# AiResearch TPE331-8 series

- Type: Engine model (FAA registry)
- Registry code: 01530
- Manufacturer (registry): AIRESEARCH
- Model: TPE331-8 SER
- Engine type: Turbo-prop
- Power: 715 hp
- Data sheet: [TCDS E4WE](https://openairdocs.org/tcds/E4WE) (OpenAirDocs)
- Holder: Honeywell Aerospace US LLC
- Installed in: 4 registered aircraft
- Page: https://openairdocs.org/engine/airesearch-tpe331-8-series

The registry names only the engine series, so ADs for every model in the series are matched.

## ADs that may apply (OpenAirDocs)

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

- [AD 2018-22-01](https://openairdocs.org/ad/2018-22-01): Turbine Section · Honeywell International TPE331-10, TPE331-10N, TPE331-10R and 8 more. Effective Dec 10, 2018
- [AD 2018-17-15](https://openairdocs.org/ad/2018-17-15): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 39 more. Effective Oct 22, 2018
- [AD 2018-13-05](https://openairdocs.org/ad/2018-13-05): Turbine Engine Reduction Gear · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 18 more. Effective Jul 26, 2018
- [AD 2016-18-17](https://openairdocs.org/ad/2016-18-17): Compressor impeller · Honeywell International TPE331-10, TPE331-10AV, TPE331-10GP and 22 more. Effective Nov 4, 2016
- [AD 2011-18-51 R1](https://openairdocs.org/ad/2011-18-51-R1): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more. Effective Oct 19, 2011
- [AD 2006-14-03](https://openairdocs.org/ad/2006-14-03): New flight cycle counting method for first, second, and third-stage turbine rotors · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 48 more. Effective Aug 9, 2006
- [AD 2002-25-02](https://openairdocs.org/ad/2002-25-02): First stage compressors implellers · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 35 more. Effective Jan 21, 2003
- [AD 2001-21-02](https://openairdocs.org/ad/2001-21-02): Airplane Flight Manual--Electronic Engine Controls · Honeywell International TPE331-10N, TPE331-12B and TPE331-8. Effective Nov 19, 2001
- [AD 98-12-09](https://openairdocs.org/ad/98-12-09): Fuel Manifold · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more. Effective Aug 7, 1998
- [AD 95-16-08](https://openairdocs.org/ad/95-16-08): Life Limited Turbine Components · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 62 more. Effective Sep 5, 1995
- [AD 93-15-11](https://openairdocs.org/ad/93-15-11): Propeller Pitch Control (PPC) Gasket · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 58 more. Effective Sep 7, 1993
- [AD 89-07-07 R1](https://openairdocs.org/ad/89-07-07-R1): Oil Scavenge Pump Assembly · Honeywell International TPE331-1, TPE331-10, TPE331-10R and 26 more. Effective Oct 30, 1989

Historical (superseded or no longer in force):

- [AD 2018-02-14](https://openairdocs.org/ad/2018-02-14) (historical): Turbine Engine Combustion Section · Honeywell International TPE331-1, TPE331-10, TPE331-10AV and 38 more. Effective Feb 28, 2018
- [AD 2011-18-51](https://openairdocs.org/ad/2011-18-51) (historical): Main shaft bearing · Honeywell International TPE331-1, TPE331-10, TPE331-10A and 82 more
- [AD 92-02-19 PL](https://openairdocs.org/ad/92-02-19-PL) (historical): Fuel Manifold Assembly Leak · Honeywell International TPE331-10, TPE331-10A, TPE331-10AV and 29 more

## Information bulletins (advisory) (1)

- [SAIB NE-16-18](https://openairdocs.org/saib/NE-16-18): Power Lever  Loss of Power Control. Issued Jul 11, 2016

