# Pratt & Whitney JT8D-217 - Type: Engine model (FAA registry) - Registry code: 51691 - Manufacturer (registry): P & W - Model: JT8D-217 - Engine type: Turbo-jet - Power: 20,000 lb thrust - Data sheet: [TCDS E9NE](https://openairdocs.org/tcds/E9NE) (OpenAirDocs) - Holder: Pratt & Whitney - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/pratt-whitney-jt8d-217 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 2021-22-19](https://openairdocs.org/ad/2021-22-19): Turbine Engine Compressor Section · Pratt & Whitney JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 2021 - [AD 2011-04-04](https://openairdocs.org/ad/2011-04-04): Critical life-limited parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 22, 2011 - [AD 97-17-04 R1](https://openairdocs.org/ad/97-17-04-R1): Front compressor front hub · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Apr 22, 2010 - [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 2005-21-01](https://openairdocs.org/ad/2005-21-01): High pressure turbine (HPT) shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 21, 2005 - [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 2004-26-04](https://openairdocs.org/ad/2004-26-04): HPT containment hardware · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 9, 2005 - [AD 2003-16-05](https://openairdocs.org/ad/2003-16-05): High pressure compressor (HPC) disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 12, 2003 - [AD 2002-21-17](https://openairdocs.org/ad/2002-21-17): Fan duct and fan exit guide vane · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 29, 2002 - [AD 2002-16-08](https://openairdocs.org/ad/2002-16-08): Combustion Chamber Outer Case (CCOC) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 20, 2002 - [AD 99-10-11](https://openairdocs.org/ad/99-10-11): Fan Blades and Shrouds · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jun 14, 1999 - [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 96-15-06](https://openairdocs.org/ad/96-15-06): First Stage Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 3, 1996 - [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 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 88-04-02](https://openairdocs.org/ad/88-04-02): Anti-rotation Pin Failures · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 4, 1988 - [AD 87-03-13](https://openairdocs.org/ad/87-03-13): Compressor Blade · Pratt & Whitney Division JT8D-209, JT8D-217 and JT8D-217A. Effective Feb 16, 1987 - [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 Historical (superseded or no longer in force): - [AD 2011-07-02](https://openairdocs.org/ad/2011-07-02) (historical): Turbine Blade · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 28, 2011 - [AD 2006-17-07](https://openairdocs.org/ad/2006-17-07) (historical): Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 18 more. Effective Oct 4, 2006 - [AD 2005-18-02](https://openairdocs.org/ad/2005-18-02) (historical): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 28, 2006 - [AD 2005-02-03](https://openairdocs.org/ad/2005-02-03) (historical): Turbine (LPT) Blades 3rd and 4th Stage · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 3, 2005 - [AD 2002-23-14](https://openairdocs.org/ad/2002-23-14) (historical): High Pressure Compressor (HPC) Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 31, 2002 - [AD 2002-13-09](https://openairdocs.org/ad/2002-13-09) (historical): Rotating engine parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 30, 2002 - [AD 2000-21-07](https://openairdocs.org/ad/2000-21-07) (historical): Critical