# Pratt & Whitney JT8D-15A

- Type: Engine model (FAA registry)
- Registry code: 51731
- Manufacturer (registry): P & W
- Model: JT8D-15A
- Engine type: Turbo-fan
- Power: 15,500 lb thrust
- Data sheet: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Holder: Pratt & Whitney
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-jt8d-15a

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 2011-03-01](https://openairdocs.org/ad/2011-03-01): Critical life- limited parts · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 9 more. Effective Mar 4, 2011
- [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1): High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Nov 2, 2006
- [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16): Critical life-limited rotating parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Sep 30, 2005
- [AD 2003-12-07](https://openairdocs.org/ad/2003-12-07): 12th Stage high pressure compressor · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jul 18, 2003
- [AD 2003-05-07](https://openairdocs.org/ad/2003-05-07): Low pressure compressor (LPC) · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 17, 2003
- [AD 2001-15-18](https://openairdocs.org/ad/2001-15-18): Stage Compressor Disks · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Sep 4, 2001
- [AD 2000-22-06](https://openairdocs.org/ad/2000-22-06): Main Fuel Pump · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 8 more. Effective Dec 4, 2000
- [AD 99-01-08](https://openairdocs.org/ad/99-01-08): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT3D-1, JT3D-1-MC6, JT3D-1-MC7 and 30 more. Effective Jan 5, 1999
- [AD 98-21-24](https://openairdocs.org/ad/98-21-24): Compressor Disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Nov 16, 1998
- [AD 98-04-39](https://openairdocs.org/ad/98-04-39): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Feb 25, 1998
- [AD 96-23-14](https://openairdocs.org/ad/96-23-14): Combustion Chamber Outer Cases · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 2, 1997
- [AD 95-26-03](https://openairdocs.org/ad/95-26-03): High Pressure Compressor Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Jan 11, 1996
- [AD 86-09-02 R2](https://openairdocs.org/ad/86-09-02-R2): Combustion Chamber Liners · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 17, 1995
- [AD 95-16-07](https://openairdocs.org/ad/95-16-07): High Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 11 more. Effective Sep 11, 1995
- [AD 95-10-10](https://openairdocs.org/ad/95-10-10): Compressor Fan Hub · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jul 21, 1995
- [AD 94-25-07](https://openairdocs.org/ad/94-25-07): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Mar 30, 1995
- [AD 95-02-16](https://openairdocs.org/ad/95-02-16): Fuel Nozzle and Support Assembly · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Feb 21, 1995
- [AD 94-20-09](https://openairdocs.org/ad/94-20-09): Low Pressure Turbine Blade Sets · Pratt & Whitney Division JT8D-15A, JT8D-17A and JT8D-17AR. Effective Nov 14, 1994
- [AD 91-24-14](https://openairdocs.org/ad/91-24-14): Bearing Seal Spacer · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jan 21, 1992
- [AD 89-25-11](https://openairdocs.org/ad/89-25-11): Fan Blade Retaining Plates · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Jan 15, 1990
- [AD 86-08-04 R1](https://openairdocs.org/ad/86-08-04-R1): HPC Removable Sleeve Spacers · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Nov 4, 1986
- [AD 86-02-52 R1](https://openairdocs.org/ad/86-02-52-R1): Combustion Chamber · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 12 more. Effective Apr 14, 1986
- [AD 78-17-02 R3](https://openairdocs.org/ad/78-17-02-R3): Compressor Front Hubs · Pratt & Whitney Division JT8D-11, JT8D-15, JT8D-15A and 6 more. Effective Mar 30, 1984
- [AD 75-05-06](https://openairdocs.org/ad/75-05-06): Fuel Manifold Leakage · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Feb 24, 1977
- [AD 70-26-05](https://openairdocs.org/ad/70-26-05): First Stage Compressor Rotor Blades · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 29, 1970
- [AD 70-25-08](https://openairdocs.org/ad/70-25-08): Seventh Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 15, 1970
- [AD 70-11-03](https://openairdocs.org/ad/70-11-03): Sixth Stage Compressor Discs · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jun 12, 1970
- [AD 70-02-02](https://openairdocs.org/ad/70-02-02): Sixth Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Apr 15, 1970