## Registered aircraft (4)

- [N14FJ](https://openairdocs.org/aircraft/N14FJ): [Land Safely LLC](https://openairdocs.org/faa-owner/LAND%20SAFELY%20LLC), [Tinton Falls, NJ](https://openairdocs.org/faa-place/NJ/Tinton%20Falls), built 1980, S/N 441-0118
- [N152AF](https://openairdocs.org/aircraft/N152AF): [Uas Transervices Inc](https://openairdocs.org/faa-owner/UAS%20TRANSERVICES%20INC), [Boca Raton, FL](https://openairdocs.org/faa-place/FL/Boca%20Raton), built 1982, S/N AC520
- [N441BF](https://openairdocs.org/aircraft/N441BF): [Amt Services Leasing Co Inc](https://openairdocs.org/faa-owner/AMT%20SERVICES%20LEASING%20CO%20INC), [Colorado Springs, CO](https://openairdocs.org/faa-place/CO/Colorado%20Springs), S/N 441-0145
- [N441MJ](https://openairdocs.org/aircraft/N441MJ): [Gw Aviation LLC](https://openairdocs.org/faa-owner/GW%20AVIATION%20LLC), [Woods Cross, UT](https://openairdocs.org/faa-place/UT/Woods%20Cross), built 1978, S/N 441-0024

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (1)

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 20200723009989I](https://openairdocs.org/incident/20200723009989I), Jul 23, 2020: Cessna 441 (N14FJ), Ocean City, MD, Minor damage. On 7/23/2020 at approximately 2:30 pm local time [privacy data omitted] was conducting a landing on runway 32 at the Ocean City Municipal Airport. Shortly…

