# Honeywell TFE731-3C

- Type: Engine model (FAA registry)
- Registry code: 33841
- Manufacturer (registry): HONEYWELL
- Model: TFE731-3C
- Engine type: Turbo-fan
- Power: 3,700 lb thrust
- Data sheet: [TCDS E6WE](https://openairdocs.org/tcds/E6WE) (OpenAirDocs)
- Holder: Honeywell Aerospace US LLC
- Installed in: 10 registered aircraft
- Page: https://openairdocs.org/engine/honeywell-tfe731-3c

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 2008-02-19](https://openairdocs.org/ad/2008-02-19): High pressure (HP) turbine rotor assemblies · Honeywell International TFE731-20AR, TFE731-20BR, TFE731-20R and 15 more. Effective Mar 6, 2008
- [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 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 97-04-03](https://openairdocs.org/ad/97-04-03): First stage low pressure turbine (LPT) seal plates · Honeywell International TFE731-2A, TFE731-3C and TFE731-3CR. Effective May 5, 1997
- [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 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 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

## Registered aircraft (10)

- [N117BG](https://openairdocs.org/aircraft/N117BG): [Johnson Calvin](https://openairdocs.org/faa-owner/JOHNSON%20CALVIN), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), built 1983, S/N 650-0007
- [N264GV](https://openairdocs.org/aircraft/N264GV): [Csc Delaware Trust Co Trustee](https://openairdocs.org/faa-owner/CSC%20DELAWARE%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 2000, S/N 650-0104
- [N419MK](https://openairdocs.org/aircraft/N419MK): [Aviation Trust Co LLC Trustee](https://openairdocs.org/faa-owner/AVIATION%20TRUST%20CO%20LLC%20TRUSTEE), [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City), built 1993, S/N 066
- [N4554](https://openairdocs.org/aircraft/N4554): [D&J Air LLC](https://openairdocs.org/faa-owner/D%26J%20AIR%20LLC), [Canyon, TX](https://openairdocs.org/faa-place/TX/Canyon), built 2001, S/N 143
- [N47AN](https://openairdocs.org/aircraft/N47AN): [Lagoinha Orlando Church Inc](https://openairdocs.org/faa-owner/LAGOINHA%20ORLANDO%20CHURCH%20INC), [Orlando, FL](https://openairdocs.org/faa-place/FL/Orlando), built 1984, S/N 650-0054
- [N56DH](https://openairdocs.org/aircraft/N56DH): [Metro Builders Supply Inc](https://openairdocs.org/faa-owner/METRO%20BUILDERS%20SUPPLY%20INC), [Tulsa, OK](https://openairdocs.org/faa-place/OK/Tulsa), built 1990, S/N 045
- [N577AN](https://openairdocs.org/aircraft/N577AN): [Fifteen Seventy Aviation LLC](https://openairdocs.org/faa-owner/FIFTEEN%20SEVENTY%20AVIATION%20LLC), [Greenville, TX](https://openairdocs.org/faa-place/TX/Greenville), S/N 060
- [N664MM](https://openairdocs.org/aircraft/N664MM): [Aquarius Aircraft Leasing LLC](https://openairdocs.org/faa-owner/AQUARIUS%20AIRCRAFT%20LEASING%20LLC), [Nashville, TN](https://openairdocs.org/faa-place/TN/Nashville), built 1984, S/N 650-0037
- [N949SA](https://openairdocs.org/aircraft/N949SA): [N501wj LLC](https://openairdocs.org/faa-owner/N501WJ%20LLC), [Ottawa Lake, MI](https://openairdocs.org/faa-place/MI/Ottawa%20Lake), built 1985, S/N 650-0074
- [N962A](https://openairdocs.org/aircraft/N962A): [D & E Aviation LLC](https://openairdocs.org/faa-owner/D%20%26%20E%20AVIATION%20LLC), [Missoula, MT](https://openairdocs.org/faa-place/MT/Missoula), built 1989, S/N 031