## Registered aircraft (1)

- [N289MT](https://openairdocs.org/aircraft/N289MT): [Raytheon Co](https://openairdocs.org/faa-owner/RAYTHEON%20CO), [Ontario, CA](https://openairdocs.org/faa-place/CA/Ontario), built 1981, S/N 22467

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (3)

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

- [Incident 19990507015189I](https://openairdocs.org/incident/19990507015189I), May 7, 1999: Boeing 737200 (N309DL), Kansas City, MO. Delta express airlines flight 2587 returned to Kansas City International Airport on 5-7-99 at 19:95. The return was due to a popping noise followed by a…
- [Incident 19970521019239I](https://openairdocs.org/incident/19970521019239I), May 21, 1997: Boeing 737232 (N309DL), Jacksonville, FL. Encountered severe weather turbulence. Flight attendants and passengers suffered minor injuries.
- [Incident 19910921045789I](https://openairdocs.org/incident/19910921045789I), Sep 21, 1991: Boeing 737232 (N309DL), Covington - Cin, OH. Airframe vibration on climbout. Diverted and landed. Replaced missing hardware on left pack ram door.

## Service difficulty reports (538, newest 50)

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

- [SDR NACA2017072000044](https://openairdocs.org/sdr/NACA2017072000044), Jul 18, 2017: ENGINE. FAILED. NR 2 ENGINE FAILED AT 2000 FEET ON TAKEOFF. MI AT 1705 FEET DURING CLIMB, LOUD NOISE FROM NR 2 ENGINE, NO EPR, SMOKE IN COCKPIT, AND ENGINE VIBRATION. NR 2 ENGI
- [SDR K11A2016080391601](https://openairdocs.org/sdr/K11A2016080391601), Aug 1, 2016: WARNING LIGHT. ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN OF LEFT ENGINE DUE TO OIL PRESSURE LOW LIGHT, LOW OIL PRESSURE & ZERO ON OIL QUANTITY
- [SDR CA150805005](https://openairdocs.org/sdr/CA150805005), Jul 31, 2015: PULLEY BRACKET. BROKEN. (CAN) DURING A DAILY SERVICE CHECK THE MECHANIC FOUND THE RT MLG DOOR WOULD NOT OPEN USING THE MANUAL RELEASE. VISUAL INSPECTION OF THE SYS FOUND THE PULLEY BRA
- [SDR K11A2014122200001](https://openairdocs.org/sdr/K11A2014122200001), Dec 19, 2014: SHAFT. SHEARED. FUEL PUMP DRIVE GEAR SHAFT SHEARED, CAUSING ENGINE TO FLAME OUT.
- [SDR NACA201411140001](https://openairdocs.org/sdr/NACA201411140001), Nov 4, 2014: SLEEVE. LEAKING. NR 1 ENGINE SHUTDOWN DOWN DUE TO LOSS OF OIL PRESSURE. ENGINE MAIN OIL FILTER HOUSING ON GEARBOX SLEEVE BORE REPAIR LEAKING AT MATING SURFACES. REMOVED REPAIR S
- [SDR PCSA2014060501](https://openairdocs.org/sdr/PCSA2014060501), Jun 5, 2014: COMPRESSOR. STALLED. AT 3500’ NR 3 ENG COMPRESSOR STALL. RETARDED THRUST, SLOWLY INCREASED THRUST, COMPRESSOR STALLED AGAIN. THRUST AT IDLE, RETURNED TO MIAMI.