## Service difficulty reports (89, newest 50)

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

- [SDR DSCR20151005001](https://openairdocs.org/sdr/DSCR20151005001), Sep 24, 2015: RELIEF VALVE. FRACTURED. DURING CRUISE PHASE OF FLIGHT, THE RT ENG EXPERIENCED LOSS OF FUEL PRESS. PILOT SHUT THE RT ENG DOWN, CONTACTED ATC & WAS DIVERTED. TECHNICIANS INSPECTED THE EN
- [SDR 5XWR201307110363](https://openairdocs.org/sdr/5XWR201307110363), Jul 11, 2013: STRUCTURE. MISOVERHAULED. PERFORMED A PHASE 2, 3, & D, TASK A361004, BLEED AIR LINE EXHIBITED CORROSION WHERE ITS FLANGE FASTENS TO THE FUSELAGE SKIN BS 187.87 RBL 27, AND WL 62.79. ON D
- [SDR CA080304011](https://openairdocs.org/sdr/CA080304011), Jan 18, 2008: ACTUATOR. FAILED. (CAN) AIRCRAFT INDICATED (3 GREEN) ON APPROACH, UPON LANDING, NOSE GEAR RETRACTED RESULTING IN AC DAMAGE. UPON ARRIVAL, MAINT NOTED GEAR INDICATION REMAINED (3 
- [SDR AU510001538](https://openairdocs.org/sdr/AU510001538), Dec 12, 2005: TENSIONER. SHEARED. HF ANTENNA SUPPORT AND TENSION UNIT SNAPPED AT ANTENNA CONNECTION TO VERTICAL STABILIZER.
- [SDR AU510001559](https://openairdocs.org/sdr/AU510001559), Dec 12, 2005: ACTUATOR. FAULTY. RT MAIN LANDING GEAR NIL DOWN INDICATION.
- [SDR AU510001724](https://openairdocs.org/sdr/AU510001724), Dec 12, 2005: RIVET. CRACKED. ELEVATOR LT OUTBOARD HINGE BRACKET ATTACHMENT RIVET HEAD CRACKED. FOUND DURING INSPECTION IAW AD/C400/102 AMDT3.
- [SDR AU510001767](https://openairdocs.org/sdr/AU510001767), Dec 12, 2005: CAP. CRACKED. (AUS) RT WING CANTED RIB CAP CRACKED. CRACK LENGTH APPROXIMATELY 40MM (1.574IN). CRACK WAS LOCATED IN THE RADIUS OF THE UPPER CAP AND TRAVELLED REARWARDS FROM T
- [SDR AU510001768](https://openairdocs.org/sdr/AU510001768), Dec 12, 2005: BRACKET. CRACKED. (AUS) LT ELEVATOR OB HINGE ASSY IB ATTACHMENT BRACKET CRACKED IN LOWER FORWARD RADIUS. FOUND DURING INSPECTION IAW AD/C400/102 AMDT 3 PART 3. BOTH LT AND RT ELE
- [SDR AU510001769](https://openairdocs.org/sdr/AU510001769), Dec 12, 2005: BULB. BURNED OUT. (AUS) RT MAIN LANDING GEAR POSITION INDICATOR LIGHT BULB BLOWN. (CASA NR 510001769)
- [SDR AU510001776](https://openairdocs.org/sdr/AU510001776), Dec 12, 2005: RIB. CRACKED. LT WING ROOT CANTED RIB UPPER CAP LOCATED AT CWS 26.85 CRACKED.
- [SDR AU510001885](https://openairdocs.org/sdr/AU510001885), Dec 12, 2005: RIB. CRACKED. RT CANTED RIB CAP CRACKED BENEATH REPAIR.
- [SDR AU510001886](https://openairdocs.org/sdr/AU510001886), Dec 12, 2005: RIB. CRACKED. RT CANTED RIB CAP FORWARD PN 5720001-4S AND AFT PN 5720001-6S ANGLES CRACKED, FOUND DURING EDDY CURRENT INSPECTION.
- [SDR AU510001944](https://openairdocs.org/sdr/AU510001944), Dec 12, 2005: GOVERNOR. FAULTY. (AUS) RT ENGINE PROPELLER GOVERNOR FAULTY. INVESTIGATION CONTINUING. (CASA NR 510001944)
- [SDR AU510001993](https://openairdocs.org/sdr/AU510001993), Dec 12, 2005: ALTIMETER. FAILED. ENCODING ALTIMETER FAILED.
- [SDR AU510002026](https://openairdocs.org/sdr/AU510002026), Dec 12, 2005: ENGINE. SEIZED. RT ENGINE SEIZED. INVESTIGATION CONTINUING.
- [SDR AU510002156](https://openairdocs.org/sdr/AU510002156), Dec 12, 2005: DOOR. SEPARATED. LT FORWARD NOSE LOCKER SEPARATED FROM AIRCRAFT SEVERING BOTH HINGES. ONE BAG LOST OVERBOARD. DOOR STRUCK PROPELLER CAUSING A TORQUE SHIFT IN THE ENGINE. LT ENGI
