# Pratt & Whitney JT8D-217C

- Type: Engine model (FAA registry)
- Registry code: 51693
- Manufacturer (registry): P & W
- Model: JT8D-217C
- Engine type: Turbo-fan
- Power: 20,000 lb thrust
- Data sheet: [TCDS E9NE](https://openairdocs.org/tcds/E9NE) (OpenAirDocs)
- Holder: Pratt & Whitney
- Installed in: 2 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-jt8d-217c

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 2015-14-05](https://openairdocs.org/ad/2015-14-05): Cracking in the low-pressure turbine (LPT) shaft · Pratt & Whitney Division JT8D-217C and JT8D-219. Effective Aug 25, 2015
- [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 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 (2)

- [N918AV](https://openairdocs.org/aircraft/N918AV): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1982, S/N 49104
- [N987GC](https://openairdocs.org/aircraft/N987GC): [Genesis Custom Jetliners LLC](https://openairdocs.org/faa-owner/GENESIS%20CUSTOM%20JETLINERS%20LLC), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), built 1991, S/N 53040

## 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 (252, newest 50)

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

- [SDR VGCA20260917001](https://openairdocs.org/sdr/VGCA20260917001), Sep 17, 2026: ENGINE. MAKING METAL. ENGINE OIL BYPASS INDICATION. METAL IN OIL FILTER
- [SDR 2017FA0000453](https://openairdocs.org/sdr/2017FA0000453), Sep 26, 2016: ENGINE. DETACHED. DURING THE LANDING ROLL, THE NR 3 ENGINE SEPARATED COMPLETELY FROM THE FUSELAGE, AFTER THRUST REVERSE APPLICATION AND DEPLOYMENT. THE ENGINE FELL TO THE RUNWAY.
- [SDR AALA20160530005](https://openairdocs.org/sdr/AALA20160530005), May 30, 2016: REGULATOR. FAULTY. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. R & R THE RT PNEUMATIC PILOT PRESS REGULATOR VLV, BROKEN SENSE LINE
- [SDR AALA20160603010](https://openairdocs.org/sdr/AALA20160603010), May 30, 2016: LINE. BROKEN. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILO
- [SDR AALA20160603011](https://openairdocs.org/sdr/AALA20160603011), May 30, 2016: LINE. CHAFED. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILO
- [SDR AALA20160603012](https://openairdocs.org/sdr/AALA20160603012), May 30, 2016: FITTING. STRIPPED. DURING CLIMB THE TAIL COMPARTMENT TEMPERATURE HIGH LIGHT ILLUMINATED. AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED, LANDING UNEVENTFUL. R & R THE RT PNEUMATIC PILO
- [SDR AALA20160525007](https://openairdocs.org/sdr/AALA20160525007), May 25, 2016: INDICATOR. FAULTY. DURING TAKEOFF ROLL THE LT ENG EPR STAGNATED AT 1.64 - 1.68, LAGGING BEHIND THE RT ENG. TAKEOFF ABORTED AT APPROX 70 KNOTS. REMOVED AND REPLACED ENGINE PRESSURE