- [SDR CA131018009](https://openairdocs.org/sdr/CA131018009), Oct 16, 2013: HOUSING. DAMAGED. (CAN) DURING TROUBLESHOOTING OF A L/E FLAP/SLAT DEFECT, UPON CYCLING FLAPS UP & DOWN HYD SYSTEM "A" MODULE CHECK VALVE FAILED, THREADED CHECK VALVE DEPARTED THE
- [SDR CA130912006](https://openairdocs.org/sdr/CA130912006), Sep 9, 2013: BLADES. FAILED. (CAN) ON ENGINE THROTTLE UP FOR TAKE OFF CREW REPORTED A BANG ON NR 2 ENGINE WITH HIGH EGT AND LOSS OF THRUST. TAKEOFF ABORTED WITHOUT INCIDENT. MAINTENANCE FOU
- [SDR 7AHR201308072272](https://openairdocs.org/sdr/7AHR201308072272), Aug 7, 2013: SKIN. CORRODED. NR 1 ENGINE OTB COWL HAS CORROSION. INSTALLED REPAIR IAW SRM 51-30-02.
- [SDR 7AHR201308072305](https://openairdocs.org/sdr/7AHR201308072305), Aug 7, 2013: CHANNEL. CHAFED. NR 1 OTBD ENGINE COWL ZEE CHANNEL CHAFED 45" FROM AFT END UPPER. INSTALLED REPAIR IAW SRM 51-40-3, PG 1.-6.
- [SDR NACA201305230001](https://openairdocs.org/sdr/NACA201305230001), May 23, 2013: INDICATOR. FAULTY. ABORTED TAKEOFF DUE TO INTERMITTENT EGT NR 1 GAUGE. REMOVED AND REPLACED INDICATOR.
- [SDR NACA2013051000001](https://openairdocs.org/sdr/NACA2013051000001), May 10, 2013: ENGINE. FAILED. NR 1 ENGINE FAILURE IN FLIGHT, ENGINE SHUT DOWN. REMOVED AND REPLACED ENGINE DUE TO TURBINE FAILURE.
- [SDR NACA2013040900001](https://openairdocs.org/sdr/NACA2013040900001), Apr 9, 2013: TRANSMITTER. FAULTY. TAKEOFF WAS ABORTED AT 90KTS DUE TO EXCESSIVE FUEL FLOW INDICATION ON NR 2 ENGINE. REPLACED NR 2 ENGINE FUEL FLOW TRANSMITTER, REF: B737-200MM 73-31-11.
- [SDR NACA2013032700001](https://openairdocs.org/sdr/NACA2013032700001), Mar 27, 2013: OIL FILTER. DIRTY. ABORTED TAKEOFF DUE TO NR 1 ENGINE OIL FILTER BY-PASS LIGHT ILLUMINATING DURING TAKEOFF ROLL. REPLACED MAIN OIL FILTER. RAN ENGINE, NO LEAKS NOTED. P&WMM 72-61-
- [SDR CA130308011](https://openairdocs.org/sdr/CA130308011), Mar 7, 2013: TURBINE BLADES. FAILED. (CAN) CREW REPORTED UPON ADVANCING THRUST ON TAKEOFF ROLL NR 1 ENGINE FAILED. TAKEOFF ABORTED ACFT RETURNED TO GATE WITH OUT INCIDENT. UPON MAINTENANCE INVESTIG
- [SDR NACA20130116001](https://openairdocs.org/sdr/NACA20130116001), Jan 15, 2013: SEAL. FAILED. MECHANICAL INTERUPTION,NR 1 ENGINE SHUTDOWN IN FLIGHT DUE TO LOSS OF OIL QUANTITY AND DECREASE IN OIL PRESSURE. WINDMILL TIME APPROX. 3-4 MINUTES WITH OIL PRESS
- [SDR NACA20121129001](https://openairdocs.org/sdr/NACA20121129001), Nov 29, 2012: ENGINE. FAULTY. NR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE. REPLACING ENGINE AT THIS TIME.
- [SDR SPAA2012080800001](https://openairdocs.org/sdr/SPAA2012080800001), Aug 6, 2012: SLIDING WINDOW. CRACKED. PREFLIGHT CHECK, CAPTAIN'S NR 2 SLIDING WINDOW SHOWS SIGNS OF INTERLAYER CRACKING. REPLACED WINDOW IAW AMM 56-12-11.
