SB NR 1103 REV.B NOTE: THIS SHOULD BE NOTIFIED TO ALL OWNERS BY AN AIRWORTHINESS DIRECTIVE.
- [SDR 2004FA0000052](https://openairdocs.org/sdr/2004FA0000052), Jan 9, 2004: FITTING. LOOSE. DURING A RECENT INSPECTION IT WAS NOTED THAT THE LOCK FASTENERS SECURING THE STEEL LOWER ENGINE MOUNT ATTACH FITTINGS, INBOARD AND OUTBOARD, TO THE FUSELAGE WER
- [SDR 2004FA0000051](https://openairdocs.org/sdr/2004FA0000051), Jan 9, 2004: FASTENER. LOOSE. DURING A RECENT INSPECTION IT WAS NOTED THAT ALL OF THE LOCK FASTENERS THAT SECURE THE STEEL ATTACH FITTINGS TO THE AIRFRAME FOR THE ENGINE MOUNT LOWER ATTACH P
- [SDR CA030828002](https://openairdocs.org/sdr/CA030828002), Aug 20, 2003: EXHAUST VALVE. BROKEN. (CAN) CRUISING AT 25,000 FT, MANIFOLD PRESS DROPPED BY 5 INCHES, DID NOT RECOVER UNTIL BELOW 10,000 FT. MAINT CHECKS ON GROUND DETERMINED NO (ZERO) COMPRESS ON 
- [SDR AUS20030446](https://openairdocs.org/sdr/AUS20030446), Apr 10, 2003: CRANKSHAFT. CRACKED. (AUS) CRANKSHAFT CRACKED RADIALLY IN AREA LOCATED BEHIND THE PROPELLER FLANGE. CRACK LENGTH APPROXIMATELY 50.8MM (2IN).
- [SDR SL52003F00000](https://openairdocs.org/sdr/SL52003F00000), Apr 2, 2003: EXHAUST GATE. CRACKED. DURING MAINTENANCE, CHECKING EXHAUST FOR POSSIBLE LEAKS, FOUND RIGHT HAND EXHAUST TEE ABOVE RIGHT TURBOCHARGER CRACKED HALF WAY AROUND, THE CRACK IS NOT VISIBLE
- [SDR ZKG2003F00002](https://openairdocs.org/sdr/ZKG2003F00002), Feb 24, 2003: BELLCRANK. BROKEN. PILOT REPORTED A ROLL OF THE AIRCRAFT WHEN THE FLAPS WERE SELECTED DOWN, INSPECTION FOUND LEFT FLAP BELLCRANK BROKEN. THE FAILED PART WAS PREVOUSLY INSPECTED IA
- [SDR 2002FA0001379](https://openairdocs.org/sdr/2002FA0001379), Nov 20, 2002: COLLAR. LOOSE. LEFT WING REAR ATTACH FITTING COLLAR FOUND IN RECESS BELOW FITTING. RIVET LOOSE IN HOLE. REPLACED WITH OVERSIZE FASTENER AND TORQUED COLLAR. DISCOVERED DURING A
- [SDR ECWR200201](https://openairdocs.org/sdr/ECWR200201), Jun 25, 2002: SCREEN. FAILED. INDUCTION AIR FILTER METAL PROTECTIVE SCREEN FAILED AND THE METAL FROM THE SCREEN WAS INDUCTED INTO THE TURBOCHARGER ASSEMBLY AND INTAKE AIR OF THE ENGINE. THE 
- [SDR 200202](https://openairdocs.org/sdr/200202), Jun 6, 2002: RELAY. CHAFED. DURING AVIONICS TROUBLE SHOOTING, AN INSPECTION PANEL WAS REMOVED FROM THE COCKPIT FLOOR IN THE AREA JUST FORWARD OF THE CO PILOT'S SEAT TO GAIN ACCESS TO A SWI
- [SDR 2002FA0000682](https://openairdocs.org/sdr/2002FA0000682), May 15, 2002: VALVE. BROKEN. DE-ICE BOOTS INOPERATIVE, FOUND AIRBORN MANIFOLD VALVE BROKEN IN TWO.
- [SDR 2002FA0000180](https://openairdocs.org/sdr/2002FA0000180), Jan 24, 2002: MAGNETO. FAILED. PILOT REPORTED FAILED RT MAGNETO. REMOVED MAGNETO FROM ENGINE AND DISASSEMBLED. FOUND ONE OF THE COIL ANCHOR WEDGES WAS DISPLACED AND HAD MIGRATED ONTO THE SECO