- [SDR AALA20160417001](https://openairdocs.org/sdr/AALA20160417001), Apr 16, 2016: ENGINE. OUT OF TRIM. AIRCRAFT WAS GNDED. DURING TAKEOFF ROLL NR 2 ENG WOULD NOT MAKE TAKEOFF POWER. TAKEOFF ABORTED AT APPROX 40 KNOTS. ACCOMPLISHED MCM 71-91-08 & FOUND NR 2 ENG ID
- [SDR AALA20160329007](https://openairdocs.org/sdr/AALA20160329007), Mar 23, 2016: FITTING. LEAKING. AT GATE AFTER PAXS DEPLANED, CREW NOTED A BLUE HAZE IN CABIN, ACCOMPANIED BY AN OIL ODOR. ACCOMPLISHED MCM CARD 21-96-01 & NR 2 ENG IGV CASE LEAKING OIL OUT OF 
- [SDR AALA20150805009](https://openairdocs.org/sdr/AALA20150805009), Aug 3, 2015: SENSOR. FAULTY. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TUR
- [SDR AALA20150805010](https://openairdocs.org/sdr/AALA20150805010), Aug 3, 2015: SENSOR. FAULTY. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB, THE TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED. R & R TUBE ASSEMBLY FROM TUR
- [SDR 2CCA2015060100066](https://openairdocs.org/sdr/2CCA2015060100066), May 29, 2015: PISTON. OUT OF ADJUST. DURING POST MAINTENANCE VISIT ACCEPTANCE FLIGHT, DURING FLIGHT CONTROL CHECK IN EXCESS OF 250 KTS, FOUND LT RUDDER HAD NO EFFECT WHEN DEPRESSED FULLY - EITHER W
- [SDR AALA20150511008](https://openairdocs.org/sdr/AALA20150511008), May 11, 2015: ACCUMULATOR. FAULTY. EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING DESCENT, RT THRUST REVERSER ACCUMULATOR LOW PRESS LIGHT ILLUMINATED. RAN QRH, LIGHT REMAINE
- [SDR WX0A2015032672479](https://openairdocs.org/sdr/WX0A2015032672479), Mar 20, 2015: HYDRAULIC LINE. CRACKED. DURING DESCENT, NOTICED LT HYD PRESS READ 6 AT LAS QTY. AT LAS IT READ 12, PERFORMED QRH, HYD LEAK SUSPECTED. AFTER LANDING FLUID PRESS & QTY BOTH WENT TO ZERO.
- [SDR AALA20150226019](https://openairdocs.org/sdr/AALA20150226019), Feb 26, 2015: FUEL FILTER. FAULTY. DURING TAKEOFF NR 1 ENG FUEL FILTER INLET PRESS LOW LIGHT ILLUMINATED. TAKEOFF ABORTED AT 40 KNOTS. R & R NR 1 ENG FUEL FILTER. PERFORMED LEAK CHECK IAW AMM 73-
- [SDR AALA20150226030](https://openairdocs.org/sdr/AALA20150226030), Feb 26, 2015: COMPRESSOR. STALLED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS NOT OVERWEIGHT. RT ENG COMPRESSOR STALL & SHUT DOWN AT 3000 FEET & ACFT RETURNED. R & R RT ENG. FOUN
- [SDR AALA20150224020](https://openairdocs.org/sdr/AALA20150224020), Feb 24, 2015: INDICATOR. FAULTY. DURING TAKEOFF NR 1 ENG EPR STUCK AT 1.4. TAKEOFF WAS ABORTED AT UNDER 50 KNOTS. ALL OTHER INDICATIONS UNRESPONSIVE. R & R NR 1 ENG EPR INDICATOR IAW AMM 77-11-
- [SDR AALA20150204012](https://openairdocs.org/sdr/AALA20150204012), Feb 4, 2015: ENGINE. MALFUNCTIONED. DURING CLIMB RT ENG OIL PRESSURE INCREASED TO 60 PSI, OIL QTY DROPPED TO ZERO & ENG SHUTDOWN. RETURNED & EMERGENCY DECLARED. LANDING UNEVENTFUL. R & R RT ENG PO
