# Alliedsign TFE731-3R

- Type: Engine model (FAA registry)
- Registry code: 02612
- Manufacturer (registry): ALLIEDSIGN
- Model: TFE731-3R
- Engine type: Turbo-fan
- Power: 3,880 lb thrust
- Data sheet: [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Holder: Honeywell Aerospace US LLC
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/alliedsign-tfe731-3r

Model codes come from the FAA registry's reference file.

## 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 2010-06-11](https://openairdocs.org/ad/2010-06-11): Second stage low-pressure compressor rotor (LPCR) discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2C and 16 more. Effective Apr 21, 2010
- [AD 2005-13-07](https://openairdocs.org/ad/2005-13-07): Turbine rotor discs. · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Jul 27, 2005
- [AD 2005-05-15](https://openairdocs.org/ad/2005-05-15): (LPT) stage 1 disks · Honeywell International TFE731-2, TFE731-2C, TFE731-3 and 5 more. Effective Apr 18, 2005
- [AD 2001-23-09](https://openairdocs.org/ad/2001-23-09): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Dec 21, 2001
- [AD 2000-15-09](https://openairdocs.org/ad/2000-15-09): HPC Impeller · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 20 more. Effective Oct 10, 2000
- [AD 98-17-01 R1](https://openairdocs.org/ad/98-17-01-R1): Flex Fuel Tube · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Nov 29, 1999
- [AD 96-05-03](https://openairdocs.org/ad/96-05-03): Fan rotor disks · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 13 more. Effective Apr 2, 1996
- [AD 96-04-01](https://openairdocs.org/ad/96-04-01): Fan Rotor Assembly · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Mar 15, 1996
- [AD 95-07-02](https://openairdocs.org/ad/95-07-02): Low Pressure Turbine Disks · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 3 more. Effective Jun 19, 1995
- [AD 94-07-03](https://openairdocs.org/ad/94-07-03): Turbine Nozzles · Honeywell International TFE731-2A, TFE731-3, TFE731-3A and 4 more. Effective Jun 6, 1994
- [AD 92-21-06](https://openairdocs.org/ad/92-21-06): Low Pressure Turbine (LPT) Rotor Disks · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Nov 27, 1992
- [AD 90-24-06](https://openairdocs.org/ad/90-24-06): Thermocouple Lead Assemblies · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 8 more. Effective Nov 13, 1990
- [AD 90-03-04](https://openairdocs.org/ad/90-03-04): High Pressure Turbine Rotor Discs · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Feb 22, 1990
- [AD 88-18-03](https://openairdocs.org/ad/88-18-03): High Pressure Turbine Rotor Disc · Honeywell International TFE731-3, TFE731-3A, TFE731-3AR and 1 more. Effective Jul 21, 1989
- [AD 86-03-01](https://openairdocs.org/ad/86-03-01): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 4 more. Effective Feb 24, 1986
- [AD 82-23-03 R1](https://openairdocs.org/ad/82-23-03-R1): High Pressure Compressor Impellers · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective Dec 9, 1983
- [AD 81-24-08](https://openairdocs.org/ad/81-24-08): Turbine Interstage Transition Ducts · Honeywell International TFE731-2, TFE731-3, TFE731-3A and 2 more. Effective Jan 6, 1982
- [AD 80-16-04](https://openairdocs.org/ad/80-16-04): Tie Rod · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Aug 7, 1980
- [AD 78-22-10](https://openairdocs.org/ad/78-22-10): Low Pressure Rotor Thrust Ball Bearings · Honeywell International TFE731-2, TFE731-3 and TFE731-3R. Effective Nov 13, 1978
- [AD 75-07-10](https://openairdocs.org/ad/75-07-10): Transfer Gearbox Vertical Bevel Gear Bearing · Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 12 more. Effective May 1, 1975

Historical (superseded or no longer in force):

