# Pratt & Whitney JT15D-5 - Type: Engine model (FAA registry) - Registry code: 52379 - Manufacturer (registry): P & W - Model: JT15D-5 - Engine type: Turbo-fan - Power: 2,905 lb thrust - Data sheet: [TCDS E25EA](https://openairdocs.org/tcds/E25EA) (OpenAirDocs) - Holder: Pratt & Whitney Canada Corp. - Installed in: 1 registered aircraft - Page: https://openairdocs.org/engine/pratt-whitney-jt15d-5 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 2008-24-10](https://openairdocs.org/ad/2008-24-10): Fuel Control Hydro Mechanical Unit (HMU) P3 servo · Pratt & Whitney Canada JT15D-5, JT15D-5B, JT15D-5F and 1 more. Effective Jan 2, 2009 - [AD 91-01-03](https://openairdocs.org/ad/91-01-03): Hydromechanical Fuel Control Units · Pratt & Whitney Canada JT15D-5, PW118, PW118A and 3 more. Effective Jan 7, 1991 ## Information bulletins (advisory) (1) - [SAIB NE-07-03](https://openairdocs.org/saib/NE-07-03): Dual-engine flameouts. Issued Oct 12, 2006 ## Registered aircraft (1) - [N974AJ](https://openairdocs.org/aircraft/N974AJ): [Hix Aviation LLC](https://openairdocs.org/faa-owner/HIX%20AVIATION%20LLC), [Norman, OK](https://openairdocs.org/faa-place/OK/Norman), built 1996, S/N 5600349 ## 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 (953, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2026FA0000640](https://openairdocs.org/sdr/2026FA0000640), Aug 14, 2026: ENGINE. BIRD INGESTION. MASTER WARNING FOLLOWED BY LOSS OF OIL PRESSURE. ENGINE SHUT DOWN AND RETURNED TO KCCO. DISCOVERED BIRD STRIKE AND BENT FAN BLADES AFTER LANDING - [SDR 3N0A2025121800284](https://openairdocs.org/sdr/3N0A2025121800284), Dec 13, 2025: WINDSHIELD. DELAMINATED. THE RIGHT WINDSHIELD SHOWED SIGNS OF DELAMINATION SHORTLY AFTER DEPARTING PWN. AFTER LANDING AT BNA A PICTURE WAS SENT TO DIR. OF MAINTENANCE AND TRIP SUPPORT, - [SDR 2024FA0000040](https://openairdocs.org/sdr/2024FA0000040), Jan 16, 2024: DUCT. CRACKED. PILOT REPORTED GETTING THE "BL AIR DCT FAIL" LIGHT IN FLIGHT, DURING CRUISE OPERATION. DURING TROUBLESHOOTING, IT WAS NOTED THAT THE BLEED AIR TUBE THAT CONNECT - [SDR 2023F00225](https://openairdocs.org/sdr/2023F00225), Mar 25, 2023: TURBINE. OUT OF POSITION. RH AVIATION, LLC SENT ENGINE SERIAL NUMBER 108361 TO STANDARDAERO FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR FOUND METAL DEBRIS IN THE EXHAUST OF THE ENGIN - [SDR R3WA202108130001](https://openairdocs.org/sdr/R3WA202108130001), Aug 11, 2021: ENGINE. FLAMED OUT. AT 43000 AIRCRAFT WAS CROSSING A SMALL LINE OF WEATHER. ENCOUNTERED SOME MODERATE TURBULENCE. RIGHT ENGINE SHUT OFF. CREW DECLARED AN EMERGENCY AND STARTED A DE - [SDR YQSA2021062803](https://openairdocs.org/sdr/YQSA2021062803), Jun 26, 2021: ENGINE. LEAKING. CREW TOOK OFF FROM KSDL ON 6/26. ON CLIMB OUT, THEY FELT A COUPLE OF THUMPS, LEFT ENGINE OIL TEMP INCREASED. CREW PULLED POWER BACK AND TURNED BACK. LEFT ENGINE - [SDR 2021FA0000289](https://openairdocs.org/sdr/2021FA0000289), Mar 25, 2021: IGNITER. CRACKED. REMOVED IGNITER FOR INSPECTION, FOUND A CRACK 180 DEGREES AROUND THE BASE OF THE IGNITER ABOVE THE THREADS AND BELOW THE HEX AREA. - [SDR 9JLA2021021227023](https://openairdocs.org/sdr/9JLA2021021227023), Feb 6, 2021: ANTI-ICE VALVE. DEFECTIVE. THE FLIGHT CREW REPORTED A RIGHT ENGINE TEMP LOW ANNUNCIATOR WHILE IN FLIGHT AND REMAINED ILLUMINATED