## NTSB investigations (2)

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 WPR22LA039](https://openairdocs.org/ntsb/WPR22LA039), Nov 14, 2021: Iai 1125 Westwind Astra (N771DX), North Las Vegas, NV, substantial damage. Probable cause: The pilot landed long and failed to deploy the thrust reversers, which resulted in a runway overrun and impact with terrain. Contributing to the accident was the pilot’s decision to operate the…
- [NTSB FTW96LA405](https://openairdocs.org/ntsb/FTW96LA405), Sep 30, 1996: Israel Aircraft Industries 1125 Westwind Astra (N419MK), Aspen, CO, substantial damage. Probable cause: failure of the right brake antiskid, due to corrosion of a canon plug; and failure of the flight crew to revert to the normal brake system.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20211114019529A](https://openairdocs.org/incident/20211114019529A), Nov 14, 2021: Israel Aircraft Industries 1125 WESTWIND ASTRA (N771DX), North Las Vegas, NV, Substantial damage. On November 14, 2021, at approximately 1442 PST, the las FSDO received notification from the western pacific?s regional operations center, regarding an…
- [Accident 19960930047019A](https://openairdocs.org/incident/19960930047019A), Sep 30, 1996: Israel 1125 (N419MK), Aspen, CO, Substantial damage. (-16) At this time the aircraft is still under investigation to see if there was/is a mechanical problem or not which would cause the aircraft to drift to the…

