# Pratt & Whitney JT8D-217A

- Type: Engine model (FAA registry)
- Registry code: 51692
- Manufacturer (registry): P & W
- Model: JT8D-217A
- Engine type: Turbo-fan
- 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-217a

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 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

## 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 MIA03LA155](https://openairdocs.org/ntsb/MIA03LA155), Aug 4, 2003: McDonnell Douglas MD-82 (N7527A), Charlotte, NC, no damage. Probable cause: The pilot-in-command's failure to sufficiently deviate to avoid known weather, and his failure to activate the seatbelt sign to ensure flight attendants and passengers were seated, which resulted in…

## 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 20150218001159I](https://openairdocs.org/incident/20150218001159I), Feb 18, 2015: Mcdonnell Douglas DC-9-82(MD-82) (N803WA), Jamaica, NY, Minor damage. Aircraft N803WA was being deiced prior to departure from jfk, the left wing was struck by the deicing truck while the vehicle was backing up. It caused damage…
- [Accident 20030803027409A](https://openairdocs.org/incident/20030803027409A), Aug 3, 2003: Doug DC982 (N7527A), Charlotte, NC. (-23) On August 3, 2003, about 2207 hrs. Eastern time, a DC-9-82, N7527A, registered to wilmington trust co. and operated by American airlines inc., a 121…
- [Incident 19910915052189I](https://openairdocs.org/incident/19910915052189I), Sep 15, 1991: Doug DC982 (N7527A), Baltimore, MD. Smoke in cabin of unoccupied aircraft. Service clerk shut down APU. No fire. APU had internal failure.