- [SDR 2001FA0000128](https://openairdocs.org/sdr/2001FA0000128), Jul 11, 2001: ROD. CORRODED. ELEVATOR PUSH PULL CONTROL ROD VERY RUSTY AND PITTED. LOCATED IN TAIL SECTION WHERE MOISTURE AND CONTAMINATION ACCUMULATE.
- [SDR SW15200111824](https://openairdocs.org/sdr/SW15200111824), Apr 25, 2001: KNOB. INOPERATIVE. MANUAL OVER RIDE (MOR) CONTROL LEVER KNOB CAME APART CAUSING THIS SYSTEM TO BE RENDERED INOPERATIVE AND A CERTAIN SAFETY ISSUE. PROBLEM CAN BE SOLVED WITH PROPE
- [SDR 2001F00048](https://openairdocs.org/sdr/2001F00048), Jan 6, 2001: MOUNT. DAMAGED. FOUND ENGINE CONTROL CABLES CHAFFING ON THE ENGINE MOUNT DURING ENGINE CHANGE. DAMAGE WAS FOUND TO BE BEYOND LIMITS. SENT MOUNT FOR REPAIR. ENGINE MOUNT WAS FOU
- [SDR 20000802SH017](https://openairdocs.org/sdr/20000802SH017), Jun 26, 2000: ROD END. CORRODED. DURING ANNUAL INSPECTION, TUBE WAS FOUND WITH EXTERIOR CORROSION ON BOTTOM AFT SURFACE. FLAKED OFF LOOSE PAINT FOUND A DEEP PIT. ABLE TO PASS THIS TUBE WITH AN 
- [SDR CA991209064](https://openairdocs.org/sdr/CA991209064), Dec 15, 1999: BOLT. WRONG PART. (CAN) ONE BOGUS PART (HUB BOLT) FOUND.
- [SDR CA991209039](https://openairdocs.org/sdr/CA991209039), Dec 15, 1999: CONTROL SHAFT. CRACKED. (CAN) DURING INSPECTION NDT PROCESS REVEALED A CRACK IN THE CONTROL SHAFT.
- [SDR CA991209040](https://openairdocs.org/sdr/CA991209040), Nov 11, 1999: BLADE. CORRODED. (CAN) CORROSION FOUND UNDERDEICE BOOTS.
- [SDR 99ZZZX2477](https://openairdocs.org/sdr/99ZZZX2477), May 28, 1999: SPRING. WEAK. NOSE GEAR EMERGENCY EXTENSION SPRING UNABLE TO EXTEND NOSE GEAR AND LOCK IN-FLIGHT. AFTER LANDING AND ROLL-OUT ON MAINS HOLDING NOSE OFF, NOSE GEAR LOCKED AT 30
- [SDR 99ZZZX976](https://openairdocs.org/sdr/99ZZZX976), Feb 3, 1999: GEAR DIST. FAILED. PILOT REPORTED LOSS OF POWER AND A ROUGH RUNNING ENGINE. AFTER COMPLETING MAGNETO CHECK, A DEAD LT MAGNETO WAS DISCOVERED. THE MAGNETO WAS DISASSEMBLED AND THE 
- [SDR CA990119044](https://openairdocs.org/sdr/CA990119044), Jan 5, 1999: BOLT. FRACTURED. (CAN) THE NR 2 CYLINDER ROCKER COVER HOLD-DOWN BOLTS BROKE, SENDING INTAKE BOLT UPPER BROKEN HALF THROUGH THE ROCKER COVER. THE CYLINDER WAS REMOVED AND SENT FO
- [SDR AU981663](https://openairdocs.org/sdr/AU981663), Dec 23, 1998: ACTUATOR. LEAKING. (AUS) AFTER TAKEOFF AND LANDING GEAR RETRACTED, THE HYDRAULIC PRESSURE CYCLED AND TRIPPED THE HYDRAULIC MOTOR CIRCUIT BREAKER. THE LANDING GEAR THEN PARTIALLY E
- [SDR AU981655](https://openairdocs.org/sdr/AU981655), Dec 2, 1998: ENGINE. DETERIORATED. (AUS) DURING SCHEDULED ENGINE MAINTENANCE, THE FOLLOWING PROBLEMS WERE FOUND: 1. ENGINE OIL FILTER INSPECTED AND FOUND (EXCESSIVE) HIGH LEVELS OF COPPER. 2. TWO
- [SDR 98ZZZX4224](https://openairdocs.org/sdr/98ZZZX4224), Nov 6, 1998: BELLCRANK. FAILED. ON APPROACH, THE PILOT NOTICED THE RIGHT FLAP DID NOT EXTEND. THE LEFT FLAP WAS PROMPTLY RETRACTED AND A SAFE LANDING WAS MADE WITHOUT INCIDENT. THE INVESTIGATI