- [SDR AU510002181](https://openairdocs.org/sdr/AU510002181), Dec 12, 2005: ACM. FAILED. AIR CYCLE MACHINE (ACM) FAILED AND EMERGENCY PRESSURISATION VALVE AUTOMATICALLY OPENED.
- [SDR AU510002089](https://openairdocs.org/sdr/AU510002089), Oct 11, 2005: SKIN. CRACKED. UPPER AFT RT NACELLE SKIN CRACKED AND CORRODED.
- [SDR AU510001809](https://openairdocs.org/sdr/AU510001809), Feb 9, 2005: RIB. CRACKED. LT WING UPPER FORWARD PN 572001-3S AND AFT PN 572001-5S DRAG ANGLES CRACKED. FOUND DURING EDDY CURRENT INSPECTION IAW CQB03-1 REV 1. EDDY CURRENT INSPECTION REV
- [SDR AUS20040448](https://openairdocs.org/sdr/AUS20040448), May 21, 2004: SELECTOR VALVE. FAULTY. (AUS) LANDING GEAR SELECTOR VALVE SOLENOID FAILED.
- [SDR AUS20040447](https://openairdocs.org/sdr/AUS20040447), May 17, 2004: O-RING. DAMAGED. (AUS) NOSE LANDING GEAR UPLOCK ACTUATOR O-RING DAMAGED. HYDRAULIC FLUID LEAKING FROM ACTUATOR BODY.
- [SDR AUS20040368](https://openairdocs.org/sdr/AUS20040368), Apr 29, 2004: BOOT. FAILED. (AUS) RT WING OUTER DE-ICE BOOT BURST AT THE UPPER SEAM AND SPLIT FOR THE ENTIRE LENGTH FROM THE OB RT NACELLE TO THE WINGTIP.
- [SDR AUS20040324](https://openairdocs.org/sdr/AUS20040324), Apr 27, 2004: WIRE. WORN. (AUS) RT FUEL TANK QUANTITY WIRE CHAFED ON STRINGERS LOCATED AT STATION PWS 61.80.
- [SDR AUS20040327](https://openairdocs.org/sdr/AUS20040327), Apr 24, 2004: PUMP. CRACKED. (AUS) ENGINE OIL PUMP HOUSING CRACKED.
- [SDR AUS20040333](https://openairdocs.org/sdr/AUS20040333), Apr 21, 2004: VALVE. LEAKING. (AUS) START FUEL VALVE LEAKING BETWEEN VALVE BODY AND SOLENOID.
- [SDR AUS20040183](https://openairdocs.org/sdr/AUS20040183), Mar 8, 2004: PIPE. CRACKED. (AUS) HYDRAULIC PIPE CRACKED AND LEAKING. LOSS OF HYDRAULIC FLUID. PIPE IS LOCATED IN RT WING LEADING EDGE. INVESTIGATION FOUND TOOLING MARKS ON THE PIPE IN THE
- [SDR AUS20040128](https://openairdocs.org/sdr/AUS20040128), Feb 24, 2004: SWITCH. OUT OF ADJUST. (AUS) LT MAIN LANDING GEAR UPLOCK SWITCH OUT OF ADJUSTMENT. MICROSWITCH WAS SWITCHING OFF LOADING VALVE BUT NOT THE IN TRANSIT LIGHT. INVESTIGATION FOUND SOME W
- [SDR CA040220007](https://openairdocs.org/sdr/CA040220007), Feb 18, 2004: VALVE. FAILED. (CAN) DURING THE CLIMB THE AIRCRAFT EMERGENCY PRESSURIZATION VALVE OPENED WITH OUT BEING SELECTED. THE CREW DEPRESSURIZED THE AIRCRAFT AND RETURNED TO BASE. THE
- [SDR AUS20040076](https://openairdocs.org/sdr/AUS20040076), Feb 11, 2004: SPAR. DEBONDED. (AUS) LT WING SPAR WEB DISBONDED IN AREA LOCATED AT CWS 57.
- [SDR AUS20040037](https://openairdocs.org/sdr/AUS20040037), Jan 21, 2004: BRACKET. CRACKED. (AUS) LT WING OB AILERON ATTACHMENT BRACKET CRACKED. INVESTIGATION FOUND INDICATIONS OF SURFACE INTERGRANNULAR CORROSION AND CONFIRMATION OF A CRACK LOCATED APP
- [SDR AUS20031313](https://openairdocs.org/sdr/AUS20031313), Dec 16, 2003: SEAL. LEAKING. (AUS) RT ENGINE COMPRESSOR SEAL SUSPECT FAULTY. LEAKING OIL CAUSED SMOKE IN COCKPIT.
- [SDR AUS20031179](https://openairdocs.org/sdr/AUS20031179), Nov 14, 2003: TIRE. DEFLATED. (AUS) RT MAIN LANDING GEAR TIRE, DEFLATED DURING LANDING ROLL.
- [SDR AUS20030552](https://openairdocs.org/sdr/AUS20030552), Jun 4, 2003: WEB. CRACKED. (AUS) BEAM WEB CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).