WITH N2 AT 82%. THEY INDICATED THE ITT DID SHOW A RISE DUR - [SDR DBCA202102040001](https://openairdocs.org/sdr/DBCA202102040001), Feb 4, 2021: ANTI-ICE VALVE. FAILED. AFTER TAKE-OFF CREW NOTED RT ENGINE ANTI-ICE FAIL INDICATION. CREW RETURNED TO HOME BASE. MX TROUBLESHOT. REPLACED RT ENGINE INLET ANTI-ICE SOLENOID VALVE WITH - [SDR 9JLA2020120824759](https://openairdocs.org/sdr/9JLA2020120824759), Nov 18, 2020: ENGINE. INOPERATIVE. A FLIGHT WAS CANCELLED DUE TO THE CREW NOT BEING ABLE TO START THE NR 1 ENGINE. THE MAINTENANCE TEAM TROUBLESHOT, BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY. A - [SDR T17A20200811041](https://openairdocs.org/sdr/T17A20200811041), Sep 23, 2020: ANGLE. CRACKED. RIGHT TR FAN DUCT ANGLE CRACKED. REMOVED AND REPLACED TR FAN DUCT ANGLE, IAW HAWKER 400XP CMM 78-30-07. - [SDR T17A20200811031](https://openairdocs.org/sdr/T17A20200811031), Aug 11, 2020: INLET. CRACKED. DURING SCHEDULED MX FOUND RT ENGINE INLET AT 9 O'CLOCK POSITON CRACKED. INSTALLED SERVICABLE R/H ENGINE INLET DUCTL - [SDR 2HGR2020012301](https://openairdocs.org/sdr/2HGR2020012301), Jan 12, 2020: CONTROLLER. INTERMITTENT. CREW WAS RE-POSITIONING N233MW FROM KSBA TO KCRQ. DURING THE TAKE-OFF PHASE, THE CREW NOTICED A FLASHING MASTER CAUTION WARNING AND THE R EFC OFF ANNUNCIATIOR I - [SDR CA190219004](https://openairdocs.org/sdr/CA190219004), Jan 30, 2019: FCU. MALFUNCTIONED. (CAN) PILOT REPORTED THAT ON DOWNWIND, ENGINE ROLLED BACK FROM IDLE TO 24%. THEN, WHEN PILOT WAS ON FINAL APPROACH, THE ENGINE COMPLETELY CEASED TO PRODUCE POWE - [SDR 2019F00107](https://openairdocs.org/sdr/2019F00107), Jan 4, 2019: FUEL LINE. DEFECTIVE. IN MAINTENANCE DURING ENGINE INSPECTION AND THE FUEL BOOST PUMP ON, A VERY TINY STREAM OF FUEL (ABOUT THE SIZE OF A FINE HAIR) WAS FOUND SPRAYING FROM THIS LINE - [SDR ESMR201707130001](https://openairdocs.org/sdr/ESMR201707130001), Jul 12, 2017: OIL CAP. CRACKED. DURING THE DEPARTURE, CLIMBING THROUGH FL240, WHEN THE OIL PRESSURE ON THE LEFT ENGINE STARTED DROPPING. THE MASTER WARNING LIGHT AND THE LOW OIL PRESSURE ANNUN - [SDR T17A201706134022](https://openairdocs.org/sdr/T17A201706134022), Jun 10, 2017: ENGINE. MALFUNCTIONED. DURING CRUISE FLIGHT AT 39,000 FT, CREW RECEIVED THE MASTER WARNING ANNUNCIATION, ACCOMPANIED BY A LT FUEL PRESSURE LOW LIGHT WITH IMMEDIATE ROLL BACK OF THE NR - [SDR 2017FA0000194](https://openairdocs.org/sdr/2017FA0000194), May 17, 2017: SWITCH. OUT OF LIMITS. DURING TROUBLESHOOTING OF THE ANTI-ICE SYSTEM, THE ENGINE ANTI-ICE TEMP SWITCH WAS FOUND OUT OF LIMITS ON THE INDICATION. THE SWITCH WAS REPLACED WITH NEW. - [SDR CVGA20170406001](https://openairdocs.org/sdr/CVGA20170406001), Apr 4, 2017: ENGINE. SHUTDOWN. NORMAL CLIMB THROUGH 10,000 FEET. ONCE WE PAST 18,000 FEET, THE AIRPLANE YAWED TO THE LEFT, I TOOK CONTROL AND AT THE SAME TIME I LOOKED AT MY ENGINE GAUGED FRO - [SDR PAIR20170308S3720](https://openairdocs.org/sdr/PAIR20170308S3720), Mar 8, 2017: ENGINE. MAKING METAL. DURING PRE-PURCHASE SURVEY, INSPECTED ENGINE OIL FILTER AND FOUND LARGE AMOUNT OF METAL DEBRIS. ENGINE REMOVED FROM SERVICE AND SENT TO OVERHAUL FACILITY FOR RE - [SDR T17A201604154013](https://openairdocs.org/sdr/T17A201604154013), Apr 12, 2016: ENGINE. POWER LOSS. PILOT REPORTED RT ENG EXPERIENCED SLOW ROLLBACK ON BASE & FINAL APPROACH. THE