- [SDR AALA20150116015](https://openairdocs.org/sdr/AALA20150116015), Jan 16, 2015: NOSE BULLET. DETACHED. AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING TAKEOFF THE NR 1 ENG EXPERIENCED COMPRESSOR STALLS. UPON INSPECTION FO
- [SDR AALA20141219002](https://openairdocs.org/sdr/AALA20141219002), Dec 18, 2014: SWITCH. DIRTY. EMERGENCY DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CRUISE LT ENG REVERSE UNLOCK LIGHT ILLUMINATED. ACCOMPLISHED QRH PROCEDURE & LIGHT REMAINED
- [SDR AALA20141213004](https://openairdocs.org/sdr/AALA20141213004), Dec 13, 2014: PRESSURE SWITCH. DEFECTIVE. AIR INTERRUPT, DIVERTED & EMER DECLARED & LANDING UNEVENTFUL. ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG OIL FILTER BYPASS LIGHT ILLUMINATED. R & R LT ENG OIL F
- [SDR AALA20141207010](https://openairdocs.org/sdr/AALA20141207010), Dec 7, 2014: ENGINE. FAILED. AIR INTERRUPT, RETURNED & EMERGENCY DECLARED. LANDING UNEVENTFUL. DURING CLIMBING THRU 25000 HEARD A VIOLENT BANG & ACFT SHOOK, NR 1 ENGINE FAILED. DURING INSPE
- [SDR AALA20141124006](https://openairdocs.org/sdr/AALA20141124006), Nov 24, 2014: OIL FILTER. CLOGGED. EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH RT ENG OIL STRAINER CLOG LIGHT ILLUMINATED. REDUCED POWER IAW QRH & LANDED. R & R 
- [SDR AALA20140905007](https://openairdocs.org/sdr/AALA20140905007), Sep 5, 2014: ENGINE. MALFUNCTIONED. LEFT ENG LOW OIL PRESS LIGHT ILLUMINATED & LOW OIL PRESS GAUGE AT ZERO. LT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED, LANDED W
- [SDR I5PA201406010001](https://openairdocs.org/sdr/I5PA201406010001), Jun 25, 2014: ENGINE. LEAKING. NR 3 ENGINE SHUTDOWN IN FLIGHT DUE TO POSSIBLE COMPRESSOR STALL FOLLOWED BY OIL LOSS. THE INLET & EXHAUST LOOKED OK, BUT EVIDENCE OF OIL LOSS FROM THE EXHAUST. 
- [SDR I5PA201406010002](https://openairdocs.org/sdr/I5PA201406010002), Jun 25, 2014: ENGINE. LEAKING. NUMBER 3 ENG SHUT DOWN IN FLIGHT DUE TO POSSIBLE COMPRESSOR STALL, FOLLOWED BY OIL LOSS. THE INLET & EXHAUST LOOKED OK, BUT EVIDENCE OF OIL LOSS FROM THE EXHAUS
- [SDR AALA20140614006](https://openairdocs.org/sdr/AALA20140614006), Jun 14, 2014: FILTER. CLOGGED. LEFT ENG OIL BYPASS LIGHT ILLUMINATED. EMER DECLARED FLIGHT DIVERTED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND CARBON IN FILTER, REPLACED ENG 
- [SDR AALA20140203004](https://openairdocs.org/sdr/AALA20140203004), Feb 3, 2014: ENGINE. FAILED. DFW CREW REPORTED HEARING TWO LOUD BANGS FOLLOWED BY THE RT HAND ENG FAILURE SINGLE ENG TIME 7 TO 8 MINUTES. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHO
- [SDR AALA20140203006](https://openairdocs.org/sdr/AALA20140203006), Feb 3, 2014: VALVE. INOPERATIVE. RDU INFLIGHT EWR-DFW. THE RT HAND ENG FUEL HEAT TEMPERATURE INDICATION. EMERGENCY DECLARED FLIGHT DIVERTED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SE