- [SDR CA120112007](https://openairdocs.org/sdr/CA120112007), Jan 4, 2012: DUCT. CRACKED. (CAN) ON DECENT CREW OBSERVED NR 2 ENGINE FIRE WARNING INDICATION. COMPLETED FIRE DRILL, FIRE LIGHT STAYED ON, FIRE BOTTLE DISCHARGED. DECLARED EMERGENCY, LANDE
- [SDR K11A2011111572601](https://openairdocs.org/sdr/K11A2011111572601), Nov 15, 2011: PUMP. SHEARED. ENGINE NR 1 FLAME OUT DURING TAKEOFF AT 80 KNOTS, ALL PARAMETERS WERE NORMAL UNTIL FLAME OUT OCCURED. CREW ADVICED TOWER CLEARED RUNWAY AND RETURNED BACK TO BLO
- [SDR CA110802001](https://openairdocs.org/sdr/CA110802001), Jul 28, 2011: LINE. RUPTURED. DURING APPROACH ON SHORT FINAL THE ACFT HAD LOST ALL HYD FLUID IN SYS A. THE ACFT CONTINUED THE APPROACH AND LANDED WITHOUT FURTHER PROBLEMS. UPON POST-FLIGHT I
- [SDR NACA20110044](https://openairdocs.org/sdr/NACA20110044), Jun 15, 2011: TURBINE BLADES. DISINTEGRATED. NR 2 ENGINE FAILURE ON TAKEOFF ROLL (TURBINE SHELLED). REPLACEMENT OF ENGINE IN PROGRESS. TURBINE BLADES DISINTEGRATED. UNCLEAR WHY AT THIS TIME. DAMAGE CONTAIN
- [SDR K11A2011042072601](https://openairdocs.org/sdr/K11A2011042072601), Apr 20, 2011: SHAFT. SHEARED. ENGINE NR 2 LOW OIL PRESSURE LIGHT CAME ON IN FLIGHT, OIL PRESSURE GAUGE ALSO INDICATED NO OIL PRESSURE, CREW PERFORMED PRECAUTIONARY ENGINE SHUTDOWN IAW PROCED
- [SDR SPAA1000009](https://openairdocs.org/sdr/SPAA1000009), Oct 22, 2010: STRUCTURE. CRACKED. RT OTBD MIDFLAP INBD THRUST BEARING BORE HAS CRACK AT 3 O'CLOCK POSITION. REPLACED FLAP WITH O/H SERVICEABLE UNIT IAW AMM.
- [SDR FDEA201009023244](https://openairdocs.org/sdr/FDEA201009023244), Sep 2, 2010: RELAY. BURNED. DURING COCKPIT PREFLIGHT, NOTICED HEAVY WHITE SMOKE COMING FROM OVERHEAD CONTROL PANEL. ADVISED 2ND OFFICER TO REMOVE ELECTRICAL POWER FROM ACFT. ADVISED CREW T
- [SDR PCSA2010083001](https://openairdocs.org/sdr/PCSA2010083001), Aug 27, 2010: TUBE. LEAKING. NUMBER 1 ENGINE OIL QUANTITY STEADILY DECREASED DURING FLIGHT. ALSO OIL TEMP EXCESSIVE. ONLY DROPPED DURING POWER BACK. MAINTENANCE FOUND THE NUMBER 6 BEARING O
- [SDR NACA20100005](https://openairdocs.org/sdr/NACA20100005), Aug 24, 2010: LINE. LEAKING. NR 2 ENGINE POWER LOSS, ENGINE SHUT DOWN. REMOVED PRESSURIZING & DUMP VALVE, REPLACED LEAKING LINE AND RE-INSTALLED P&D VALVE. OP & LEAK CHECK GOOD. REF: P&W MM
- [SDR KNNA2497232010CMH](https://openairdocs.org/sdr/KNNA2497232010CMH), Jul 23, 2010: PUMP. FAILED. FAR 91 MX FERRY KACY-KSLC-KMER FOR C-CHECK, AT FL360 NR 2 RIGHT ENGINE SHUTDOWN, FUEL FLOW 0 N1, N2, & OIL PRESS NORMAL. DIVERTED TO KCMH.
- [SDR 2010FA0000221](https://openairdocs.org/sdr/2010FA0000221), Feb 19, 2010: FUEL NOZZLE. BURNED. AS A RESULT OF BURNED T2 VANES, COMBUSTION MODULE DISASSEMBLED. NR 8 FUEL NOZZLE RETAINING NUT FOUND LOOSE WITH LOCK TAB INTACT. SEVERE BURN AWAY AREAS OF FUEL 