APPROACH & LANDING WERE UNEVENTFUL. AFTER LANDING THE ENG WAS SECURED. PERFORMED N - [SDR T17A201603224011](https://openairdocs.org/sdr/T17A201603224011), Mar 17, 2016: FASTENER. SHEARED. A LOCK FASTENER WAS NOTED MISSING FROM THE RT ENG INLET. UPON FURTHER INSPECTION, ENG FAN BLADE DAMAGED & COMPRESSOR VANE DAMAGE WAS FOUND. ENG IS BEING REMOVED - [SDR 2016FA0000136](https://openairdocs.org/sdr/2016FA0000136), Mar 15, 2016: STARTER GEN. FAILED. RIGHT STARTER GENERATOR FAILED IN FLIGHT, ACFT RETURNED TO BASE REMOVED RT STARTER GENERATOR AND FOUND THE FORWARD BEARING NEXT TO THE COOLING FAN FAILED. - [SDR CA160302004](https://openairdocs.org/sdr/CA160302004), Feb 23, 2016: HMU. MALFUNCTIONED. (CAN) CUSTOMER REPORTED NR 1 ENGINE BARELY MAKES TAKE OFF OF THE DAY AND THEN ROLLS BACK ONE PERCENT. THE ENGINE HAS JUST RECEIVED FROM AN HOT SECTION INSPECTIO - [SDR CA160205002](https://openairdocs.org/sdr/CA160205002), Feb 2, 2016: GROUND STUD. CORRODED. (CAN) DURING A POST FLIGHT INSPECTION OF THE ACFT IT WAS OBSERVED THAT THE SIDE OF THE FUSELAGE, ADJACENT THE EXTERNAL POWER PLUG WAS WARN TO TOUCH. INVESTIGATI - [SDR CA151229002](https://openairdocs.org/sdr/CA151229002), Dec 20, 2015: OIL FILTER. BYPASSING. (CAN) WHILE GETTING READY FOR TAKEOFF, THE CREW REPORTED THAT THE OIL FILTER BYPASS INDICATION CAME ON MOMENTARILY AND WENT OUT WITH A CORRESPONDING SPIKE IN OI - [SDR CA151201007](https://openairdocs.org/sdr/CA151201007), Nov 25, 2015: ENGINE. SHUTDOWN. (CAN) FLYING LEVEL AT FL 360, PILOT NOTICED A VIBRATION ON THE ACFT, FOLLOWED BY THE MESSAGE RT GENERATOR OFF, GENERATOR RESET PERFORMED AND THE SYS WORKED FOR - [SDR CA151130007](https://openairdocs.org/sdr/CA151130007), Nov 14, 2015: FLOW DIVIDER. DEFECTIVE. (CAN) THE ENGINE HAD AN UNCOMMANDED FLAMEOUT ON APPROACH AT AROUND 2000 FT. ACFT LANDED UNEVENTFULLY. AFTER TROUBLESHOOTING, IT WAS DECIDED TO REPLACE THE FUEL - [SDR CA151029011](https://openairdocs.org/sdr/CA151029011), Oct 15, 2015: ENGINE. SHUTDOWN. (CAN) DURING DESCENT THROUGH APPROXIMATELY 2500, THE ENGINE SHUT ITSELF DOWN FROM A SETTING OF 5-10 PERCENT ABOVE FLIGHT IDLE. THE WARNING INDICATIONS CAME ON W - [SDR CA151029012](https://openairdocs.org/sdr/CA151029012), Oct 13, 2015: UNKNOWN. SMOKE. (CAN) THE CREW REPORTED SMOKE IN THE COCKPIT DURING TAKEOFF. THEY ELECTED TO RETURN TO THE POINT OF DEPARTURE WHERE A SAFE LANDING WAS MADE. POST FLIGHT ENGINE - [SDR CA150817005](https://openairdocs.org/sdr/CA150817005), Aug 4, 2015: ENGINE. FLAMED OUT. (CAN) AT FLIGHT LEVEL 45000 FEET, BOTH LEFT AND RIGHT HAND ENGINE FLAMEOUT THE MOMENT PILOT REDUCED POWER TO BEGIN DESCENT. PILOT HAD UNSUCCESSFUL ATTEMPTS OF R - [SDR CA150727009](https://openairdocs.org/sdr/CA150727009), Jul 15, 2015: ENGINE. MALFUNCTIONED. (CAN) THE PILOT REPORTED THAT DURING FLIGHT AT CRUISE, THE LT ENGINE POWER INCREASES BY ITSELF. THE PILOT MUST REDUCE THE POWER WITH THE THROTTLE TO MATCH THE R - [SDR 9JLA201504038653](https://openairdocs.org/sdr/9JLA201504038653), Mar 23, 2015: PRESSURE SWITCH. DEFECTIVE. DURING LANDING THE RT THRUST REVERSER ARM LIGHT TESTS, BUT DOES NOT ILLUMINATE WHEN THE THRUST REVERSER SYS WAS ARMED. THRUST REVERSER OPERATION WAS REPORTED TO - [SDR VIB42015FA0000091](https://openairdocs.org/sdr/VIB42015FA0000091), Mar 17, 2015: PCB. DEACTIVATED. IGNITER WOULD NOT