- [SDR AALA20121004008](https://openairdocs.org/sdr/AALA20121004008), Oct 4, 2012: ENGINE. FAILED. LIT - INFLIGHT DFW-IND. CREW REPORTED RIGHT ENGINE LOW OIL PRESSURE, ZERO OIL QUANTITY AND OIL TEMP AT 170 DEGREES. CAPTAIN PERFORMED INFLIGHT SHUTDOWN OF RIGHT
- [SDR AALA20120518006](https://openairdocs.org/sdr/AALA20120518006), May 18, 2012: FUEL CONTROL. DEFECTIVE. DFW - CREW REPORTED LEFT ENGINE PARAMETERS FLUCTUATING. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED 
- [SDR WX0A071207](https://openairdocs.org/sdr/WX0A071207), May 18, 2012: ENGINE. MALFUNCTIONED. FLIGHT CREW PERSONNEL REPORTED THAT DURING CLIMBOUT AT APPROX FL270, LEFT ENGINE COMPRESSOR STALL/ ENGINE PARAMETERS ROLLED BACK ENGINE SHUTDOWN PER CHECKLIST. 
- [SDR AALA20120208TUL01](https://openairdocs.org/sdr/AALA20120208TUL01), Feb 7, 2012: BULLET. LOOSE. OMA - CREW REPORTED RIGHT ENGINE COMPRESSOR STALL. RIGHT ENGINE REDUCED TO IDLE. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INS
- [SDR AALA20120103DFW01](https://openairdocs.org/sdr/AALA20120103DFW01), Jan 3, 2012: PROBE. LEAKING. DFW - CREW REPORTED RIGHT THROTTLE 3 KNOBS FORWARD OF LEFT WITH EPR MATCHED. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FR
- [SDR AALA20110918DFW01](https://openairdocs.org/sdr/AALA20110918DFW01), Sep 18, 2011: FLEX LINE. LEAKING. DFW - CREW REPORTED LEFT ENGINE NO RESPONSE, 2 KNOB THROTTLE SPLIT, EGT IN AMBER AND N1 & N2 FLUCTUATIONS. FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT
- [SDR FDEA201107182780](https://openairdocs.org/sdr/FDEA201107182780), Jul 18, 2011: LINE. LOOSE. REJECTED TAKEOFF DUE TO LOW N1. ENGINE RUN AFTER RTO. FOUND LINE AT MOISTURE TRAP HOLDING ON BY 1 THREAD. INSPECTED INLET ON NR 1 ENGINE AND FOUND PT2 INLET COM
- [SDR AALA20110623DFW02](https://openairdocs.org/sdr/AALA20110623DFW02), Jun 23, 2011: VALVE. INOPERATIVE. DFW - CREW REPORTED LEFT FUEL HEAT INDICATION DURING CLIMBOUT. HAD TO PUSH LEFT ENGINE THROTTLE UP TO KEEP OIL TEMP LESS THAN 135 DEGREES AND FUEL HEAT WOULD NO
- [SDR AALA20110528DFW01](https://openairdocs.org/sdr/AALA20110528DFW01), May 28, 2011: PUMP. FAILED. DFW - CREW REPORTED ON APPROACH AIRCRAFT YAWED TO THE RIGHT, BOTH PACKS SHUTDOWN AND THE RIGHT ENGINE APPEARED TO QUIT PRODUCING THRUST FOR A VERY SHORT PERIOD 
- [SDR AALA20110422PHX01](https://openairdocs.org/sdr/AALA20110422PHX01), Apr 21, 2011: SPRING. BROKEN. CREW REPORTED LEFT ENGINE LOST THRUST POWER. EMERGENCY DECLARED FLIGHT RETURNED PHX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND LEFT FUEL SHUT
- [SDR AALA20101027TUL01](https://openairdocs.org/sdr/AALA20101027TUL01), Oct 26, 2010: SLAT. DAMAGED. MFE - CREW REPORTED BIRD STRIKE TO LEFT WING ROOT, ENGINE VIBRATION EGT SEEMED NORMAL. REDUCED VIBRATION WITH REDUCED THRUST. EMERGENCY DECLARED RETURNED MFE LA