All 119: https://openairdocs.org/model/new-piper-pa-46-310p/reports.md

## STCs that may be installed (OpenAirDocs) (185, 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 SA00079NY](https://openairdocs.org/stc/SA00079NY): Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Airwolf Filter 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 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 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 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 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 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 SA1793CE-D](https://openairdocs.org/stc/SA1793CE-D): ONE ONLY STC, SN 46-8508024: Installation of King KNS 660 Multi-Sensor Mangement System. 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 SA03286CH](https://openairdocs.org/stc/SA03286CH): Install an electronic engine ignition system. Electroair Acquisition Corporation
- [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation
- [STC SA00344BO PAGE 2](https://openairdocs.org/stc/SA00344BO%20PAGE%202): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine
- [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation

All 185: https://openairdocs.org/model/new-piper-pa-46-310p/stcs.md

## PMA parts (OpenAirDocs) (573, 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.

- [RAP164-21600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132311683620260722154733.0001): Brake Disc. Rapco Inc. · PMA PQ2101CE · Replaces 164-21600 · Jun 3, 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
- [LA82280C-006-70A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199888817220250624160123.0001): Windshield Assy, RH, CoolView (Alternate). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82342C-005-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183530451620250624160125.0001): Cabin PAX 2 Window Assy, LH, CoolView. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82280C-006-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179943788220250624160123.0001): Windshield Assy, RH, CoolView. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82280C-005-70A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171130128220250624160123.0001): Windshield Assy, LH, CoolView (Alternate). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82399C-003-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161707675820250624160125.0001): Cabin PAX 1 Window Assy, CoolView. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82282C-006-70A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152695061620250624160124.0001): Side Cockpit Window Assy, RH, CoolView(Alternate). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82342C-006-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138755374120250624160125.0001): Cabin PAX 2 Window Assy, RH, CoolView. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82343C-005-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134541685220250624160125.0001): Cabin PAX 3 Window Assy, LH, CoolView. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82282C-005-70A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127139612720250624160124.0001): Side Cockpit Window Assy, LH, CoolView (Alternate). Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 2025
- [LA82343C-006-70](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124138333620250624160125.0001): Cabin PAX 3 Window Assy, RH, CoolView. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jun 15, 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
- [PM-159](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132291242220260625165812.0001): Wing Root Fairing Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 20, 2024
- [PM-15801](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114153999920251118174430.0001): Spinner Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 19, 2024
- [TAU03323](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194359759020240221143039.0001): AV/Cabin Heat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Dec 14, 2023
- [PM-158](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167693801620260625151412.0001): Radome Mask. PM Research, Inc. · PMA PQ10049NE · Modification part · Nov 21, 2023
- [01-7079-24](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168735715720231108124804.0001): LIGHT-ASSY, StarLight. AeroLEDs LLC · PMA PQ5259NM · Replaces WA7079B-24NLI7079-24CMA-7079B-24A7079B… · Nov 3, 2023
- [APS68-01100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102488499820231102131426.0001): Shim, Brake. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 068-01100 · Sep 25, 2023
- [UAV-1004236-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179059944320230707211347.0001): AV-30-C. uAvionix Corporation · PMA PQ05445NM · Modification part · Jun 28, 2023
- [130360-21     Series 1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149025992020230807135214.0001): Controller, Outflow Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 557-120 · Oct 18, 2022
- [103638-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128790278820230807135212.0001): Outflow/Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 491-814 · Oct 18, 2022
- [103638-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105017981120230807135213.0001): Outflow/Safety Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 491-815 · Oct 18, 2022