FUNCTION, NO POWER TO UNIT. NO POWER TO UNIT IN IGNITER ON OR STANDBY POSITION OR DURING START. ENGINE LIP HEAT VALVE NOT POWERED WITH BATTERY - [SDR CA150325011](https://openairdocs.org/sdr/CA150325011), Mar 10, 2015: ENGINE. FLAMED OUT. (CAN) FOLLOWING THROTTLE REDUCTION TO IDLE DURING DESCENT THE ENGINE FLAMED OUT. THE PILOT WAS ABLE TO RESTART THE ENGINE WHICH FLAMED OUT AGAIN TWICE WHILE BRI - [SDR CA150128005](https://openairdocs.org/sdr/CA150128005), Dec 18, 2014: ENGINE. MAKING METAL. (CAN) THE AIRCRAFT RETURNED FROM A SERIES OF FLIGHTS DEC 18/2014 . THE CREW REPORTED NO DEFECTS. DURING A POST/PRE-FLIGHT OF THE AIRCRAFT MAINTENANCE NOTED META - [SDR CA140908014](https://openairdocs.org/sdr/CA140908014), Aug 28, 2014: ENGINE. POWER LOSS. (CAN) THE PILOT REPORTED AN UNCOMMANDED POWER ROLLBACK AND IFSD OF NR 2 ENGINE ON APPROACH. UNEVENTFUL SINGLE ENGINE LANDING WAS CARRIED OUT. THE PILOT ATTEMPTE - [SDR 2014FA0000611](https://openairdocs.org/sdr/2014FA0000611), Aug 26, 2014: DISPLAY. FAILED. ON OUR ABOVE DATED FLIGHT, WE DISCOVERED THE LOSS OF 2 DU-870 EFIS DISPLAYS. AT FIRST THE MFD WENT BLANK AND ABOUT 15 MINUTES LATER PFD NR 2 FAILED AND WENT BLA - [SDR R3W2014F00001](https://openairdocs.org/sdr/R3W2014F00001), Aug 25, 2014: COUPLING. SEPARATED. DURING CLIMB TO 38,000 FT TO FLIGHT LEVEL OF 40,000 FT, THE CABIN STARTED TO CLIMB 2000 FT PER MINUTE. CAPTAIN DECLARED AN EMERGENCY AND DESCENDED TO A SAFE OXY - [SDR 9JLA2014081304054](https://openairdocs.org/sdr/9JLA2014081304054), Aug 2, 2014: WIRE HARNESS. DEFECTIVE. THE LT ENG ANTI-ICE ANNUNCIATOR WOULD NOT ILLUMINATE WHEN THE SYS WAS ACTIVATED. EXTENSIVE TROUBLESHOOTING FOUND THE LT ENG WIRING HARNESS PN 3052134-01 SN AA87 - [SDR R3WA2014082200001](https://openairdocs.org/sdr/R3WA2014082200001), Jul 26, 2014: SWITCH. BURNED. DURING TAXIING FOR TAKEOFF, A STRONG ODOR WAS DETECTED IN COCKPIT. CAPTAIN ELECTED TO RETURN TO THE TERMINAL BEFORE TAKEOFF. THE LANDING GEAR LIGHT SWITCH HAD S - [SDR CA140602019](https://openairdocs.org/sdr/CA140602019), May 19, 2014: ENGINE. MALFUNCTIONED. (CAN) PILOT ABORTED TAKEOFF DURING TAKEOFF ROLL DUE TO UNCOMMANDED ACCELERATION. PILOT SECURED THE ENGINE AND RETURNED TO RAMP. - [SDR CA140508003](https://openairdocs.org/sdr/CA140508003), May 5, 2014: ELBOW. FAILED. (CAN) DURING CLIMB OUT ITT ON LT ENGINE APPROACHED UPPER LIMIT. ACFT RETURNED TO BASE. ON APPROACH ENGINE IGNITERS WERE SELECTED BUT LT SIDE DID NOT INDICATE TH - [SDR 9JLA2014050604051](https://openairdocs.org/sdr/9JLA2014050604051), May 2, 2014: WIRE HARNESS. INTERMITTENT. DURING THE CLIMB AFTER TAKEOFF THE CREW REPORTED THAT THE LT EFC FAILED. ONCE THE ACFT WAS IN CRUISE FLIGHT THE EFC WAS RESET & NO FAULTS WERE NOTED UNTIL THE D - [SDR CA140401006](https://openairdocs.org/sdr/CA140401006), Mar 27, 2014: WARNING LIGHT. ILLUMINATED. (CAN) DURING TAKEOFF ROLL, AN EEC INDICATION LIGHT OCCURRED FOLLOWED BY A N1 ROLLBACK. THE PILOTS SECURED THE ENGINE, AND TAXIED BACK TO HANGAR. EEC TROUBLESHOO - [SDR CA140326013](https://openairdocs.org/sdr/CA140326013), Mar 17, 2014: OIL SYSTEM. LOW PRESSURE. (CAN) THE PILOT SHUTDOWN THE ENGINE IN CRUISE DUE TO LOW OIL PRESSURE. THE ENGINE WAS SECURED FOLLOWED BY A UNEVENTFUL LANDING. IT WAS REPORTED 3 OIL QUARTZ WER - [SDR CA140313008](https://openairdocs.org/sdr/CA140313008), Mar 10, 