- [SDR FDEA201002090366](https://openairdocs.org/sdr/FDEA201002090366), Feb 9, 2010: ENGINE. POWER LOSS. DURING STANDARD PWR TAKEOFF AT 2000 FT, EXPERIENCED SUDDEN VIBRATION IN CTR PEDESTAL ACCOMPANIED BY ABNORMAL NOISE. DISCOVERED RETARDING NR 2 THROTTLE RESOLVED 
- [SDR CA090416004](https://openairdocs.org/sdr/CA090416004), Apr 8, 2009: MANIFOLD. CHAFED. (CAN) DURING MX RUN, FOUND SIGNIFIGANT FUEL LEAKING FROM NR 3 ENGINE "COLD STREAM" COWL. MX DETERMINED FUEL NOZZLE MANIFOLD CHAFED THROUGH ON HEAT SHROUD TO PRO
- [SDR NWAA09679759](https://openairdocs.org/sdr/NWAA09679759), Feb 28, 2009: FUEL SYS. MALFUNCTIONED. DURING TAKEOFF ENGINE NR 1 WAS SLOW TO REACH TAKEOFF POWER. DURING ROTATION AND CLIMB, ENG NR 1 EPR BEGAN TO DETERIORATE. ENGINE NR 1 FUEL FLOW WAS HIGHER THAN 
- [SDR FDEA200812015036](https://openairdocs.org/sdr/FDEA200812015036), Dec 1, 2008: PRESSURE SWITCH. MALFUNCTIONED. NR 1 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW PRESSURE/FILTER BYPASS LIGHT. COMPLIED WITH QRH ENGINE WINDMILLED 2 MIN PRIOR TO SHUT DOWN. OIL PRESSURE AT APPROX 40
- [SDR CA081112005](https://openairdocs.org/sdr/CA081112005), Nov 7, 2008: CONNECTOR. DAMAGED. (CAN) AT APPROX 700 FT, AGL T/O YHZ FIRE WARNING LIGHTS ON GLARE SHIELD WERE DIMMLY ILLUMINATED. NO AURAL WARNING. APU FIRE HANDLE ILLUMINATED. SWITCH PULLED AN
- [SDR CA080917003](https://openairdocs.org/sdr/CA080917003), Sep 16, 2008: SHUTOFF VALVE. FAILED. (CAN) DURING CLIMBOUT, SEPT 16 2008, PRESSURIZATION FAILED TO OPERATE NORMALLY. WHEN CLIMBING THROUGH 23,000 FT, CABIN ALTITUDE EXCEEDED 10000 FT. FUEL DUMP CAR
- [SDR PID2008F00006](https://openairdocs.org/sdr/PID2008F00006), Jul 13, 2008: SWITCH. DIRTY. OIL FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. SHUTDOWN RT ENGINE IAW QRH. DIVERTED FLT, INSPECTED NR 2 MAIN ENGINE OIL FILTER AND CLEANED BYPASS CONNECTOR SWIT
- [SDR CA080707002](https://openairdocs.org/sdr/CA080707002), Jul 5, 2008: INDICATOR. BROKEN. (CAN) AFTER TAKE-OFF WHEN RETRACTING FLAPS THE INBD FLAPS STUCK AT APPROXIMATELY 5 DEGREES WITH AN ASYMMETRY. THE ACFT DECLARED AN EMERGENCY WITH A FLAP PROBLEM
- [SDR NACA20080009](https://openairdocs.org/sdr/NACA20080009), May 14, 2008: ENGINE. OUT OF TRIM. NR 2 ENGINE NOT MAKING TAKEOFF THRUST. REJECTED TAKEOFF AT APPROXIMATELY 80 KNOTS. FOD INSPECTION COMPLETED WITH NO DEFECTS. FOUND ENGINES OUT OF TRIM. TRIMMED 
- [SDR DHLA200800038](https://openairdocs.org/sdr/DHLA200800038), Apr 4, 2008: ENGINE. VIBRATION. FLT NR 155 ON TAKEOFF ROLL LOUD BANG AUTO PACK TRIP AND ENG FAIL LIGHTS ILLUMINATE AT 70KTS. RTO, ALL ENG RUNNING W/IN NORM, PARAMETER. CLEARED AUTO PACK TRIP A