- [AD 98-17-01](https://openairdocs.org/ad/98-17-01) (historical): Honeywell International TFE731-2, TFE731-2A, TFE731-2B and 14 more. Effective Oct 13, 1998
- [AD 96-18-13](https://openairdocs.org/ad/96-18-13) (historical): Fan rotor disk · Honeywell International TFE731-2, TFE731-2A, TFE731-3 and 10 more. Effective Nov 12, 1996
- [AD 86-11-05](https://openairdocs.org/ad/86-11-05) (historical): Fan Rotor Discs · Honeywell International TFE731-2, TFE731-3 and TFE731-3R

## Registered aircraft (1)

- [N910KS](https://openairdocs.org/aircraft/N910KS): [Aircraft Holding Solutions LLC](https://openairdocs.org/faa-owner/AIRCRAFT%20HOLDING%20SOLUTIONS%20LLC), [Newark, DE](https://openairdocs.org/faa-place/DE/Newark), built 1982, S/N NA0328

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (24)

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

- [SDR CA110316004](https://openairdocs.org/sdr/CA110316004), Mar 7, 2011: SERVO. MALFUNCTIONED. (CAN) ON THE RETURN FLIGHT AFTER COMMENCING DESCENT FROM FL400, WHILE ON AUTOPILOT AT APPROX FL220, THE ACFT BEGAN A TURN TO THE LEFT UN-COMMANDED. DISCONNECTED
- [SDR CA071011007](https://openairdocs.org/sdr/CA071011007), Sep 14, 2007: ATTACH FITTING. CRACKED. (CAN) AFTER REPAINT OF A/C INSPECTION REVEALED A CRACK ON SIDE OF ATTACH POINT. LDG WAS PULLED TO REPLACE ATTACH POINT BRACKET AND ATTACH POINT BRACKET BOLTS. T
- [SDR CA060906011](https://openairdocs.org/sdr/CA060906011), Sep 6, 2006: SKIN. CRACKED. (CAN) DURING REMOVAL FOR ACCESS, A GENERAL VISUAL INSPECTION OF THE RT MAIN GEAR DOOR REVEALED A LARGE CRACK IN THE INNER SKIN PANEL AS WELL AS SEVERAL PULLED R
- [SDR CA050919006](https://openairdocs.org/sdr/CA050919006), Aug 31, 2005: GEARSHAFT. BROKEN. (CAN) AS A/C WAS TAXIING FOR T/O, CREW LOST LT ENGINE OIL PRESSURE. ENGINE WAS SHUTDOWN AND A/C WENT BACK TO GATE. LT ENGINE OIL PUMP WAS FOUND DAMAGED. PUMP WA
- [SDR 2004FA0000077](https://openairdocs.org/sdr/2004FA0000077), Jan 4, 2004: WIRE HARNESS. DETERIORATED. WHILE EN ROUTE, NOTED RT ENGINE COMPUTER AMBER WARNING LAMP BECAME ANNUNCIATED. ALSO NOTED, INDICATED LOSS OF POWER RT ENGINE. CONSULTED AND COMPLIED WITH EMERG