## Service difficulty reports (36)

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

- [SDR 2JKA20240425002](https://openairdocs.org/sdr/2JKA20240425002), Apr 20, 2024: ENGINE. FLAMED OUT. TOOK OFF FROM KAUS AT 17:36 UTC. DURING CRUISE, AROUND 2 HRS AFTER DEPARTURE, FLYING AT FL 400, FUEL ON BOARD WAS 4500 LBS, VMC CONDITIONS, AND NO TURBULENCE, H
- [SDR WNDA2016FA0000105](https://openairdocs.org/sdr/WNDA2016FA0000105), Mar 1, 2016: ACM. OVERHEATED. ON CLIMBOUT AFTER TAKEOFF, PILOT NOTICED SMOKE IN THE CABIN FOLLOWED BY RT PAC OVERHEAT LIGHT. AFTER FURTHER INVESTIGATION BY MAINTENANCE FOUND THE RT AIR CYCLE
- [SDR T8VA2016F00013](https://openairdocs.org/sdr/T8VA2016F00013), Oct 15, 2015: ACTUATOR. FAILED. PRIMARY TRIM FAILED IN FLIGHT. IAW CHECKLIST SWITCH TO SECONDARY TRIM. SECONDARY TRIM FAILED. ACCOMPLISHED DUAL TRIM FAILURE CHECKLIST. DECLARED AN EMERGENCY AN
- [SDR CA150415004](https://openairdocs.org/sdr/CA150415004), Apr 8, 2015: LINK. BENT. (CAN) UPON A THRUST REVERSER DETAILED INSPECTION & LUBRICATION, THE LT OTBD UPPER AFT THRUST REVERSER DOOR LINK WAS FOUND BENT. UPON FURTHER INVESTIGATION FOUND
- [SDR CA140217005](https://openairdocs.org/sdr/CA140217005), Feb 15, 2014: ENGINE. FAILED. (CAN) LEFT ENGINE FAILURE, ENROUTE, LT ENGINE WENT FROM CRUISE POWER TO IDLE AND WAS UNRESPONSIVE TO THROTTLE LEVER MOVEMENT. AFTER A COUPLE OF MINUTES THE ENGI
- [SDR CA121231002](https://openairdocs.org/sdr/CA121231002), Dec 22, 2012: CONNECTOR. DAMAGED. (CAN) GEAR UNSAFE LIGHT ON AFTER RETRACTION AFTER T/O. CREW CYCLED L/G 2X, BOTH TIMES THE GEAR DID NOT RETRACT PROPERLY, FOLLOWED ABNORMAL PROCEDURES CHECKLIST 
- [SDR CA121012012](https://openairdocs.org/sdr/CA121012012), Oct 9, 2012: TRUNNION. GOUGED. (CAN) DURING REPLACEMENT OF THE RT MLG OLEO, THE OTBD GEAR DOOR WAS REMOVED. WHEN REINSTALLING THE DOOR IT WAS NOTICED THAT THE RT MAIN GEAR TRUNNION WAS GOUGED
- [SDR 2012FA0000599](https://openairdocs.org/sdr/2012FA0000599), Aug 30, 2012: STEERING UNIT. OUT OF LIMITS. CREW REPORTED THAT NOSEWHEEL STEERING SEEMED "SLOPPY" AROUND NEUTRAL THAN PREVIOUS. INSPECTED ACFT. FUNCTIONAL TESTED NOSE WHEEL STEERING WITH NO OBVIOUS DISCRE
- [SDR 2012FA0000571](https://openairdocs.org/sdr/2012FA0000571), Aug 15, 2012: ANNUNCIATOR. FALSE INDICATION. AT FL170, CREW RECEIVED A FUEL LOW PRESSURE, HYD PRESSURE LOW, FUEL F/W SHUTOFF, AND AN EMERGENCY PRESSURE INDICATIONS. IN ADDITION, THE MASTER WARNING SWITCH L
- [SDR FCPA20110816](https://openairdocs.org/sdr/FCPA20110816), Aug 11, 2011: CHIP DETECTOR. CONTAMINATED. AFTER DEPARTURE DURING CLIMBOUT, THE RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. AIRCRAFT FLIGHT MANUAL INDICATES TO SHUT DOWN ENGINE (WHEN PRACTICAL) AND LAN
- [SDR 2010FA0000963](https://openairdocs.org/sdr/2010FA0000963), Sep 5, 2010: FUEL CONTROL. OUT OF ADJUST. LT ENGINE SHUTDOWN IN CRUISE AT 30,000 FT. FLIGHT CREW ABLE TO RESTART NO FURTHER DEFECTS NOTED. FUEL CONTROL REPLACED WITH O/H UNIT, OPS CHECKS PROVIDED SATISF