- [SDR AUS20030595](https://openairdocs.org/sdr/AUS20030595), Jun 4, 2003: BEAM. CRACKED. (AUS) BEAM WEB CRACKED. CRACK LENGTH APPROXIMATELY 25.4MM (1IN).
- [SDR AUS20030485](https://openairdocs.org/sdr/AUS20030485), Apr 26, 2003: BOLT. MISSING. (AUS) MAIN WHEEL BRAKE DISC RETAINING BOLTS (3OFF) MISSING AND FIVE BOLTS LOOSE.
- [SDR CA030421010](https://openairdocs.org/sdr/CA030421010), Dec 21, 2002: BEARING. FAILED. (CAN) STARTER GEN WAS HAVING NEW BRUSHES SEATED AT MID-TBO USING GEN DRIVESTAND METHOD.APPRX 3 HRS INTO THE PROCESS, THE ANTI-DRIVE END BEARING FAILED COMPLETEL
- [SDR AUS20021376](https://openairdocs.org/sdr/AUS20021376), Nov 6, 2002: VALVE. FAILED. (AUS) EMERGENCY PRESSURISATION VALVE FAILED.
- [SDR AUS20021305](https://openairdocs.org/sdr/AUS20021305), Aug 28, 2002: SOLENOID. LEAKING. (AUS) LT ENGINE PRIMARY-ONLY SOLENOID LEAKING FROM VALVE BODY.
- [SDR AUS20020943](https://openairdocs.org/sdr/AUS20020943), Aug 19, 2002: BOOT. SPLIT. (AUS) LEADING EDGE DE-ICE BOOT SPLIT LONGITUDINALLY.
- [SDR AUS20020792](https://openairdocs.org/sdr/AUS20020792), Jul 16, 2002: VALVE. FAILED. (AUS) RT ENGINE PRIMARY FUEL SOLENOID VALVE FAULTY. INVESTIGATION FOUND THE OPERATING COIL SHORT CIRCUITED TO EARTH.
- [SDR CA020611001](https://openairdocs.org/sdr/CA020611001), Jun 10, 2002: WIRE HARNESS. CHAFED. (CAN) DURING INSPECTION AND COMPLYING WITH AD 2002-09-13 AND CESSNA SERVICE BULLITEN CQB02-1 REV. 1, FOUND THAT THE BLACK WIRE IN THE HARNESS WAS CHAFED THROUGH
- [SDR AUS20020577](https://openairdocs.org/sdr/AUS20020577), Jun 4, 2002: PUMP. FAILED. (AUS) LT ENGINE TORQUE FLUCTUATIONS. METAL CONTAMINATION OF OIL FILTER AND CHIP DETECTOR. SUSPECT CAUSED BY FAILURE OF OIL SCAVENGE PUMP.
- [SDR AUS20020530](https://openairdocs.org/sdr/AUS20020530), May 31, 2002: WIRE HARNESS. CHAFED. (AUS) FUEL BOOST PUMP WIRING HARNESSES CHAFED. FOUND DURING INSPECTION IAW AD/CESSNA400/111 (SB CQB02-1R1).
- [SDR AUS20020464](https://openairdocs.org/sdr/AUS20020464), May 13, 2002: HARNESS. WORN. (AUS) LT FUEL BOOST PUMP WIRING HARNESS CHAFED. FOUND DURING INSPECTION IAW SB CQB02-1.
- [SDR AUS20020453](https://openairdocs.org/sdr/AUS20020453), May 9, 2002: FASTENER. MISINSTALLED. (AUS) CHERRY RIVETS IN FUSELAGE EMERGENCY EXIT DOOR CUTOUT FRAMEPREVENTING OPERATION OF EMERGENCY EXIT.
- [SDR AUS20020408](https://openairdocs.org/sdr/AUS20020408), May 4, 2002: HARNESS. CHAFED. (AUS) LT FUEL TANK HARNESS WIRE CHAFFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.
- [SDR AUS20020409](https://openairdocs.org/sdr/AUS20020409), May 3, 2002: HARNESS. CHAFED. (AUS) RT FUEL TANK HARNESS WIRE CHAFED BUT WITHIN ACCEPTABLE LIMITS OF SB CQB02-1. HARNESS MODIFIED IAW SB AND REINSTALLED.
- [SDR AUS20020323](https://openairdocs.org/sdr/AUS20020323), Mar 27, 2002: PUMP. CRACKED. (AUS) LT ENGINE OIL PRESSURE PUMP CRACKED.
- [SDR AUS20020263](https://openairdocs.org/sdr/AUS20020263), Mar 12, 2002: PUSHROD. CRACKED. (AUS) LT AILERON TRIM TAB PUSH ROD AFT ROD END CRACKED ACROSS BEARING RETAINER. RODEND BEARING CORRODED. CRACK FOUND WHEN PUSHROD WAS REMOVED FOR REPLACEMENT DU
- [SDR AUS20020043](https://openairdocs.org/sdr/AUS20020043), Jan 22, 2002: BEARING. FAILED. (AUS) LT OUTBOARD FLAP INBOARD BELLCRANK BEARING HAD EXCESSIVE PLAY. SUSPECT CAUSED BY WATER INGRESS.