Life-Limited Parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 23, 2001 - [AD 99-26-06](https://openairdocs.org/ad/99-26-06) (historical): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 22, 2000 - [AD 99-27-01](https://openairdocs.org/ad/99-27-01) (historical): Low Pressure Turbine Blades · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 2, 2000 - [AD 99-22-14](https://openairdocs.org/ad/99-22-14) (historical): High Pressure Turbine Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 1999 - [AD 99-12-04](https://openairdocs.org/ad/99-12-04) (historical): Critical Life Limited Part Inspection · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jul 8, 1999 - [AD 97-19-13](https://openairdocs.org/ad/97-19-13) (historical): High Pressure Turbine (HPT) Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Oct 24, 1997 - [AD 97-17-04](https://openairdocs.org/ad/97-17-04) (historical): Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Sep 30, 1997 ## Information bulletins (advisory) (2) - [SAIB NE-16-22](https://openairdocs.org/saib/NE-16-22): Turbine Engine Combustion Section JT8D Series Turbofan Engines. Issued Sep 2, 2016 - [SAIB NE-10-32](https://openairdocs.org/saib/NE-10-32): Turbine Engine Accessory Drive. Issued May 7, 2010 ## Registered aircraft None registered with this engine model now. ## NTSB investigations (1) 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 MIA88LA075](https://openairdocs.org/ntsb/MIA88LA075), Dec 26, 1987: Boeing 727-200 (N705AA), San Juan, PR, substantial damage ## FAA accident and incident reports (6) 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 20120229024959I](https://openairdocs.org/incident/20120229024959I), Feb 29, 2012: Boeing 727-200 (N705AA), GU, No damage. No information regarding this incident and closing this item this date. 10-24-2012. - [Incident 19891030063529I](https://openairdocs.org/incident/19891030063529I), Oct 30, 1989: Boeing 727200 (N705AA), Atlantic Ocean, FL. Experienced turbulence for a period of seconds. One crewmenber injured. - [Incident 19890607038309I](https://openairdocs.org/incident/19890607038309I), Jun 7, 1989: Boeing 727200 (N705AA), Dallas-Ft Worth, TX, Minor damage. While taxiing, right wing tip struck a bus parked on right side of taxiway. Minor damage. - [Accident 19871226074841A](https://openairdocs.org/incident/19871226074841A), Dec 26, 1987: Boeing 727200 (N705AA), San Juan, Puerto Rico, Substantial damage. Struck the wing of N893AA while trying to pass on a taxiway to position for takeoff. Both were Boeing 727S. - [Incident 19840523023969I](https://openairdocs.org/incident/19840523023969I), May 23, 1984: Boeing 727200 (N705AA), Detroit, MI. Right main gear left the taxiway during a turn. Gear stuck in the ground. No damage to aircraft. - [Incident 19811214086839I](https://openairdocs.org/incident/19811214086839I), Dec 14, 1981: Boeing 727200 (N705AA), Chicago, IL. Lost all electrical power on approach. Landed on standby power only. #1 generator had failed. Replaced gen panel. ## Service difficulty reports (279, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR I5PA20200106104](https://openairdocs.org/sdr/I5PA20200106104), Dec 21, 2019: ENGINE. DAMAGED. AFTER DEPARTURE OUT OF ROR, ON CLIMB OUT CREW EXPERIENCED A LOUD BANG FROM ENGINE #3, CREW KEPT ENGINE AT IDLE AND RETURNED AND LANDED SAFELY IN ROR. MAINTENANC - [SDR FXGA201812043001](https://openairdocs.org/sdr/FXGA201812043001), Nov 30, 2018: HANDLE. STUCK. GEAR HANDLE STUCK IN THE UP POSITION - [SDR