- [SDR FDEA201009183537](https://openairdocs.org/sdr/FDEA201009183537), Sep 18, 2010: HANDLE. UNSECURE. ON CLIMB OUT OF DAY FELT A SLIGHT ACFT VIBRATION (LIKE A SPOILER) RECYCLED NOT HELP- CONTINUUTE TO CLIMB AT ABOUT 12,500 HEARD AND FELT SEVERAL LOUD BANGS-LAST 
- [SDR FDEA201009013243](https://openairdocs.org/sdr/FDEA201009013243), Sep 1, 2010: FAN. FAILED. ON TAKEOFF FROM DSM, THE LT PACK TRIPPED AND THE LT DUCT OVERHEAT LIGHT ILLUMINATED. THIS WAS ACCOMPAINED BY THE USUAL ODOR OF A PACK OVERHEATING AND SMOKE IN T
- [SDR AALA20100816LAX01](https://openairdocs.org/sdr/AALA20100816LAX01), Aug 16, 2010: CLAMP. LOOSE. DURING FLIGHT CHECK RIGHT ENGINE LOW POWER ON CLIMB. FOUND PT2 FLEX LINE LEAKING MULTIPLE LOCATIONS UNDER PRESSURE. FOUND THE PNEUMATIC DUCT CLAMPS LOOSE IN THE
- [SDR AALA20100815LAX01](https://openairdocs.org/sdr/AALA20100815LAX01), Aug 14, 2010: SENSE LINE. LEAKING. LAX - CREW REPORTED RIGHT ENGINE THRUST DECREASED WITH ALTITUDE INCREASE. EMERGENCY DECLARED, RETURNED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVIC
- [SDR AALA20100811LAS01](https://openairdocs.org/sdr/AALA20100811LAS01), Aug 11, 2010: ENGINE. MAKING METAL. LAS - INFLIGHT LAX-DFW. ON CLIMBOUT CREW REPORTED LOUD BANG FOLLOWED BY RIGHT ENGINE OIL FILTER CLOG LIGHT ACCOMPANIED WITH GRINDING NOISE. EMERGENCY DECLARED, 
- [SDR AALA20100721PHL01](https://openairdocs.org/sdr/AALA20100721PHL01), Jul 21, 2010: FILTER. CLOGGED. PHL - ON DESCENT RIGHT ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED, IDLE POWER WAS NECESSARY TO KEEP LIGHT OUT. EMERGENCY DECLARED, LANDED PHL WITHOUT INCIDEN
- [SDR AALA20100605DFW01](https://openairdocs.org/sdr/AALA20100605DFW01), Jun 5, 2010: DUCT. BLOWN. DFW - CREW REPORTED NUMBER 2 ENGINE FIRE LOOP HAD A FIRE INDICATION FOLLOWED BY WARNING BELL. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT 
- [SDR AALA20100520MIA06](https://openairdocs.org/sdr/AALA20100520MIA06), May 20, 2010: ENGINE. MALFUNCTIONED. MIA - CREW REPORTED RIGHT ENGINE OVERTEMP INDICATION THEN LOUD BANG AND ENGINE RETURNED TO IDLE. EMERGENCY DECLARED RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRA
- [SDR AALA20100318DFW02](https://openairdocs.org/sdr/AALA20100318DFW02), Mar 18, 2010: VALVE. STICKING. DFW - CREW REPORTED DURING CLIMB OUT THE RIGHT FUEL HEAT LIGHT ILLUMINATED WITH CORRESPONDING RISE IN OIL TEMPERATURE. ACCOMPLISHED QRH PROCEDURES AND LIGHT REM
- [SDR AALA20091129DFW03](https://openairdocs.org/sdr/AALA20091129DFW03), Nov 29, 2009: ENGINE. LEAKING. ON CLIMB-OUT, RIGHT ENGINE POWER DECREASED TO APPROX 50 PERCENT. UNABLE TO REGAIN ANY POWER. SEVERAL MINUTES LATER, ENGINE WOULD NOT RESPOND TO THROTTLE MOVEMEN