All 89: https://openairdocs.org/engine/airesearch-tpe331-8-series/reports.md

## STCs that may be installed (OpenAirDocs) (3)

Approved for this engine 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 SE03035AT](https://openairdocs.org/stc/SE03035AT): Installation of Royal Atlantic Aviation Engine Oil Filter Bypass Warning System, Kit P/N RAA2003-1-1. Reds Aircraft Service Inc
- [STC SE00265AT](https://openairdocs.org/stc/SE00265AT): Install Ayres Fuel Manifold Purge Assembly Kit, P/N 21757-1 in accordance with "Installation Instructions - Ayres P/N 21757-1 Fuel Manifold Purge Assy-Kit" Dwg. No. 21757-1(1), Revision none, dated April 20, 1993, or later FAA approved revision. Thrush Aircraft Inc
- [STC SE2924SO](https://openairdocs.org/stc/SE2924SO): Installation of Garrett TPE-331-10 combustor and turbine in the TPE331-8 engine. National Flight Lakeland

## PMA parts (OpenAirDocs) (187, 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 engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [S9413-114WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144043282220261009134010.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-114 · Oct 1, 2026
- [3101373-1HP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126059261820250813163423.0001): Lock Plate. Central Texas Aircraft Parts (CTAP) · PMA PQ0880SW · Replaces 3101373-1 · Aug 7, 2025
- [1010-808ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186320971520240926215357.0001): Washer. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1010-808 · Sep 5, 2024
- [3003-348ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133544675020240926215358.0001): Shim. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3003-348 · Sep 5, 2024
- [3210-100ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109913645120240926215358.0001): Washer. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3210-100 · Sep 5, 2024
- [AAP-1410- 628](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176846208520240515131435.0001): Thrust Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Woodward P/N: 1410-628 used in… · May 6, 2024
- [AAP-1415- 336](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136948528220240424190520.0001): Thrust Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Woodward P/N: 1415-336 used in… · Apr 17, 2024
- [AAP-1415- 336](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111511963520240424190519.0001): Thrust Bearing. Approved Air Parts Co Inc · PMA PQ4173NE · Replaces Woodward P/N: 1415-336 used in… · Apr 17, 2024
- [3103365-1ANB](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153947124120250430234712.0001): Screen. ANB Aviation of CT, LLC · PMA PQ10055NE · Replaces 3103365-1 · Feb 15, 2024
- [S9413-012WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164716779820240919135854.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-012 · Sep 11, 2023
- [182662ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109141066520220523181049.0001): Packing, Preformed. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 182662 · Apr 8, 2022
- [2118250-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186433805520230727204705.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118250-2 · Mar 8, 2022
- [2117420-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184114086320230727204701.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2117420-3 · Mar 8, 2022
- [2101322-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183301110720230727204657.0001): Electronic Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101322-15 · Mar 8, 2022
- [2101322-14](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181206374420230727204656.0001): Electronic Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101322-14 · Mar 8, 2022
- [2118600-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178945110720230727204707.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118600-3 · Mar 8, 2022
- [2117700-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID159584220120230727204702.0001): Integrated Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2117700-4 · Mar 8, 2022
- [2118600-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID154125286620230727204708.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118600-4 · Mar 8, 2022
- [2101826-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149262360420230727204658.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101826-3 · Mar 8, 2022
- [2117420-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136784847620230727204700.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2117420-1 · Mar 8, 2022
- [2118356-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129256531020230727204706.0001): Electronic Engine Control. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118356-1 · Mar 8, 2022
- [2118724-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123850908720230727204709.0001): Integrated Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118724-2 · Mar 8, 2022
- [2117868-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122037585620230727204703.0001): Memory Module. Honeywell International Inc. · PMA PQ1222NM · Replaces 2117868-1 · Mar 8, 2022