- [SDR ILPA048F](https://openairdocs.org/sdr/ILPA048F), Jan 24, 2003: PRESSURE PANEL. CRACKED. DURING ROUTINE INSPECTION OF THE RIVETS AT THE FORWARD PRESSURE BULKHEAD, TWO SEPERATE CRACKS WERE NOTED IN THE LT DISHPAN JUST FORWARD OF THE PILOTS RUDDER PED
- [SDR CA020607009](https://openairdocs.org/sdr/CA020607009), May 30, 2002: GASKET. MISSING. (CAN) CREW NOTICED RT ENGINE OIL PRESSURE FLUCTUATING SLIGHTLY.- AFTER A PERIOD OF TIME THE OIL PRESSURE STARTED TO DECAY TO WHERE THE RED LOW OIL PRESSURE LIGH
- [SDR CA020201010](https://openairdocs.org/sdr/CA020201010), Jan 21, 2002: WIRE. WORN. (CAN) LT ENGINE STARTER GENERATOR WIRING WORN AT SUPPORT BRACKET.
- [SDR CA020201012](https://openairdocs.org/sdr/CA020201012), Jan 21, 2002: FAIRLEAD. BROKEN. (CAN) LT ENGINE STARTER GENERATOR WIRING WORN AT SUPPORT BRACKET AND PHENOLIC FAIRLEAD BROKEN.
- [SDR UO22001F00011](https://openairdocs.org/sdr/UO22001F00011), Oct 18, 2001: BEARING. FAILED. LOWER TOWER SHAFT BEARING FAILED CAUSING DAMAGE TO RELATED SHAFT AND CARRIERS ALSO CAUSING METAL CONTAMINATION TO OIL SYSTEM.
- [SDR CA010209017](https://openairdocs.org/sdr/CA010209017), Jan 31, 2001: RELAY. FAILED. (CAN) AFTER TAXI IN AT YVR THE NR 2 AC INVERTER FAIL LIGHT ILLUMINATED AS WELL AS XS2 BUSS FAIL LIGHT ILLUMINATED. RESET THE NR 2 INVERTER SWITCH FAILED TO RESE
- [SDR 99ZZZM808](https://openairdocs.org/sdr/99ZZZM808), Nov 18, 1999: BLADE. BROKEN. ENGINE WAS DISASSEMBLED FOR SCHEDULED MPI. DISCOVERED A FIRST STAGE LOW PRESSURE TURBINE BLADE FAILURE. THE SINGLE BLADE HAD FAILED AT THE MID-POINT OF THE BLAD
- [SDR 99ZZZX3009](https://openairdocs.org/sdr/99ZZZX3009), Jul 30, 1999: CARBON SEAL. FAILED. ENGINE LOST OIL PRESSURE IN-FLIGHT. DISASSEMBLY FOUND NR 5 CARBON SEAL BROKEN. CONTAMINATED OIL SYSTEM. PART S/N 960811401752. ENG TSN: 7,666.3 HOURS. ENG CSN: 
- [SDR 20000712SH038](https://openairdocs.org/sdr/20000712SH038), Jul 26, 1999: TURBINE WHEEL. CHAFED. SECOND OCCURRENCE OF 3RD STAGE LP TURBINE RUBBING FORWARD SIDE OF 3RD STAGE LPT SEAL. (X)
- [SDR CA990301002](https://openairdocs.org/sdr/CA990301002), Feb 3, 1999: BEARING. SEIZED. (CAN) APU SHUT DOWN DUE TO ROTOR GROUP SEIZURE. THE BEARING WAS A CORRECT ONE, AND FAILED MUCH TOO EARLY.