All 252: https://openairdocs.org/engine/pratt-whitney-jt8d-217c/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 SE02128AT](https://openairdocs.org/stc/SE02128AT): Installation of a replacement ring manufactured by Praxair as part of the Praxair Second Stage Turbine inner air seal ring assembly. PAS Technologies Inc
- [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 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

## 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.

- [E800005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186250455020260305201703.0001): Bushing – Sleeve, .562 x .7523 x .290. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 800005 · Oct 28, 2024
- [570566](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148867501520260305211425.0001): Bushing – Diffuser Case, Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 570566 · Oct 28, 2024
- [E823652](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102138852020260305201703.0001): Vane Cluster – Low Pressure Turbine, 2 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 823652 · Oct 28, 2024
- [823078-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101644115520260305170151.0001): Housing Assy – Gearbox, Rear. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 823078-01 · Oct 28, 2024
- [VL1268PW95](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137365938620240320173441.0001): Washer. Proponent Inc. · PMA PQ1383NM · Replaces 761768 · Mar 11, 2024
- [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
- [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
- [1058V0700](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108551373220230914183257.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 803533 Rev. Original (2/25/87) · 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
- [214635JP-1](https://drs.faa.gov/browse/excelExternalWindow/9EA1CA66E80613DF86258656006E94AD.0001): Bearing. Jet Parts Engineering, LLC. (JPE) · PMA PQ2060NM · Replaces 214635-1 · Nov 26, 2020
- [214636JP-1](https://drs.faa.gov/browse/excelExternalWindow/4B8B89479566606F86258656006E94FF.0001): Bearing. Jet Parts Engineering, LLC. (JPE) · PMA PQ2060NM · Replaces 214636-1 · Nov 26, 2020
- [214633JP-1](https://drs.faa.gov/browse/excelExternalWindow/2812D632F351186B86258656006E942E.0001): Bearing Set. Jet Parts Engineering, LLC. (JPE) · PMA PQ2060NM · Replaces 214633-1 · Nov 26, 2020
- [214637JP-1](https://drs.faa.gov/browse/excelExternalWindow/1A5BBF8E6D7CEC2586258656006E9562.0001): Bearing. Jet Parts Engineering, LLC. (JPE) · PMA PQ2060NM · Replaces 214637-1 · Nov 26, 2020
- [214634JP-1](https://drs.faa.gov/browse/excelExternalWindow/150B4AD6F8826AB386258656006E9473.0001): Bearing. Jet Parts Engineering, LLC. (JPE) · PMA PQ2060NM · Replaces 214634-1 · Nov 26, 2020
- [DEC01- 039-501](https://drs.faa.gov/browse/excelExternalWindow/5A5B9C31B2BCC0F586258629005AC1D4.0001): Lever - Pressure Ratio Bleed Control. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 393909 · Nov 16, 2020
- [758308P10WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID903782019520210611172529.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P10W · Oct 15, 2020
- [758308WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID883733558820210611172526.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308 · Oct 15, 2020
- [758308P15WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID853154829220210611172530.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P15W · Oct 15, 2020
- [739585WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID766647496220210611172340.0001): Seal Face # 4 ½ Bearing. Wencor LLC · PMA PQ1370NM · Replaces 728982 · Oct 15, 2020
- [758308P20WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID740415996320210611172532.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P20W · Oct 15, 2020
- [758308P5WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID692977346202106111725280.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P5W · Oct 15, 2020
- [740259WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID435910374620210611172341.0001): Rivet-Tubular. Wencor LLC · PMA PQ1370NM · Replaces 740259 · Oct 15, 2020
- [738615WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID408467792120210611172335.0001): Seal-Face #6 Bearing. Wencor LLC · PMA PQ1370NM · Replaces 716299 · Oct 15, 2020
- [760016WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID248028746020210611172546.0001): Bolt-Externally Relieved Body, DH. Wencor LLC · PMA PQ1370NM · Replaces 760016 · Oct 15, 2020
- [758308P25WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID202417483920210611172533.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P25W · Oct 15, 2020
- [RD3003](https://drs.faa.gov/browse/excelExternalWindow/ECBA00B8EECE3F71862585D600471174.0001): Spacer, Sleeve. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces Pratt & Whitney P/N 781982 · Jul 8, 2020
- [F50030-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195391980820240703183033.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 744238 · Apr 1, 2020
- [H22-5PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195032076420240703182915.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 395037 · Apr 1, 2020
- [K1000X4PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190779431820240703183043.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 753965 · Apr 1, 2020
- [F53816-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180597416120240703183054.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces ST1572-04 · Apr 1, 2020
- [K29109-4-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171669181720240703182950.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 638671 · Apr 1, 2020
- [F29964-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171652783720240703182948.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 637285 · Apr 1, 2020
- [K39085-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170214002920240703183011.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 650410 · Apr 1, 2020
- [K2000-4CW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168219310320240703183042.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 751942 · Apr 1, 2020
- [F29724-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165439618320240703182932.0001): Nut, plain, bbl. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 594405 · Apr 1, 2020
- [CN29116-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162022931620240703182945.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 627798 · Apr 1, 2020
- [H29220-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160362046020240703183000.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 639335 · Apr 1, 2020
- [MF49663-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158888513120240703183015.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 677828 · Apr 1, 2020
- [H29908-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147545014320240703182947.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 627799 · Apr 1, 2020
- [F29724-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147155505220240703183018.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 696690 · Apr 1, 2020
- [MK2000-3PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147150668320240703183028.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 715018 · Apr 1, 2020
- [K29109-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145462505320240703182954.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 638674 · Apr 1, 2020
- [MF39839-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143884569520240703183032.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 743080 · Apr 1, 2020
- [F5000-4CWPW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143552543320240703183039.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 751929 · Apr 1, 2020
- [H49513-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142433141520240703183102.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces ST2119-09 · Apr 1, 2020
- [K29843-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID140735931020240703183003.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 646391 · Apr 1, 2020

All of them: https://openairdocs.org/engine/pratt-whitney-jt8d-217c/pma.md

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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.