- [SDR C1HA200879001](https://openairdocs.org/sdr/C1HA200879001), Mar 16, 2008: ENGINE. OVERHEATED. ON TAKEOFF ROLL, ENGINES WERE BROUGHT TO 1.4 EPR THEN WERE BEING ADVANCED TO FLEX THRUST WHEN NR 2 ENGINE MADE A LOUD NOISE, FE CONFIRMED NR 2 ENGINE WAS AT 1.6
- [SDR KNNA20080003](https://openairdocs.org/sdr/KNNA20080003), Mar 8, 2008: ENGINE. FAILED. ACCORDING TO THE PILOT IN COMMAND’S REPORT, THEY HAD TO DEICE THE PLANE BEFORE TAKEOFF. THEN, ON TAKEOFF ROLL, DURING ROTATION, THERE WAS A LOUD BANG AND VIBRAT
- [SDR DHLA200800017](https://openairdocs.org/sdr/DHLA200800017), Feb 26, 2008: FCU. OUT OF ADJUST. FLT NR 385, 1 ENG WOULD NOT PRODUCE TAKEOFF EPR RTO WT 174.9 24 DEGED C PA-70 BRAKE ENERGY ZONE NORMAL IAS LESS THAN 60 NTS SWAPPED NR 1 AND 2 EPR GAUGES FOR TR
- [SDR SPAA0800096](https://openairdocs.org/sdr/SPAA0800096), Feb 15, 2008: POWER SUPPLY. INOPERATIVE. AFT SECTION OF FLOOR PATH ESCAPE LIGHTING INOPERATIVE. REPLACED FLOOR TRACK POWER SUPPLY IAW MM 33-21-27. OPS CHECK SATISFACTORY.
- [SDR DHLA200700093](https://openairdocs.org/sdr/DHLA200700093), Dec 27, 2007: OVERHEAT LOOP. MISROUTED. NR 1 STRUT OVERHEAT LIGHT AFTER T/O PERFORMED NORMAL SHUTDOWN NR 1 ENGINE PER PROCEDURE. FOUND 4 DUCT CONNECTIONS LEAKING ON DUCT FROM PRECOOLER TO THE ENG. REM
- [SDR NWAA073589993](https://openairdocs.org/sdr/NWAA073589993), Oct 28, 2007: ENGINE. MALFUNCTIONED. DURING FLIGHT, ENGINE NR 1 PARAMETERS WERE ERRATIC AND THROTTLE LEVER SPLIT OF 1.5 KNOBS. ENGINE NR 1 FLAMED OUT AT APPROX 14,000 FT. FLIGHT CREW DIVERTED AC TO
- [SDR NWAA073189967](https://openairdocs.org/sdr/NWAA073189967), Sep 14, 2007: ENGINE. SEIZED. DURING APPROACH AT 1000 FEET FLIGHT CREW HEARD A LOUD BANG AND FELT AIRCRAFT YAW. FLIGHT CREW LOG ENTRY STATES ENGINE "SEIZED" AND N1, N2 INDICATING 0. FLIGHT C
- [SDR CA070813002](https://openairdocs.org/sdr/CA070813002), Jul 30, 2007: PITOT TUBE. BLOCKED. (CAN) THE AIRCRAFT BEGAN TO DEPART ON THE TAKE-OFF ROLL WHEN THE FLIGHT CREW OBSERVED THAT THE CAPTAINS AIRSPEED INDICATION HAD FAILED. THE TAKE-OFF WAS ABORTED
- [SDR C8GA20070006](https://openairdocs.org/sdr/C8GA20070006), Jun 8, 2007: CONNECTOR. LOOSE. FLT 716 FROM TOL TO MEM, AFTER TAKEOFF, NR 2 ENGINE OIL TEMPERATURE PEGGED HIGH. CREW PERFORMED PRECAUTIONARY ENGINE SHUT DOWN, DECLARED EMERGENCY, AND RETURNED
- [SDR C8GA20070005](https://openairdocs.org/sdr/C8GA20070005), May 30, 2007: LINE. LEAKING. FLT 2819 FROM DFW TO TOL. DURING DESCENT INTO TOL, THE NR 1 ENGINE WAS UNRESPONSIVE TO THROTTLE MOVEMENT. AS PRECAUTIONARY NR 1 ENGINE WAS SHUTDOWN AND AN EMERG
- [SDR KNNA200700030](https://openairdocs.org/sdr/KNNA200700030), Apr 28, 2007: LEVER. BINDING. IN FLIGHT DURING DESCENT INTERMITTENTLY AT FIRST THEN STEADY PROCEDURES WERE FOLLOWED WITH THRUST LEVERS BINDING (RESTRICTED) ENGINE 1 WAS SHUTDOWN IAW CHECK LI