- [SDR CA100908001](https://openairdocs.org/sdr/CA100908001), Aug 4, 2010: SEAL. WORN. WHILE CRUISING AT FL380, AUTOPILOT HEADING CONTROL BEGAN BEHAVING ABNORMALLY. WHEN THE FLIGHT CREW DISCONNECTED THE AUTOPILOT THEY WERE UNABLE TO MOVE AILERON C
- [SDR JGVR2010F00103](https://openairdocs.org/sdr/JGVR2010F00103), May 7, 2010: ATTACH BRACKET. CORRODED. ( JGVR ) DURING A SCHEDULED A-CHECK INSPECTION, CORROSION WAS FOUND ON THE LT AILERON ACTUATOR ATTACH BRACKET. STARTED REMOVING CORROSION AND FOUND CORROSION MI
- [SDR Y9PA199HE5.29.09](https://openairdocs.org/sdr/Y9PA199HE5.29.09), May 29, 2009: VALVE. FAILED. CREW NOTICED CABIN DUCT TEMP HI LIGHT ON MASTER WARNING PANEL, CABIN AIR COMING INTO CABIN WAS HOT, CREW FOLLOWEWD ACFT CHECK LIST TO EXTINGUISH THE WARNING LIG
- [SDR Y9PAN199HE4.24.09](https://openairdocs.org/sdr/Y9PAN199HE4.24.09), Apr 24, 2009: HINGE FITTING. MISLOCATED. UPON DEPARTURE, AFTER GEAR RETRACTION, THE GEAR UNSAFE LIGHT REMAINED ILLUMINATED INDICATING ONE OF THE GEAR HAD NOT COMPLETELY RETRACTED INTO THE UPLOCK. OBTAI
- [SDR 2009FA0000276](https://openairdocs.org/sdr/2009FA0000276), Apr 3, 2009: SYMBOL GENERATOR. FAILED. BOUGHT AN EXCHANGED SG-603 SYMBOL GENERATOR WITH AN 8130 THAT SAID REPAIRED ON IT. INSTALLED PART IN AIRCRAFT, IT HAD THE VERY SAME FAILURE AS THE INCOMING FAIL
- [SDR DBCA20081219605SA](https://openairdocs.org/sdr/DBCA20081219605SA), Dec 18, 2008: O-RING. CUT. DURING CRUISE FLIGHT, CREW NOTICED NR 1 ENG OIL PRESSURE DECREASING FROM 42 PSI TO 35 PSI. CREW REDUCED POWER ON NR 1 ENGINE AND CONTINUED TO MONITOR OIL PRESSU
- [SDR CA080326003](https://openairdocs.org/sdr/CA080326003), Mar 24, 2008: COUPLING. MISINSTALLED. (CAN) CREW WROTE UP, CABIN PAC STUCK ON FULL COLD. TROUBLESHOOTING CARRIED OUT AND FOUND THAT THE COUPLING FOR CABIN TEMP CONTROL HAD DISCONNECTED FROM THE ENVI
- [SDR CA060822001](https://openairdocs.org/sdr/CA060822001), Aug 5, 2006: BOLT. BROKEN. (CAN) ON DAILY INSPECTION, FOUND (1) BOLT BROKEN ON NR 4 MAIN WHEEL ASSY. (TC NR 20060822001)
- [SDR CA060224008](https://openairdocs.org/sdr/CA060224008), Feb 24, 2006: TURNBUCKLE. CHAFED. DURING A SCHEDULED PHASE 5 INSPECTION ON CESSNA 650 C-FIMO, THE TECHNICIAN DISCOVERED THAT THE LT AND RT AILERON OUTBOARD AFT CABLE CHAFED THROUGH THE LOKCLAD A
- [SDR ZN3R556712](https://openairdocs.org/sdr/ZN3R556712), Jan 3, 2006: STATOR. SEPARATED. ENGINE 4TH LPC STATOR HAD INNER RING FRACTURE, LEADING TO A SINGLE VANE SEPARATING FROM THE STATOR ASSEMBLY. THE VANE CAUSED DAMAGE TO THE HPC AREA OF THE ENGIN
- [SDR CA051018001](https://openairdocs.org/sdr/CA051018001), Oct 17, 2005: TURNBUCKLE. CHAFED. DURING PHASE 1-5 INSPECTION ON AIRCRAFT, TECHNICIANS DISCOVERED THAT THE LT AND RT AILERON CABLES WERE FOULING. THE RESULT WAS THAT THE LT TURNBUCKLE WAS CHAFED
- [SDR DJFA2005148](https://openairdocs.org/sdr/DJFA2005148), Oct 6, 2005: LINE. LEAKING. CREW REPORTED THAT RT ENGINE OIL LOW PRESSURE ANNUNCIATOR HAD ILLUMINATED WHILE IN CRUISE FLIGHT APPROX AN HOUR AND A HALF AFTER TAKE OFF. RT ENGINE OIL PRESSUR
- [SDR CA050714001](https://openairdocs.org/sdr/CA050714001), Jul 6, 2005: RETAINER. MISSING. (CAN) WHILE DOING A VISUAL INSPECTION, IT WAS FOUND THAT THE RT FLAP FLEXSHAFT RETAINER WAS MISSING (BROKEN OFF). NEW RETAINER WAS INSTALLED.