2014: FLOAT VALVE. UNSERVICEABLE. DURING SINGLE POINT REFUELING, FUEL LEAKED OUT OF THE LT NACA VENT. FOUND THE LT VENT FLOAT VALVE FAILED CLOSED. THE SCREW ATTACHING THE VALVE FLAP TO THE FLOAT - [SDR CA140313006](https://openairdocs.org/sdr/CA140313006), Feb 28, 2014: ENGINE. SMOKE. ACFT WAS ON TAXI PREPARING FOR TAKEOFF WHEN CONTROL TOWER CONTACTED THE PILOT TO ADVISE OF SIGNIFICANT SMOKE FROM LT ENGINE EXHAUST. PILOT SECURED ENGINE AND RE - [SDR CA140224009](https://openairdocs.org/sdr/CA140224009), Feb 15, 2014: ENGINE. POWER LOSS. (CAN) WHILE TAXIING FOR A REGULAR FLIGHT THE NR 2 ENGINE POWER ROLLED BACK AND IT FLAMED OUT. TROUBLESHOOTING IS ONGOING. - [SDR CA140203006](https://openairdocs.org/sdr/CA140203006), Jan 26, 2014: DUCT. CONTAMINATED. (CAN) THE CREW ABORTED A MISSION DUE TO FUMES AND A STRONG OIL ODOR COMING FROM THE BLEED AIR SYSTEM. DECLARED AN IN-FLIGHT EMERGENCY, IFE AND LANDED WITHOUT IN All 953: https://openairdocs.org/engine/pratt-whitney-jt15d-5/reports.md ## STCs that may be installed (OpenAirDocs) (1) 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 SE01232AT](https://openairdocs.org/stc/SE01232AT): Installation of Unison Ignition Lead, P/N 10-395428-3, 38.5-inch Type 3 Ignition Lead. Unison Industries ## PMA parts (OpenAirDocs) (418, 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. - [3013984CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198788985620261008195302.0001): Washer, Key. Core Parts LLC · PMA PQ05326NM · Replaces 3013984 · Sep 3, 2026 - [3015195CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196740150420261008195303.0001): Washer, Key. Core Parts LLC · PMA PQ05326NM · Replaces 3015195 · Sep 3, 2026 - [3013694CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178447794820261008195302.0001): Washer, Key. Core Parts LLC · PMA PQ05326NM · Replaces 3013694 · Sep 3, 2026 - [3030494CEM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109443755220261008134712.0001): Air Seal. Cobalt Engineering and Manufacturing LLC · PMA PQ00015EB · Replaces 3030494 · Jul 20, 2026 - [3102837-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197448929920260726233157.0001): Seal, Air,No. 3 Bearing Rotor. Core Parts LLC · PMA PQ05326NM · Replaces 3102837-01 · Jun 12, 2026 - [3038515CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180780805320260615130505.0001): Seal, Plain. Core Parts LLC · PMA PQ05326NM · Replaces 3038515 · May 26, 2026 - [3119009-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163936384320260615130505.0001): Seal, Air Bleed Valve. Core Parts LLC · PMA PQ05326NM · Replaces 3119009-01 · May 26, 2026 - [3100594-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134365135920260528133314.0001): Washer, Key. Core Parts LLC · PMA PQ05326NM · Replaces 3100594-01 · Apr 15, 2026 - [3030669CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145948082720260217163407.0001): Pin Support Combustion Chamber Liner. Core Parts LLC · PMA PQ05326NM · Replaces 3030669 · Jan 16, 2026 - [3039928CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID189388683020260108163244.0001): Gasket, Two-Hole. CORE PARTS LLC · PMA PQ05326NM · Replaces 3039928 · Oct 21, 2025 - [3039933CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179646143020260108163245.0001): Gasket, Cover, Accessory Gearbox. CORE PARTS LLC · PMA