All 538: https://openairdocs.org/engine/pratt-whitney-jt8d-15a/reports.md

## STCs that may be installed (OpenAirDocs) (15)

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 SE2930SO](https://openairdocs.org/stc/SE2930SO): Installation of an alternate gearbox cover seal utilizing an aluminum retainer .040-inch thick with a molded-in-place elastomeric seal contoured to fit the main housing/cover flange interface. Parker O-Seal Division. Lists JT8D Series
- [STC SE3916NM](https://openairdocs.org/stc/SE3916NM): Installation of CADC bleed valve supports brackets, P/N B10002 or RB10003, as a replacement part for P&W P/N 578273. Aeroparts Mfg & Repair. Lists JT8D Series
- [STC SE79WE](https://openairdocs.org/stc/SE79WE): Installation of CADC bleed valve support brackets, P/N B10001 or RB10006, as a replacement part for P&W P/N 493317 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Aeroparts Mfg & Repair. Lists JT8D Series
- [STC SE00049AT-D](https://openairdocs.org/stc/SE00049AT-D): Installation of Intermediate Compressor Case (JT8D SERIES). Aero Component Technologies. Lists JT8D Series
- [STC SE00048AT-D](https://openairdocs.org/stc/SE00048AT-D): Modification of compressor intermediate case diaphragm to permit acceptable of a 7th stage airseal ring. Aero Component Technologies
- [STC SE59GL](https://openairdocs.org/stc/SE59GL): Installation of O-ring face seal P/N-s 1-1337-700, -701, 1-1633-700, -701, 1-1738-700, -701; and/or 1-2233-700, 701. Rexnord, Inc
- [STC SE86WE](https://openairdocs.org/stc/SE86WE): Replace the airoils on P&WA P/Ns 495051, 478351, 583751, 653851, 653951, 572451, 583351, 653751, 653151, 676951, 728951, 709951, 710751, 627751, 737271, 578551, 738271, 747171, 792871, 786471, 583751, 777971, 780591, 782571, 793181, 799771, 794481, 794491 , 798781, and 799191. Chromizing Company
- [STC SE557NE](https://openairdocs.org/stc/SE557NE): Installation of oil tank shuttle valve. Stockbridge William D
- [STC SE2666SO](https://openairdocs.org/stc/SE2666SO): Modification of the anti-ice mount bracket. Cook Airtomic
- [STC SE593NE](https://openairdocs.org/stc/SE593NE): Installation of a Select Controls Inc. Engine Oil Shuttle Valve, P/N 2057-1-001. (See Eligibility List). Basken Valve Corporation. Lists JT8D Series
- [STC SE1930SO](https://openairdocs.org/stc/SE1930SO): Installation of power control shaft bushing. Cook Airtomic Division. Lists JT8D Series
- [STC SE83WE](https://openairdocs.org/stc/SE83WE): Installation of heat shield assembly P/N 408-007 as a replacement part for P&W P/N499941 or 749609 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series
- [STC SE84WE](https://openairdocs.org/stc/SE84WE): Installation of heat shield assembly 408-008 as a replacement part for P&W No. 586918 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series
- [STC SE67WE](https://openairdocs.org/stc/SE67WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series
- [STC SA2627WE](https://openairdocs.org/stc/SA2627WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series