- [131358-2       Series 1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101089586520230807135215.0001): Tank Auxiliary. Honeywell International Inc. · PMA PQ1222NM · Replaces 488-136 · Oct 18, 2022
- [APS177-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156099139020221020170337.0001): Pin. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 177-00300 · Aug 10, 2022
- [APS66-06200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138096606220221020170231.0001): Brake Lining. Aviation Products Systems Inc · PMA PQ3830CE · Replaces 066-06200 · Aug 10, 2022
- [AAG5-002](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID114268233020220811111805.0001): G5 Adapter Plate. Affordable Aviation LLC · PMA PQ05456NM · Replaces Garmin 115-02733-00 · Aug 2, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147881494420220706160211.0001): Whelen Aerospace Technologies · PMA PQ1372CE · Jun 21, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157614225820220809130916.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · May 10, 2022
- [EA-21000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183329600120220525194246.0001): Six-Cylinder Ignition Controller. Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127739023220220525194408.0001): Controller Wire Harness (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [EA-22000T](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118228368520220525194520.0001): Controller Wire Harness- Twin (14 Pin). Electroair Acquisition Corporation · PMA PQ4141CE · Modification part · Apr 25, 2022
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157547472220220809102546.0001): Aviation Devices & Electronic Components LLC (Av-DEC) · PMA PQ3846SW · Apr 18, 2022
- [AG844000-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199521739920220408135804.0001): Gasket – UHF/VHF Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Feb 8, 2022
- [AG728000-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101036313520220408135725.0001): Gasket – Satcom Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Jan 26, 2022
- [AA15-1936](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151669776202203081423550.0001): Induction Air Filter. Aero Accessories LLC · PMA PQ1206CE · Replaces DonaldsonP15-1936Piper561-020PS60007-3 · Jan 3, 2022
- [AG627000-23](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161079392020220408135703.0001): Gasket – Marker Beacon. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Dec 15, 2021
- [AG627000-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132314489920220408140242.0001): Gasket – Marker Beacon Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [AG358000-08](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108986355720220408135816.0001): Gasket – ELT Antenna. Aviation Devices & Electronic Components, LLC · PMA PQ03846SW · Modification part · Nov 17, 2021
- [89000023-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171375598920240229155304.0001): Final Assembly KG 71 Air Data Attitude and Heading Reference System (ADHRS). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000020-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151329495120240229155258.0001): Final Assembly KSD 100 Primary Flight Display (PFD). Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140327588020240229155314.0001): Final Assembly KCP 100 Control Panel(Landscape)e. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [89000026-001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106818448820240229155309.0001): Final Assembly KCP 100 Control Panel. Honeywell International Inc. (BendixKing) · PMA PQ05457NM · Modification part · Nov 15, 2021
- [MC155-00100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID984820721220211021173450.0001): Retaining Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 155-00100, 155-1, 3023, 752-830 · Sep 9, 2021
- [MC153-00400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID766003383420211021173337.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-004, 153-00400, 153-4, 3022… · Sep 9, 2021
- [MC153-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID734520878120211021173334.0001): Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 153-00300, 755-929, A39070 · Sep 9, 2021
- [MC154-00300](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID715924487820211021173415.0001): Felt. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 154-00300, 154-3, 3021, 751-772 · Sep 9, 2021
- [MC155-11800](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID656668920520211021173509.0001): Retaining Ring. McFarlane Aviation Inc · PMA PQ3732CE · Replaces 155-11800, 762-561, A-1636-23 · Sep 9, 2021

All of them: https://openairdocs.org/model/new-piper-pa-46-310p/pma.md

## The same model under other registry codes

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

- [Piper PA-46-310P](https://openairdocs.org/model/piper-pa-46-310p): 211 registered aircraft, registry code 7104605
- [Piper PA-46-310P](https://openairdocs.org/model/piper-pa-46-310p): 2 registered aircraft, registry code 7104611
- [Piper PA-46-310P](https://openairdocs.org/model/piper-pa-46-310p): 1 registered aircraft, registry code 7104624

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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.