PQ05326NM · Replaces 3039933 · Oct 21, 2025 - [3116670-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178422989020260108163246.0001): Gasket, Six-Hole. CORE PARTS LLC · PMA PQ05326NM · Replaces 3116670-01 · Oct 21, 2025 - [3115556-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151362744620260108163245.0001): Gasket, Four-Hole. CORE PARTS LLC · PMA PQ05326NM · Replaces 3115556-01 · Oct 21, 2025 - [3116669-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151267014020260108163245.0001): Gasket. CORE PARTS LLC · PMA PQ05326NM · Replaces 3116669-01 · Oct 21, 2025 - [ST3230-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149026679120260108163246.0001): Gasket, Four-Hole. CORE PARTS LLC · PMA PQ05326NM · Replaces ST3230-01 · Oct 21, 2025 - [3116671-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112362113420260108163246.0001): Gasket, Two-Hole. CORE PARTS LLC · PMA PQ05326NM · Replaces 3116671-01 · Oct 21, 2025 - [ST3272-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101049268920260108163246.0001): Gasket, Four-Hole. CORE PARTS LLC · PMA PQ05326NM · Replaces ST3272-01 · Oct 21, 2025 - [3018981CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177922688320260108163137.0001): Washer, Lock. CORE PARTS LLC · PMA PQ05326NM · Replaces 3018981 · Oct 3, 2025 - [3029072CEM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182937838020250702145351.0001): Washer, Lock. Cobalt Engineering and Manufacturing LLC · PMA PQ00015EB · Replaces 3029072 · Jun 10, 2025 - [3034508WFC](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168792409620250624152910.0001): Oil Filter Element. Donaldson Company Inc · PMA PQ2432CE · Replaces 3034508 3036376, Alternate: 11-11064… · Jun 2, 2025 - [3116838-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175797840520250605164233.0001): Collar, Retaining, Blade. CORE PARTS LLC · PMA PQ05326NM · Replaces 3116838-01 · Apr 7, 2025 - [3115889-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID118797563520250605164233.0001): Rivet, Solid, Countersunk. CORE PARTS LLC · PMA PQ05326NM · Replaces 3115889-01 · Apr 7, 2025 - [TB05-1241100-D013](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186558540020250328114255.0001): Engine Seal Ring. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 3117494-01 · Feb 28, 2025 - [3015032CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146061651420250923190207.0001): Seal, Ring. CORE PARTS LLC · PMA PQ05326NM · Replaces 3015032 · Feb 13, 2025 - [3119476-01CP](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138194454120260108162955.0001): Washer, Key. CORE PARTS LLC · PMA PQ05326NM · Replaces 3119476-01 · Feb 7, 2025 - [TB05-1241100-D003](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID133935007820250212131844.0001): Washer, Lock, High Turbine Rotor. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 3029072 · Jan 16, 2025 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169774044220250106202801.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012411 · Dec 10, 2024 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164469161820250106202800.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012413 · Dec 10, 2024 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152753542620250106202759.