- [2101990-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111913565620230727204659.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101990-3 · Mar 8, 2022
- [2118042-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111660216320230727204704.0001): Single Red Line Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118042-2 · Mar 8, 2022
- [2101322-13](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106726957420230727204655.0001): Electronic Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101322-13 · Mar 8, 2022
- [949594-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID105942022120230727204654.0001): Torque and Temp. Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 949594-12 · Mar 8, 2022
- [949594-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID183325598120230727204723.0001): Torque and Temp. Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 949594-9 · Mar 7, 2022
- [949592-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178202395420230727204719.0001): Torque and Temp. Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 949592-5 · Mar 7, 2022
- [949594-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174718865720230727204720.0001): Torque and Temp. Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 949594-5 · Mar 7, 2022
- [949594-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117722158620230727204721.0001): Torque and Temp. Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 949594-6 · Mar 7, 2022
- [949594-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115640397520230727204722.0001): Torque and Temp. Limiter. Honeywell International Inc. · PMA PQ1222NM · Replaces 949594-8 · Mar 7, 2022
- [218095ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID732648720520220105142916.0001): Screw, Fil HD DR CRES. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 218095 · Dec 22, 2021
- [3003-325ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID493521808820220105142917.0001): Shim, Laminated. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3003-325 · Dec 22, 2021
- [3204-059ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181465244720220105142916.0001): Washer, CRES. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 3204-059 · Dec 22, 2021
- [3003-325ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID419324450202201051428520.0001): Shim, Laminated. Torrington Distributors Inc · PMA PQ2067NE · Replaces 3003-325 · Dec 7, 2021
- [218095ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID286003867202201051428510.0001): Screw, Fil HD DR CRES. Torrington Distributors Inc · PMA PQ2067NE · Replaces 218095 · Dec 7, 2021
- [3204-059ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109754381820220105142852.0001): Washer, CRES. Torrington Distributors Inc · PMA PQ2067NE · Replaces 3204-059 · Dec 7, 2021
- [S9413-214WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170485473120240806154154.0001): Packing, Preform – Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-214 · Nov 19, 2021
- [S9413-214WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156736086320221102020330.0001): Packing, Preform – Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-214 · Nov 19, 2021
- [1386-150ACD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID557144642520210910172005.0001): Seal. Aircraft Component Design LLC · PMA PQ2138NE · Replaces 1386-150 · Jul 20, 2021
- [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID557477514020210611145222.0001): ANB Aviation Parts LLC · PMA PQ1730CE · Jan 7, 2021
- [3103590-2WE](https://drs.faa.gov/browse/excelExternalWindow/CD9F301C7FF4E37886258228007887AD.0001): Gear-Spur. Wencor LLC · PMA PQ1370NM · Replaces 3103590-2 · Nov 19, 2017
- [3103589-1WE](https://drs.faa.gov/browse/excelExternalWindow/96B4577E4AB3345B86258228007887AC.0001): Gear-Spur. Wencor LLC · PMA PQ1370NM · Replaces 3103589-1 · Nov 19, 2017
- [358894AL-1](https://drs.faa.gov/browse/excelExternalWindow/A8B885547F88F1DD8625836A00502CDB.0001): Bearing, Ball Supplement 91. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 358894-1 · Sep 7, 2016
- [358348AL](https://drs.faa.gov/browse/excelExternalWindow/9B596539329FA2DD8625836A00502C90.0001): Bearing, Ball Supplement 77. Extex Engineered Products Inc · PMA PQ2203NM · Replaces 358348 · Sep 7, 2016
- [3103035-1WD](https://drs.faa.gov/browse/excelExternalWindow/FA474A67BED4D85786257F37005F57C2.0001): Bearing Set, Annular Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 3103035-1 · Dec 14, 2015
- [3103585-1WD](https://drs.faa.gov/browse/excelExternalWindow/CBF0B872508D732D86257F37005F5BCD.0001): Bearing Set, Annular Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 3103585-1 · Dec 14, 2015
- [3101405-1WD](https://drs.faa.gov/browse/excelExternalWindow/7722B07BA165087C86257F37005F59AE.0001): Bearing, Annular Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 3101405-1 · Dec 14, 2015
- [3108098-1WD](https://drs.faa.gov/browse/excelExternalWindow/69F77033252EBA4086257F370070FAC2.0001): Bearing, Roller. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 3108098-1 · Dec 14, 2015

All of them: https://openairdocs.org/engine/airesearch-tpe331-8-series/pma.md

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