- [SDR 99ZZZX802](https://openairdocs.org/sdr/99ZZZX802), Jan 26, 1999: ENGINE. MALFUNCTIONED. ENGINE SHUT DOWN AT ALTITUDE BY PILOT. METAL PARTICLES FOUND IN TAIL PIPE DURING ENGINE REMOVAL. ENGINE FAN AND FAN TURBINE TURNED FREELY WITH NO NOISE. ENGINE 
- [SDR 99ZZZX824](https://openairdocs.org/sdr/99ZZZX824), Jan 26, 1999: BLADE. SEPARATED. DURING CRUISE AT FL 350, RT ENG HAD A RAPID RISE IN ITT AND VIBRATION LEVEL. CREW SHUT DOWN ENG. ENG REMOVED TO DETERMINE CAUSE OF FAILURE ANDTO REPAIR. DISASSY
- [SDR 99ZZZX60](https://openairdocs.org/sdr/99ZZZX60), Oct 15, 1998: BLADE. DAMAGED. DURING INSPECTION FOUND NUMEROUS FAN BLADES DAMAGED ON RIGHT ENGINE. FOUND RIVET MISSING AT 6 O'CLOCK POSITION ON ENGINE INLET LIP AND THREE LOOSE RIVETS. SUSPE
- [SDR CA980616016](https://openairdocs.org/sdr/CA980616016), Feb 18, 1998: BLADE. SEPARATED. (CAN) AFTER TAKEOFF DURING CLIMB THRU 4000 FEET, A LOUD BANG HEARD, FOLLOWED BY VIBRATION AND NR 1 ENGINE SPOOLING DOWN. ENG SHUT DOWN. NR 1 ENG SUFFERED CATAST
- [SDR CA970815014](https://openairdocs.org/sdr/CA970815014), Aug 4, 1997: SLEEVE CLAMP. LOOSE. (CAN) UNABLE TO MAINTAIN PRESSURIZATION DURING CLIMB. OPENED FLIGHT DECK VALVE AND RETURNED TO BASE. INVESTIGATION SHOWED A LOOSE CLAMP ON THE SILENCER TO SUPPL
- [SDR 97ZZZM716](https://openairdocs.org/sdr/97ZZZM716), May 19, 1997: BEARING. FAILED. EN ROUTE FROM BOS TO OXC, THE CHIP DETECTOR LIGHT FOR THE RIGHT ENGINE ILLUMINATED. NO OTHER ENGINE ABNORMALITY WAS APPARENT. THE AIRCRAFT LANDED AT OXC WITHOUT
- [SDR CA970227004](https://openairdocs.org/sdr/CA970227004), Feb 11, 1997: GENERATOR. VIBRATING. (CAN) SHORTLY AFTER TAKEOFF, INTERMITTENT VIBRATION WHICH BECAME CONTINUOUS. GENERATOR TRIPPED AND VIBRATIONS DECREASED. ENGINE SHUT DOWN AS PRECAUTIONARY. VIBR
- [SDR CA970206006](https://openairdocs.org/sdr/CA970206006), Jan 29, 1997: FUEL PUMP. FAILED. (CAN) ENGINE DRIVEN FUEL PUMP HAD NO OUTPUT PRESSURE, UNABLE TO GET START AFTER ENGINE SPOOLED DOWN FROM IDLE. TEAR DOWN REPORT REVEALED DAMAGED BEARING AT VANE
- [SDR JZBR10817](https://openairdocs.org/sdr/JZBR10817), Aug 9, 1995: ENGINE. FAILED. WHILE SITTING AT THE END OF RUNWAY, AIRCRAFT WAS CLEAR FOR TAKEOFF. CREW ADVANCED THROTTLES. WHILE SPOOLING UP TO N1 FOR TAKEOFF, THE LEFT ENGINE RELEASED A LOU