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012414 · Dec 10, 2024 - [3012414AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117377138920250106202801.0001): Nut, Self-Locking, 12 Point. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012412 · Dec 10, 2024 - [TB05- 1241100- D011](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195101954120241204113845.0001): Shroud Segmen-H.T. Rotor,.268-.270. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 3041933CL34 · Nov 19, 2024 - [TB05- 1241100- D007](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID134536532320241204113844.0001): Shroud Segmen-H.T. Rotor,.252-.254. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 3041933CL26 · Nov 19, 2024 - [TB05- 1241100- D005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131525561220241204113843.0001): Shroud Segmen-H.T. Rotor,.240-.242. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 3041933CL20 · Nov 19, 2024 - [TB05- 1241100- D009](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID126272863520241204113845.0001): Shroud Segmen-H.T. Rotor,.260-.262. Aero Tech Aviation Design, LLC · PMA PQ04281CE · Replaces 3041933CL30 · Nov 19, 2024 - [3116838-01CEM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID132358678720250530141213.0001): Collar Blade Retainer. Cobalt Engineering and Manufacturing LLC · PMA PQ00015EB · Replaces 3116838-01 · Oct 8, 2024 - [TB05-1241100-D001](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160847149420241025164021.0001): Pin-Support Comb CHMBR Liner. Aero Tech Aviation Design LLC · PMA PQ04281CE · Replaces 3030669 · Sep 3, 2024 - [3012675AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID196954661720240919140845.0001): Nut, Self-Locking, Hex. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3012675, 3005816, 3012674, 3028286… · Aug 7, 2024 - [3015234AA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID130436253520240919140838.0001): Nut, Self-Locking, Shank. Aero Attitude, LLC · PMA PQ00001CB · Replaces 3015234, 3015233, 3015232, 3016299… · Aug 7, 2024 - [MS9952-26CEM](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111670084520240701174117.0001): Cup Washer. Cobalt Engineering and Manufacturing LLC · PMA PQ00015EB · Replaces MS9952-26 · Jun 10, 2024 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198859662920240129140712.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192841579020240129140713.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178769232220240129140713.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176833134520240129140708.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173366992220240129140713.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172389434320240129140708.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161162222320240129140710.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143996098620240129140714.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141871165220240129140709.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124431282120240129140710.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 - [No part number](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119518843120240129140711.0001): PTI Technologies Inc · PMA PQ1341NM · Dec 11, 2023 All of them: https://openairdocs.org/engine/pratt-whitney-jt15d-5/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.