# Alliedsign TFE731-3C - Type: Engine model (FAA registry) - Registry code: 02617 - Manufacturer (registry): ALLIEDSIGN - 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: 0 registered aircraft - Page: https://openairdocs.org/engine/alliedsign-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 None registered with this engine model now. ## 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 (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/alliedsign-tfe731-3c/pma.md --- 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.