## PMA parts (OpenAirDocs) (102, 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.

- [S9413-008WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157713616420261009134008.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-008 · Oct 1, 2026
- [S9413-114WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144043282220261009134010.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-114 · Oct 1, 2026
- [TA3200-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197208112920260818173104.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Mar 3, 2025
- [TA3200-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122849565320260818173104.0001): Engine Preheat Kit. Hartzell Propeller LLC · PMA PQ2040CE · Modification part · Mar 3, 2025
- [S9413-012WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164716779820240919135854.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-012 · Sep 11, 2023
- [2118002-52](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195529410820230727204659.0001): Digit. Eng. Cont.. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118002-52 · Mar 8, 2022
- [2101144-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID185294538820230727204648.0001): Electronic Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101144-5 · Mar 8, 2022
- [2101142-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172222956120230727204711.0001): Electronic Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101142-4 · Mar 8, 2022
- [2118002-202](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156902722820230727204700.0001): Digit. Eng. Cont.. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118002-202 · Mar 8, 2022
- [2118002-9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147374206420230727204651.0001): Digital Electronic Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118002-9 · Mar 8, 2022
- [2118002-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129328930820230727204649.0001): Digital Electronic Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118002-6 · Mar 8, 2022
- [2118002-8](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124316171020230727204650.0001): Digital Electronic Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118002-8 · Mar 8, 2022
- [2101142-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103372920420230727204712.0001): Electronic Engine Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101142-5 · Mar 8, 2022
- [2118002-201](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103172369620230727204652.0001): Digital Electronic Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2118002-201 · Mar 8, 2022
- [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
- [JTE936193](https://drs.faa.gov/browse/excelExternalWindow/EA7F49FF3764F2A886257F2400628220.0001): Drive Coupling. Jet Tech Engineering · PMA PQ1680CE · Replaces 936193 · Dec 2, 2015
- [3073754-1PR](https://drs.faa.gov/browse/excelExternalWindow/455E4974043E2A3686257C94007032E5.0001): Ring, Retaining. Precision Ring, Inc. · PMA PQ2464CE · Replaces Garrett P/N 3073754-1 · Feb 23, 2014
- [3000002-10PR](https://drs.faa.gov/browse/excelExternalWindow/4229726F8178D8B286257C940070329F.0001): Ring, Piston Set. Precision Ring, Inc. · PMA PQ2464CE · Replaces Garrett P/N 3000002-10 · Feb 23, 2014
- [31-75105-4063-5NAD](https://drs.faa.gov/browse/excelExternalWindow/32C81E7A7367D34786257B570067A904.0001): Lube and Scavenge Pump Ref  Model 4447-10. Parker Hannifin Corp · PMA PQ0953NE · Replaces Honeywell International Inc. part… · Apr 24, 2013
- [334508WFC](https://drs.faa.gov/browse/excelExternalWindow/164F0797B5C0EFFF8625763F00662251.0001): Fuel Filter Element. Western Filter A Division of Donaldson Company Inc · PMA PQ1847NM · Replaces 897513-1, P-1008 · Aug 20, 2009
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/0D1AF728AC02291E8625763F00662238.0001): Oil Filter Element. Western Filter A Division of Donaldson Company Inc · PMA PQ1847NM · Replaces 3070945-1 · Aug 20, 2009
- [334508WFC](https://drs.faa.gov/browse/excelExternalWindow/52ACFE1327A97A7D862575BB00733276.0001): Oil Filter Element. Western Filter A Division of Donaldson Company Inc · PMA PQ1847NM · Replaces 897513-1, P-1008 · Apr 27, 2009
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/0069FF1E367A1244862575BB00733240.0001): Oil Filter Element. Western Filter A Division of Donaldson Company Inc · PMA PQ1847NM · Replaces 3070945-1 · Apr 27, 2009
- [M358206](https://drs.faa.gov/browse/excelExternalWindow/C3F94AF3BE7B1B5F86257598004C7470.0001): Ball Bearing. Miraj Corporation · PMA PQ0870NE · Replaces Honeywell 358206 · Mar 23, 2009
- [9048393-312](https://drs.faa.gov/browse/excelExternalWindow/F6D45FFF9E6F142B86257530006882B7.0001): Igniter Lead. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060722-12 · Oct 26, 2008