## PMA parts (OpenAirDocs) (over 1,000, 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.

- [E741346](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186556581720260305201741.0001): Lock- Compressor Blade. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 741346 · Oct 31, 2024
- [811086](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172993763520260305193806.0001): Housing Assy – Gearbox, Front. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 811086 · Oct 31, 2024
- [774403](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170344065020260305193807.0001): Blade – Turbine Rotor, 3 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 774403 · Oct 31, 2024
- [E655421](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161625986720260305201740.0001): Washer – Key, Turbine Rotor, 2 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 655421 · Oct 31, 2024
- [466750](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151358703220260305193807.0001): Ring – Oil Sealing, Compressor Rear Bearing. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 466750 · Oct 31, 2024
- [739585](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148214395320260305193808.0001): Seal Option (Interchange-ability Control No). Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 739585 · Oct 31, 2024
- [761519](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139626019620260305201741.0001): Bushing Option (Interchangeability Control No.). Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 761519 · Oct 31, 2024
- [809808](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125934943520260305193807.0001): Blade – High Pressure Compressor,    8 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 809808 · Oct 31, 2024
- [629886](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112406865020260305193806.0001): Ring – Sealing, #3 Bearing. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 629886 · Oct 31, 2024
- [783852](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106240135920260305193807.0001): Vane – Turbine Stator, 2 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 783852 · Oct 31, 2024
- [761518](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187972602620260305165918.0001): Boss Option(InterchangeabilityControl No.). Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 761518 · Oct 28, 2024
- [803915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181955192720260305211430.0001): Counterweight–Compressor. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 803915 · Oct 28, 2024
- [506503CL2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181748401820260318212721.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL2 · Oct 28, 2024
- [506503CL6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181091118320260318212723.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL6 · Oct 28, 2024
- [822404](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180536206620260305211431.0001): Blade – TurbineRotor, 4 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 822404 · Oct 28, 2024
- [735330](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180290137320260318212719.0001): Fairing – Fuel Nozzle Support. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 735330 · Oct 28, 2024
- [474948P3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180277325820260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P3 · Oct 28, 2024
- [474948P12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176258339120260318212721.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P12 · Oct 28, 2024
- [761812](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173772421120260318212719.0001): Case – Turbine Exhaust Assembly of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 761812 · Oct 28, 2024
- [506503CL5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170888580720260318212723.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL5 · Oct 28, 2024
- [628777](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166995481720260318212719.0001): Spacer – Plate Combustion Chamber Duct Support. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 628777 · Oct 28, 2024
- [791047](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165505708420260305170150.0001): Duct Seg FanDifsr Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 791047 · Oct 28, 2024
- [506503CL1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164114275620260318212721.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL1 · Oct 28, 2024
- [474949](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157358752120260305211424.0001): Stud – Plain, .190-24-32 x 1.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474949 · Oct 28, 2024
- [756505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155445952020260318212718.0001): Blade – Compressor Rotor 5 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 756505 · Oct 28, 2024
- [776616](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150494846020260305211430.0001): Fairing – RearCompressor FanDuct, Assy Of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 776616 · Oct 28, 2024
- [810503](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142395769320260305211431.0001): Blade – LowPressureCompressor, 3 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 810503 · Oct 28, 2024
- [664236](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141599681420260318212719.0001): Box & Cable – Thermocouple Assembly of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 664236 · Oct 28, 2024
- [768363](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136844616120260318212657.0001): Switch - Differential Pressure. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 768363 · Oct 28, 2024
- [525148](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136825413920260305211430.0001): Strut - FanExhaust. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 525148 · Oct 28, 2024
- [328419](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135955459520260305211424.0001): Seal .424 ID x .103 DIA - Round. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 328419 · Oct 28, 2024
- [506503CL3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135562819320260318212722.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL3 · Oct 28, 2024
- [474948](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135310988920260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948 · Oct 28, 2024
- [806748](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131570016020260313172447.0001): Case CC, Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 806748 · Oct 28, 2024
- [474948P9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131069181420260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P9 · Oct 28, 2024
- [505509](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124953493420260305211430.0001): Shield - Heat,NR4 Bearing,Assy Of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 505509 · Oct 28, 2024
- [506503CL4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123460851220260318212722.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL4 · Oct 28, 2024
- [616313](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121922278920260318212724.0001): Duct – Fan Combustion Chamber & Turbine Assy Of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 616313 · Oct 28, 2024
- [474948P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121155195220260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P6 · Oct 28, 2024
- [845601](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID111999284020260305211431.0001): Blade – LowPressureCompressor, 1Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 845601 · Oct 28, 2024
- [AA134S-1KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184879292020230503123547.0001): Igniter Plug. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces AA134S-1 · Apr 27, 2023
- [RD1010](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119262724320230824100842.0001): Ring, Cut. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 709237 · Apr 18, 2023
- [1058V0400-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192781976020231218190434.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 804848 Original 6/19/89 · Apr 7, 2023
- [1058V0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179125890820240306163131.0001): Start Bleed Control Valve. Goodrich Corporation · PMA PQ1352NM · Replaces 793304 Rev. B (10-18-82) · Apr 7, 2023
- [1058V0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177996651520231218190434.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 793304 Rev. B (10-18-82) · Apr 7, 2023
- [1058V0400-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116398550720240306163132.0001): Start Bleed Control Valve. Goodrich Corporation · PMA PQ1352NM · Replaces 804848 Original 6/19/89 · Apr 7, 2023
- [1058V0400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198502891520230914183258.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 802211 Rev. ORIGINAL (6-21-85) · Mar 29, 2023
- [1058V0400-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125479340120230914183259.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 806146 Rev. Original (7-1-88) · Mar 29, 2023
- [1058V0600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115763985220230914183300.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 814099 Rev. Original (4-29-93) · Mar 29, 2023
- [819771WD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127249453620260805175346.0001): Bearing, Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces 819771 · Jul 21, 2022

All of them: https://openairdocs.org/engine/pratt-whitney-jt8d-15a/pma.md

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