- [SDR CA050407002](https://openairdocs.org/sdr/CA050407002), Apr 4, 2005: PUMP. FAILED. (CAN) AFTER TAKE-OFF, THE LT HYDRAULIC PRESSURE LOW ANNUNCIATION ILLUMINATED IN CLIMB. AIRCRAFT RETURN TO MAINTENANCE BASE. LT ENGINE HYDRAULIC DRIVEN PUMP REPL
- [SDR DJFA2004029](https://openairdocs.org/sdr/DJFA2004029), Oct 21, 2004: FUEL CONTROL. UNSERVICEABLE. CREW REPORTED THAT WHILE AT V2 RIGHT FUEL COMPUTER ANNUNCIATOR ILLUMINATED AND THE NR 2 ENGINE ROLLED BACK TO 70 PERCENT AND STARTED SURGING. THE AIRCRAFT ROLLE
- [SDR DJFA2004019](https://openairdocs.org/sdr/DJFA2004019), Aug 11, 2004: SEAL. LEAKING. DURING CLIMB THE NR 1 ENGINE FIRE LIGHT CAME ON. THE CREW RETARDED THE THROTTLES AND THE LIGHT WENT OUT. THEY RETURNED TO THE DEPARTURE AIRPORT WITH NO PROBLEMS
- [SDR DBCR122D](https://openairdocs.org/sdr/DBCR122D), Jun 14, 2004: ENGINE. FAILED. AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGRADE WITH OVERTEMP LIGHT. FLIGHT CREW SECU
- [SDR DBCA122D3](https://openairdocs.org/sdr/DBCA122D3), May 14, 2004: ENGINE. FOD. AFTER TAKEOFF, FLIGHT CREW NOTICED LOUD RUMBLE FOLLOWED BY NR 1 ENGINE SPOOLING DOWN. ITT INDICATED 1000 DEGREE CENTIGRADE WITH OVERTEMP LIGHT. FLIGHT CREW SECU
- [SDR CA040213002](https://openairdocs.org/sdr/CA040213002), Feb 12, 2004: TORQUE TUBE. MISINSTALLED. (CAN) RECEIVED A RUDDER TORQUE TUBE NOT PROPERLY ASSEMBLED, FROM A MANUFACTURER. A RIB WAS NOT INSTALLED CORRECTLY DURING A MANUFACTURING PROCESS.
- [SDR CA031113008](https://openairdocs.org/sdr/CA031113008), Nov 13, 2003: CONTROL CABLE. FRAYED. (CAN) DURING A SCHEDULE INSPECTION ON RT WING OB FLIGHT SPOILER. THE OB RT SPOILER ACTUATING CABLE (FOR THE FLT SPOILER ACTUATOR) WAS FOUND FRAYED UNDER A PULLE
- [SDR CA031113007](https://openairdocs.org/sdr/CA031113007), Nov 12, 2003: TORQUE TUBE. CHAFED. (CAN) DURING A PHASE 5 INSPECTION A TASK INVOLVE THE REMOVAL OF THE AFT VERTICAL FIN TOP FAIRING, TO INSPECTED INSIDE THIS AREA. MAINTENANCE PERSONNEL FOUND THE
- [SDR CA030520001](https://openairdocs.org/sdr/CA030520001), May 16, 2003: WIRE. BROKEN. (CAN) AFTER THE AIRCRAFT TOOK-OFF PILOT SELECTED THE GEAR HANDLE TO THE UP POSITION. DURING CLIMB PILOT REPORT LT MAIN LANDING INDICATION STILL SHOWN GEAR DOWN 
- [SDR CA020829002](https://openairdocs.org/sdr/CA020829002), Aug 28, 2002: CONTROL CABLE. FRAYED. (CAN) DURING PHASE "A" INSPECTION. MAINTENANCE PERSONNEL WHEN THROUGH THE TAIL CONE AREA TO COMPLETE A VISUAL INSPECTION. ON THE LT SIDE OF THE TAIL CONE TECHNI
- [SDR 2002F00434](https://openairdocs.org/sdr/2002F00434), May 1, 2002: O-RING. DEFECTIVE. LT ENGINE HAD A LOSS OF OIL PRESSURE, SHUT DOWN LT ENGINE. LANDED IN MCO. CESSNA SERVICE CENTER TROUBLESHOT PROBLEM TO BAD O-RING ON LT ENGINE OIL CAP (OUTBOARD
- [SDR O9I2002F00001](https://openairdocs.org/sdr/O9I2002F00001), Apr 30, 2002: TIP CAP. DELAMINATED. THE TRAILING EDGE OF THE RIGHT HORIZONTAL STABILIZER TIP CAP (PN 24W45002050251) WAS FOUND TO BE DELAMINATING ON THE TRAILING EDGE . THIS IS A COMPOSITE ASSEMBL