- [421619](https://drs.faa.gov/browse/excelExternalWindow/CF0C3186FAC0CF35862575300068837E.0001): Harness. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060762-2 · Oct 26, 2008
- [9048393-311](https://drs.faa.gov/browse/excelExternalWindow/AA5BD3DF678E6198862575300068828B.0001): Igniter Lead. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060722-11 · Oct 26, 2008
- [9052326-3](https://drs.faa.gov/browse/excelExternalWindow/8EC617C8CE59C83C86257530006882E1.0001): Harness. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060729-3 · Oct 26, 2008
- [421502](https://drs.faa.gov/browse/excelExternalWindow/7CFA767D05064B6E862575300068831A.0001): Harness. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060748-3 · Oct 26, 2008
- [421618](https://drs.faa.gov/browse/excelExternalWindow/62100BA52D71FA4E862575300068834F.0001): Harness. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060757-2 · Oct 26, 2008
- [9048393-310](https://drs.faa.gov/browse/excelExternalWindow/21031DF5743E92F8862575300068824A.0001): Igniter Lead. Unison Industries · PMA PQ1052CE · Replaces Honeywell P/N 3060722-10 · Oct 26, 2008
- [334508WFC](https://drs.faa.gov/browse/excelExternalWindow/915C433D4B455B848625746B0054E055.0001): Oil Filter Element. Western Filter Corporation · PMA PQ1847NM · Replaces 897513-1, P-1008 · May 26, 2008
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/4EA67EE067C8D3108625746B0054E011.0001): Oil Filter Element. Western Filter Corporation · PMA PQ1847NM · Replaces 3070945-1 · May 26, 2008
- [334508WFC](https://drs.faa.gov/browse/excelExternalWindow/76D6BD1A1014F5458625740B005FC803.0001): Oil Filter Element. Western Filter Corporation · PMA PQ1847NM · Replaces 897513-1, P-1008 · Feb 26, 2008
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/3D85FBEA9E48933C8625740B005FC7D1.0001): Oil Filter Element. Western Filter Corporation · PMA PQ1847NM · Replaces 3070945-1 · Feb 26, 2008
- [358206WD](https://drs.faa.gov/browse/excelExternalWindow/8A03B564BBB20F2C862573E600519900.0001): Bearing, Annular Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 358206 · Dec 26, 2007
- [358272WD](https://drs.faa.gov/browse/excelExternalWindow/04E5A014AB0B6A3E862573E60051995B.0001): Bearing, Annular Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces Honeywell 358272 · Dec 26, 2007
- [2101144-5](https://drs.faa.gov/browse/excelExternalWindow/4F2CF4EA57192082862572F10055081A.0001): Electronic Engine Control (EEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2101144-5 · May 14, 2007
- [2101144-2](https://drs.faa.gov/browse/excelExternalWindow/42D796AB616A82B1862572F1005507A2.0001): Electronic Engine Control (EEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2101144-2 · May 14, 2007
- [1763585](https://drs.faa.gov/browse/excelExternalWindow/6185946877C3FA858625788800575305.0001): Element Assembly. Purolator Facet Inc (formerly Facet Filter Products) · PMA PQ1207CE · Replaces Honeywell P/N 3070945-1, PTI… · Dec 11, 2006
- [1-1497-701](https://drs.faa.gov/browse/excelExternalWindow/135321864A569974862571E90063042C.0001): O-Ring Face Seal. Rexnord Industries, LLC · PMA PQ2030CE · Replaces Honeywell (Allied Signal, Garrett)… · Aug 31, 2006
- [2101144-5](https://drs.faa.gov/browse/excelExternalWindow/E87BC39BF741BA8586257132005C2255.0001): Electronic Engine Control (EEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2101144-5 · Feb 8, 2006
- [2101144-2](https://drs.faa.gov/browse/excelExternalWindow/E12B9BA94513EB7286257132005C2214.0001): Electronic Engine Control (EEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2101144-2 · Feb 8, 2006
- [DN518498](https://drs.faa.gov/browse/excelExternalWindow/73B9A2266B0C955A8525704200569AAE.0001): Pressure Plate. Dynatech Aerospace Inc · Replaces 518498 · Jun 5, 2005
- [DN518477](https://drs.faa.gov/browse/excelExternalWindow/6ABAA5EE69472B0E8525704200569AAD.0001): Pressure Plate. Dynatech Aerospace Inc · Replaces 518477 · Jun 5, 2005
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/9FC9309BB2AD36F98525704D0059661D.0001): Oil Filter Element. Western Filter Corporation · Replaces 3070945-1 · Oct 20, 2003
- [3000002-10PR](https://drs.faa.gov/browse/excelExternalWindow/E5D2C61FB15C23678525704A0053D22A.0001): Piston Ring. Precision Ring Inc · Replaces Garrett 3000002-10 · Oct 7, 2002
- [3073754-1PR](https://drs.faa.gov/browse/excelExternalWindow/72C353B54AFA7B558525704A0053D232.0001): Retaining Ring. Precision Ring Inc · Replaces Garrett 3073754-1 · Oct 7, 2002
- [38-87006-3022-4NAD Rev - dated 09/29/98](https://drs.faa.gov/browse/excelExternalWindow/D3840527E549811A862574E5006EA9F5.0001): Valve, Regulator Adjustable. Parker Hannifin Corp, Nichols Airborne Division · PMA PQ0953NE · Replaces Allied Signal 38-87006-3022-4 · Feb 3, 2000

All of them: https://openairdocs.org/engine/alliedsign-tfe731-3r/pma.md

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