WX0A2016042773140](https://openairdocs.org/sdr/WX0A2016042773140), Apr 24, 2016: SENSE LINE. CRACKED. LEFT ENG LOW OIL PRESS ANNUNCIATOR ON EOAP. LT ENG OIL PRESS WAS INDICATING 35 PSI WITH NO OIL QTY. 10 - 15 PSI INDICATED UNTIL ENG WAS SHUT DOWN. APPROX WINDMI - [SDR WX0A2016020373085](https://openairdocs.org/sdr/WX0A2016020373085), Jan 28, 2016: ENGINE. FAILED. ABORTED TAKEOFF, HEARD THUMPING NOISE & RT ENG EGT WAS FLASHING. HAPPENED AT 50 KTS. R & R RT ENG IAW TC 71-080-003. - [SDR I5PA2015102631901](https://openairdocs.org/sdr/I5PA2015102631901), Oct 25, 2015: ENGINE. LEAKING. NR 3 ENG EXPERIENCED OIL LOSS. OIL PRESSURE AT APPROX 10 PSI ON IDLE PRIOR TO SHUT DOWN. DUE TO WEATHER ACFT DIVERTED TO ALTERNATE, FLIGHT ARRIVED SAFELY. TROUB - [SDR AALA20151004003](https://openairdocs.org/sdr/AALA20151004003), Oct 4, 2015: SWITCH. FAULTY. RIGHT ENG OIL STRAINER CLOGGING LIGHT CAME ON DURING DEPARTURE. CREW RAN THE CHECKLIST, DECLARED AN EMER & RETURNED TO FIELD. DURING THE RETURN, THE RT ENG WAS - [SDR AALA20140817017](https://openairdocs.org/sdr/AALA20140817017), Aug 17, 2014: TIRE. SEPARATED. ON TAKEOFF THE LT MLG TIRE TREAD SEPARATED & DENTED THE LT INBD FLAP, SPLASH GUARD & WAS INGESTED INTO THE LT ENG. EMER DECLARED FLIGHT RETURNED & LANDED WITHOU - [SDR AALA20140807001](https://openairdocs.org/sdr/AALA20140807001), Aug 6, 2014: TIRE. FAILED. RIGHT HAND TIRE CAP DEPARTED ACFT ON DEPARTURE. EMER DECLARED FLIGHT LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND RT FLAP DENTED FROM TIRE CAP LOSS - [SDR AALA20140728008](https://openairdocs.org/sdr/AALA20140728008), Jul 28, 2014: ENGINE. MALFUNCTIONED. ELECTRICAL ODOR IN CABIN. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. FOUND OIL WETNESS IN THE EXHAUST AREA AFTER LANDING. ACFT REMOVED FROM SERVIC - [SDR AALA20140719004](https://openairdocs.org/sdr/AALA20140719004), Jul 19, 2014: ENGINE. FAILED. AIRCRAFT SHOOK & RT ENG LOST OIL PRESS. RT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED F - [SDR AALA20140117018](https://openairdocs.org/sdr/AALA20140117018), Jan 17, 2014: GOVERNOR. MALFUNCTIONED. DFW CREW REPORTED DURING CLIMB OUT RT ENG HAD UNCOMMANDED SHUTDOWN WITH NO WARNINGS PRIOR TO SHUT DOWN. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT IN - [SDR AALA20131224009](https://openairdocs.org/sdr/AALA20131224009), Dec 24, 2013: COMPRESSOR. STALLED. STL CREW REPORTED LT ENG COMPRESSOR STALLED & LOSS OF THRUST. PULLED THE THROTTLE TO IDLE & SHUT IT DOWN, SINGLE ENGINE TIME 17 MINUTES. EMERGENCY DECLARED FLIG - [SDR AALA20131220004](https://openairdocs.org/sdr/AALA20131220004), Dec 20, 2013: COMPRESSOR. STALLED. MSP CREW REPORTED ON CLIMB OUT THE LT ENG ENCOUNTERED MULTIPLE COMPRESSOR STALLS. EMERGENCY DECLARED FLIGHT RETURNED MSP LANDED WITHOUT INCIDENT. AIRCRAFT REMOV - [SDR WX0A071765](https://openairdocs.org/sdr/WX0A071765), Dec 2, 2013: COMPRESSOR. STALLED. ON TAXI OUT WE RECEIVED 5 COMPRESSOR STALLS. UNABLE TO DETERMINE WHICH ENG. CHECKED RIG & TRIM OF LT ENG IAW MD80-MM-71-00-00 CONFIG 1. DRAINED MOISTURE TRAP, C - [SDR AALA20131003015](https://openairdocs.org/sdr/AALA20131003015), Oct 3, 2013: COMPRESSOR. STALLED. BHM CREW REPORTED ON CLIMB OUT, RT HAND ENG ENCOUNTERED 2 SUCCESSIVE COMPRESSOR STALLS. EMERGENCY DECLARED FLIGHT RETURNED BHM LANDED WITHOUT INCIDENT. AIRCRAFT - [SDR AALA20130822008](https://openairdocs.org/sdr/AALA20130822008), Aug 22, 2013: ENGINE. BIRD INGESTION. DFW CREW REPORTED BIRD STRIKE TO NR 1 ENGINE. LT ENGINE WAS SHUTDOWN SINGLE ENGINE TIME 9 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDEN - [SDR