## PMA parts (OpenAirDocs) (104, 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
- [2101144-6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179361796120230731171126.0001): Controller. Honeywell International Inc. · PMA PQ1222NM · Replaces 2101144-6 · Jul 26, 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
- [3000002-4PR](https://drs.faa.gov/browse/excelExternalWindow/BFB9CB4A4626D36586257C940070325C.0001): Ring, Piston Set. Precision Ring, Inc. · PMA PQ2464CE · Replaces Garrett P/N 3000002-4 · Feb 23, 2014
- [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
- [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
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/F796A3280CF675E786257B4000546D12.0001): Element Assembly. Western Filter A Division of Donalson Company Inc · PMA PQ1847NM · Replaces 897513-1, Alternate: 334508WFC · Mar 11, 2013
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/C93EE3A4793197F18625763F0068706C.0001): Element Assembly. Western Filter A Division of Donaldson Company Inc · PMA PQ1847NM · Replaces 897513-1, Alternate 334508WFC · Aug 20, 2009
- [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
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/8781767537282A74862575D300634D50.0001): Element Assembly. Western Filter A Division of Donaldson Company Inc · PMA PQ1847NM · Replaces 897513-1 · May 28, 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
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/D56CCCF0ADCF82648625746B0054F06A.0001): Element Assembly. Western Filter Corporation · PMA PQ1847NM · Replaces 897513-1 · Apr 16, 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
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/34E4F503DA4311DD86257348005BF898.0001): Element Assembly. Western Filter Corporation · PMA PQ1847NM · Replaces 897513-1 · Sep 18, 2007
- [2118002-203](https://drs.faa.gov/browse/excelExternalWindow/EE6117180CC2EF6B862572F1005509FE.0001): Digital Electronic Engine Control (DEEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2118002-203 · May 14, 2007
- [2101144-6](https://drs.faa.gov/browse/excelExternalWindow/B4BE7297FD3829D0862572F100550844.0001): Electronic Engine Control (EEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2101144-6 · 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
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/36C90B91F89FD440862570AD0064BF75.0001): Element Assembly. Western Filter Corporation · PMA PQ1847NM · Replaces 897513-1 · Oct 29, 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
- [2118002-203](https://drs.faa.gov/browse/excelExternalWindow/A34E8996393FF1E086257132005C249B.0001): Digital Electronic Engine Control (DEEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2118002-203 · Feb 8, 2006
- [2101144-6](https://drs.faa.gov/browse/excelExternalWindow/7D252DE11E92693386257132005C226B.0001): Electronic Engine Control (EEC). ONTIC Engineering & Manufacturing Inc · PMA PQ1398NM · Replaces 2101144-6 · Feb 8, 2006
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/77EB253FB72F40E58625706F00754A4C.0001): Oil Filter Element. Western Filter Corporation · PMA PQ1847NM · Replaces 3070945-1 · Jun 30, 2005
- [334508WFC](https://drs.faa.gov/browse/excelExternalWindow/0459856674187CE48625706F00754CAA.0001): Oil Filter Element. Western Filter Corporation · PMA PQ1847NM · Replaces 897513-1 · Jun 30, 2005
- [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
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/C32FF103402DC1B0852570500055C0F8.0001): Element Assembly. Western Filter Corporation · Replaces 897513-1 · May 15, 2005
- [1-1497-701](https://drs.faa.gov/browse/excelExternalWindow/10ACB489F61F51BC862573C60056A574.0001): O Ring Face Seal. Rexnord Industries, LLC · PMA PQ2030CE · Replaces Honeywell (Allied Signal, Garrett)… · Feb 8, 2005
- [P-1008](https://drs.faa.gov/browse/excelExternalWindow/03B428C4DD8948D0852570500055C145.0001): Element Assembly. Western Filter Corporation · Replaces 897513-1 · Jan 4, 2004
- [334504WFC](https://drs.faa.gov/browse/excelExternalWindow/9FC9309BB2AD36F98525704D0059661D.0001): Oil Filter Element. Western Filter Corporation · Replaces 3070945-1 · Oct 20, 2003
- [3000002-4PR](https://drs.faa.gov/browse/excelExternalWindow/B77A1343432789B98525704A0053D22B.0001): Piston Ring. Precision Ring Inc · Replaces Garrett 3000002-4 · Oct 7, 2002

All of them: https://openairdocs.org/engine/honeywell-tfe731-3c/pma.md

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