AALA20130810016](https://openairdocs.org/sdr/AALA20130810016), Aug 10, 2013: ENGINE. BIRD INGESTION. DFW CREW REPORTED STRONG OIL ODOR IN THE CABIN FOLLOWED BY A STRONG VIBRATION IN THE TAIL DURING CLIMB OUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOU - [SDR AALA20130402016](https://openairdocs.org/sdr/AALA20130402016), Apr 2, 2013: ENGINE. FAILED. DFW - CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS DURING CLIMBOUT. SHUTDOWN LEFT ENGINE (SINGLE ENGINE TIME 22 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED DFW - [SDR FY4Y20121122197](https://openairdocs.org/sdr/FY4Y20121122197), Nov 19, 2012: WEB. CORRODED. DURING PERFORMED 7C CHECK, CORROSION WAS FOUND ON CENTER FUEL TANK AFT VERTICAL WEB AT STATION BS 865, LBL 38, 39,WL 165-168 (DIMENSIONS OF CORROSION AREA:2 .37 - [SDR AALA20120910001](https://openairdocs.org/sdr/AALA20120910001), Sep 9, 2012: ENGINE. FAILED. LBB - INFLIGHT DFW-SAN. CREW REPORTED RIGHT ENGINE OIL QUANTITY LOSS AND VIBRATIONS. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLAR - [SDR AALA20120824005](https://openairdocs.org/sdr/AALA20120824005), Aug 24, 2012: ENGINE. FAILED. BHM - INFLIGHT DFW-CLT CREW REPORTED LEFT ENGINE OIL PRESSURE LOW AND OIL QUANTITY WENT TO ZERO. CAPTAIN FOLLOWED QRH PROCEDURES AND SHUT DOWN LEFT ENGINE (SING - [SDR AALA20120801009](https://openairdocs.org/sdr/AALA20120801009), Aug 1, 2012: ENGINE. FAILED. DFW - CREW REPORTED RIGHT ENGINE FIRE. RIGHT ENGINE SEIZED AND UNCOMMANDED SHUTDOWN (SINGLE ENGINE TIME 12 MINS). EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED - [SDR AALA20120704012](https://openairdocs.org/sdr/AALA20120704012), Jul 4, 2012: BLADE. DAMAGED. DFW - CREW REPORTED BIRD STRIKE TO NUMBER ONE ENGINE DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERV - [SDR AALA20120526002](https://openairdocs.org/sdr/AALA20120526002), May 25, 2012: ENGINE. MALFUNCTIONED. TUL - INFLIGHT DFW-STL. CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED - [SDR AALA20120501014](https://openairdocs.org/sdr/AALA20120501014), May 1, 2012: ENGINE. FAILED. BNA - CREW REPORTED LEFT ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THERE WAS SOME TYPE OF VIBRATION FELT BY THE FLIGHT CREW AND FLIGHT ATTENDANT WHICH WENT AWAY - [SDR AALA20120330012](https://openairdocs.org/sdr/AALA20120330012), Mar 30, 2012: ENGINE. VIBRATION. LGA - CREW REPORTED ON ARRIVAL A LOUD VIBRATION OCCURED ON THE RIGHT ENGINE. ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 10 MINS). EMERGENCY DECLARED FLIGHT LANDED - [SDR AALA20120305006](https://openairdocs.org/sdr/AALA20120305006), Mar 5, 2012: ENGINE. FAILED. LIT - INFLIGHT DFW-MEM. CREW REPORTED LOSS OF RIGHT ENGINE OIL PRESSURE AND QUANTITY IN FLIGHT. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 15 MINUTES). EMERG - [SDR AALA20110924DFW02](https://openairdocs.org/sdr/AALA20110924DFW02), Sep 24, 2011: ENGINE. FAILED. DFW - CREW REPORTED DURING CLIMBOUT, LEFT ENGINE OIL PRESSURE INDICATION DROPPED TO ZERO WITH QUANTITY NORMAL. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 7 MINS) - [SDR AALA20110916LAX01](https://openairdocs.org/sdr/AALA20110916LAX01), Sep 16, 2011: ENGINE. MALFUNCTIONED. LAX INFLIGHT SAN-DFW. CREW REPORTED LEFT ENGINE LOST OIL QUANTITY AND OIL PRESSURE AFTER TAKEOFF. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 23 MINS). EMERGENCY - [SDR AALA20110718TUL06](https://openairdocs.org/sdr/AALA20110718TUL06), Jul 18, 2011: GEARBOX. FAILED. BNA - CREW REPORTED NUMBER 2 ENGINE OIL QUANTITY AND OIL PRESSURE LOSS. RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 10 MIN). EMERGENCY DECLARED FLIGHT RETURNED BN - [SDR AALA20110420TUL12](https://openairdocs.org/sdr/AALA20110420TUL12), Apr 20, 2011: COMPRESSOR. STALLED. CREW REPORTED LEFT ENGINE COMPRESSOR STALLED DURING CLIMBOUT. ENGINE RETURNED TO IDLE WITH HIGH EGT. LEFT ENGINE SHUT DOWN (SINGLE ENGINE TIME 15 MINUTES). EMER - [SDR AALA20101224DFW08](https://openairdocs.org/sdr/AALA20101224DFW08), Dec 24, 2010: ENGINE. FAILED. DFW - CREW REPORTED GENERATOR FAILED MESSAGE FOLLOWED BY A FIRE WARNING ON RIGHT ENGINE. PULLED FIRE HANDLE AND DISCHARGED BOTH FIRE BOTTLES. RIGHT ENGINE SHUTD - [SDR AALA20101128TUL03](https://openairdocs.org/sdr/AALA20101128TUL03), Nov 28, 2010: ENGINE. FAILED. SAT - CREW REPORTED, HEARD A BANG FROM RIGHT ENGINE AND EGT BEGAN TO RISE. ENGINE WAS SHUT DOWN (SINGLE ENGINE TIME APPROXIMATELY 14 MINUTES). EMERGENCY DECLARE - [SDR AALA20101107DFW16](https://openairdocs.org/sdr/AALA20101107DFW16), Nov 7, 2010: COMPRESSOR. STALLED. DFW - CREW REPORTED LEFT ENGINE COMPRESSOR STALLED (SINGLE ENGINE TIME 10 MINUTES). EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FR - [SDR AALA20101102TUL10](https://openairdocs.org/sdr/AALA20101102TUL10), Nov 2, 2010: TURBINE. FAILED. MEX - CREW REPORTED RIGHT ENGINE COMPRESSOR STALL ON DEPARTURE. RIGHT ENGINE SHUTDOWN IN FLIGHT (SINGLE ENGINE TIME 17 MINUTES). EMERGENCY DECLARED RETURNED MWX - [SDR AALA20101018TPA01](https://openairdocs.org/sdr/AALA20101018TPA01), Oct 18, 2010: ENGINE. MALFUNCTIONED. TPA - CREW REPORTED ON CLIMB OUT AT FL 250 LEFT ENGINE EMITTED LOUD BANG, RPM ROLLED BACK TO SUB-IDLE AND EGT BEGAN TO SLOW CLIMB. SHUTDOWN ENGINE AT THAT POINT - [SDR AALA20100910DFW01](https://openairdocs.org/sdr/AALA20100910DFW01), Sep 10, 2010: ENGINE. MALFUNCTIONED. DFW - DURING CLIMBOUT WITH ENGINE PRESSURE RATIO AT 1.8 LEFT ENGINE POWER FELL OFF AND TEMPERATURE SPIKED. WHILE PERFORMING QHR PROCEDURE POWER SUDDENLY CAME BA - [SDR DALA1017529862](https://openairdocs.org/sdr/DALA1017529862), Jul 25, 2010: VALVE. LEAKING. AFTER TAKEOFF CLIMBING THROUGH 12K THE NUMBER 1 ENGINE ROLLED BACK SMOOTHLY AND FLAMED OUT. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO DTW LANDING WI - [SDR AALA20100723TUL13](https://openairdocs.org/sdr/AALA20100723TUL13), Jul 23, 2010: ENGINE. MALFUNCTIONED. IAD - INFLIGHT BWI-DFW. CREW REPORTED RIGHT ENGINE UNCOMMANDED INFLIGHT SHUTDOWN. SINGLE ENGINE TIME 25 MINUTES. EMERGENCY DECLARED, DIVERTED IAD LANDED WITHOUT - [SDR AALA20100630TUL09](https://openairdocs.org/sdr/AALA20100630TUL09), Jun 30, 2010: ENGINE. FAULTY. BHM - CREW HEARD LOUD BANG FOLLOWED BY LEFT ENGINE SHUTTING ITSELF DOWN INFLIGHT. EMERGENCY DECLARED FLIGHT RETURNED BHM LANDED WITHOUT INCIDENT. AIRCRAFT REMOV - [SDR AALA20100525DFW03](https://openairdocs.org/sdr/AALA20100525DFW03), May 25, 2010: ENGINE. FAILED. DFW - LEFT ENGINE FAILED DURING CLIMBOUT AT ABOUT 23,000 FEET (SINGLE ENGINE TIME 13 MINUTES). SMOKE IN THE CABIN WAS ALSO REPORTED. EMERGENCY DECLARED RETURNED - [SDR AALA20100519DFW05](https://openairdocs.org/sdr/AALA20100519DFW05), May 19, 2010: TURBINE BLADES. DAMAGED. DFW - CREW REPORTED LOUD BANG, VIBRATION AND RISE IN ENGINE GAS TEMPERATURE. LEFT ENGINE FAILED. AFTER ENGINE SHUTDOWN CREW REPORTED BANK ANGLE AUDIBLE WARNING - [SDR AALA20100505EWR01](https://openairdocs.org/sdr/AALA20100505EWR01), May 5, 2010: ENGINE. SEIZED. EWR - INFLIGHT LGA-ORD. LEFT ENGINE FAILED ON TAKEOFF (SINGLE ENGINE TIME 5 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED EWR LANDED WITHOUT INCIDENT. AIRCRAFT R - [SDR AALA20100422MCO01](https://openairdocs.org/sdr/AALA20100422MCO01), Apr 22, 2010: ENGINE. SEIZED. MCO - CAPTAIN REPORTED LEFT ENGINE SEIZED ON CLIMB OUT AT 2,000 FT. N1 INDICATED ZERO. EMERGENCY DECLARED FLIGHT RETURNED MCO LANDED WITHOUT INCIDENT. AIRCRAFT - [SDR AALA20100328ORD01](https://openairdocs.org/sdr/AALA20100328ORD01), Mar 28, 2010: ENGINE. MAKING METAL. ORD - CREW REPORTED OIL STRAINER CLOG LIGHT, HIGH OIL TEMPERATURE, AND VIBRATIONS DURING FLIGHT. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 13 MINUTES). EMER - [SDR AALA20100328DFW01](https://openairdocs.org/sdr/AALA20100328DFW01), Mar 28, 2010: COMPRESSOR. STALLED. DFW - CREW REPORTED AFTER CLIMB THE RIGHT ENGINE COMPRESSOR STALLED. CREW SHUT DOWN ENGINE (SINGLE ENGINE TIME 15 MINUTES) EMERGENCY DECLARED FLIGHT RETURNED DF - [SDR AALA20100203SAN01](https://openairdocs.org/sdr/AALA20100203SAN01), Feb 3, 2010: COMPRESSOR. STALLED. SAN - CREW REPORTED RIGHT ENGINE COMPRESSOR STALLED TWICE DURING CLIMBOUT. EMERGENCY DECLARED RETURNED SAN LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVIC - [SDR AALA20091105MCO01](https://openairdocs.org/sdr/AALA20091105MCO01), Nov 5, 2009: CSD. OVERHEATED. CREW REPORTED LEFT CONSTANT SPEED DRIVE GENERATOR OVERHEAT. RIGHT GENERATOR ON MEL. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. REPLACED LEFT CONSTANT SPEED DR - [SDR AALA20091030MEX01](https://openairdocs.org/sdr/AALA20091030MEX01), Oct 29, 2009: BEARING. DAMAGED. ON FINAL APPROACH RIGHT ENGINE OIL QUANTITY FELL TO ZERO. OIL TEMP AT RED LINE, PRESSURE NORMAL. CREW SHUT NUMBER TWO ENGINE DOWN. LANDED WITHOUT INCIDENT. FOUN - [SDR I5PA20090801](https://openairdocs.org/sdr/I5PA20090801), Aug 6, 2009: SPAR. CORRODED. DURING 5C-CHECK AND INPS CORROSION WAS FOUND ON RT AND LT WING FRONT SPAR CHORD PLATE LWR SURFACE. AFTER BLEND OUT THE MAX LOSS OF MATERIAL THICKNESS WAS BEYOND All 279: https://openairdocs.org/engine/pratt-whitney-jt8d-217/reports.md ## STCs that may be installed (OpenAirDocs) (11) 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 SE482CH](https://openairdocs.org/stc/SE482CH): Installation of Tube Processing Corporation (TPC) JT8D-200 Anti-Ice tube assemblies Part Numbers 2026-TP, 2027-TP, 2028-TP and 2029-TP and support brackets Part Number 2060-TP, 2061-TP, 2062-TP and 2063-TP. United Technologies Corporation, Pratt & Whitney Division - [STC SE01944LA](https://openairdocs.org/stc/SE01944LA): Installation of a JET Engineering, Ltd. Turbine Exhaust Cone Mixer (TECM). Jet Engineering LTD - [STC SE00429AT](https://openairdocs.org/stc/SE00429AT): Incorporate an alternate gear box stud installation. Jet Avion Corporation - [STC SE2117SO](https://openairdocs.org/stc/SE2117SO): Installation of an oil tank safety cap adapter which prevents loss of oil in the event of loss or damage to the oil filler cap. Jet Avion Corporation - [STC SE01650SE](https://openairdocs.org/stc/SE01650SE): Installation of Aviation Fleet Solutions MD-80 heavy weight noise abatement system. Aviation FLeet Solutions LLC - [STC SE6025NM](https://openairdocs.org/stc/SE6025NM): Installation of P/N T98781 first stage turbine nozzle guide vanes. Kellstrom Defense Aerospace Inc - [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 - [STC SE1683GL](https://openairdocs.org/stc/SE1683GL): Installation of Rexnord O-Ring face seal P/N's 1-1337-701, 1-1633-701, 1-1738-701, and/or1-2233-701. 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 SE1930SO](https://openairdocs.org/stc/SE1930SO): Installation of power control shaft bushing. Cook Airtomic Division --- 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.