## Service difficulty reports (235, newest 50)

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

- [SDR AALA20170321006](https://openairdocs.org/sdr/AALA20170321006), Mar 21, 2017: BOLT. WORN. FLIGHT DIVERTED DUE TO AN AIRFRAME VIBRATIONS BETWEEN THE AFT LAVATORIES. UNEVENTFUL LANDING. LEFT ENGINE ANTI-ICE VALVE MOUNTING BOLT WORN AND LOOSE. REMOVED A
- [SDR AALA20150612001](https://openairdocs.org/sdr/AALA20150612001), Jun 11, 2015: COMPRESSOR BLADE. DAMAGED. AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, CREW REPORTS A COMPRESSOR STALL ON RT ENG FOLLOWED BY A REDUCTI
- [SDR AALA20110331TUL07](https://openairdocs.org/sdr/AALA20110331TUL07), Mar 31, 2011: EXCITER. FAILED. MCO INFLIGHT TPA-ORD. CREW REPORTED LIGHTNING STRIKE TO RIGHT SIDE OF AIRCRAFT WITH RIGHT ENGINE SHUTDOWN (SINGLE ENGINE TIME 1 MINUTE). EMERGENCY DECLARED DIVE
- [SDR AALA20100418SFO01](https://openairdocs.org/sdr/AALA20100418SFO01), Apr 18, 2010: TUBE. LEAKING. SFO - CREW REPORTED RIGHT ENGINE OIL PRESSURE LIGHT DROPPED TO 20 PSI AND STABILIZED. RIGHT HAND THROTTLE REDUCED TO IDLE. FLIGHT RETURNED SFO LANDED WITHOUT IN
- [SDR ASMF200711003](https://openairdocs.org/sdr/ASMF200711003), Nov 12, 2007: BLADE. DAMAGED. DURING TRANSIT CHECK, FIVE BLADES WERE DETECTED DAMAGED DUE TO A FOD IN LT ENGINE. (4) BLADES WERE DETECTED WITH NICKS ON BLADES LEADING EDGE AND WERE REWORKED 
- [SDR ASMF200708007](https://openairdocs.org/sdr/ASMF200708007), Aug 25, 2007: CONTROL VALVE. LEAKING. DURING TRANSIT CHECK WAS DETECTED A HYDRAULIC LEAK IN THE LT ENGINE REVERSE CONTROL VALVE. THE VALVE WAS REPLACED IAW MM 78-31-04, TESTED CORRECT AND 6/4 OF HYD
- [SDR GTIA200700015](https://openairdocs.org/sdr/GTIA200700015), Feb 17, 2007: FLOORBEAM. CORRODED. CABIN FLOORBEAM CORRODED. REPLACED FLOOR SUPPORT BEAM.
- [SDR GTIA200700013](https://openairdocs.org/sdr/GTIA200700013), Feb 16, 2007: INTERCOSTAL. CRACKED. AFT CARGO CABIN FLOOR INTERCOSTAL CRACKED. REPLACED INTERCOSTAL.
- [SDR GTIA200700014](https://openairdocs.org/sdr/GTIA200700014), Feb 16, 2007: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM ANGLE. REPLACED FLOORBEAM.
- [SDR GTIA200700012](https://openairdocs.org/sdr/GTIA200700012), Feb 15, 2007: FLOORBEAM. CORRODED. CORROSION AFT CARGO CABIN FLOORBEAM. INSTALLED NEW FLOORBEAM.
- [SDR GTIA200700009](https://openairdocs.org/sdr/GTIA200700009), Feb 14, 2007: FLOOR SUPPORT. CORRODED. CORROSION ON FLOOR SUPPORT. REPAIRED FLOOR SUPPORT.
- [SDR GTIA200700010](https://openairdocs.org/sdr/GTIA200700010), Feb 14, 2007: FLOORBEAM. CORRODED. CORROSION AT FWD CABIN FLOOR SUPPORT. INSTALLED NEW FLOOR SUPPORT.
- [SDR GTIA200700011](https://openairdocs.org/sdr/GTIA200700011), Feb 14, 2007: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM. INSTALLED NEW FLOORBEAM.
- [SDR GTIA200700008](https://openairdocs.org/sdr/GTIA200700008), Feb 12, 2007: LONGERON. CORRODED. AFT CARGO COMPT LONGERON 29R HAS CORROSION. MADE LONGERON REPAIR.
- [SDR GTIA200700007](https://openairdocs.org/sdr/GTIA200700007), Feb 10, 2007: DOOR. OBSTRUCTED. UNABLE TO OPEN RT AFT OVERWING EXIT. FOUND TRIM PANEL OVERLAPPING UPPER AFT CORNER PREVENTING IT FROM OPENING.
- [SDR ASMF200612002](https://openairdocs.org/sdr/ASMF200612002), Dec 11, 2006: REGULATOR VALVE. FAILED. AIRCRAFT RETURNED DUE TO AIR CONDITIONING SYSTEMS FAILED, RT SYSTEM WAS SHUTDOWN, LT SYSTEM DID NOT OPERATE AND SMOKE ODOR WAS DETECTED. DURING MAINTENANCE CHEC
- [SDR ASMF200604013](https://openairdocs.org/sdr/ASMF200604013), Apr 25, 2006: FAN BLADE. DAMAGED. DURING TRANSIT CHECK, IT WAS DETECTED ONE LEFT ENGINE C1 FAN BLADE DAMAGED BY AN SCREW SANK INTO THE ACOUSTIC PANEL (FOD). THE DAMAGE WAS EVALUATED IAW M/M 72-0
- [SDR ASMF200603005](https://openairdocs.org/sdr/ASMF200603005), Mar 13, 2006: FILTER. DIRTY. CAPTAIN REPORTED THAT DURING TAXING LT ENGINE DID NOT ACCELERATE EVEN WITH THRUST LEVER FULLY FORWARDED, RETURNING TO PLATFORM. DURING CHECK, MAINTENANCE PERSON
- [SDR AALA20060143](https://openairdocs.org/sdr/AALA20060143), Mar 4, 2006: ENGINE. SHUTDOWN. DEN - RIGHT ENGINE FAILED AFTER TAKEOFF AT ABOUT 300 FEET ABOVE GROUND LEVEL. RIGHT HAND ENGINE EXHAUST GAS TEMPERATURE AT ROTATION WAS ABOUT 570 DEGREES. ENGIN
- [SDR 06FDEA0547](https://openairdocs.org/sdr/06FDEA0547), Feb 6, 2006: FUEL CONTROL. MALFUNCTIONED. NO THROTTLE RESPONSE ON NR 1 ENGINE ON TAKEOFF. REMOVED AND REPLACED NR 1 ENGINE FUEL CONTROL IAW FX B 727-200 MM 73-20-001-2. PERFORMED ENGINE RUN AND TRIM MED
- [SDR ASMF200602001](https://openairdocs.org/sdr/ASMF200602001), Feb 2, 2006: FAN BLADE. DAMAGED. DURING TRANSIT CHECK, DETECTED 09 LEFT ENGINE FAN BLADES WITH DAMAGES. ONE OF THEM WAS OUT OF LIMITS. 04 FAN BLADES WERE REPLACED IAW M/M 72-33-21 AND 06 WERE R
- [SDR ASMF200512019](https://openairdocs.org/sdr/ASMF200512019), Dec 25, 2005: ANNUNCIATOR. FAILED. AIRCRAFT RETURNED TO PLATFORM DURING TAXING THE SLAT DISAGREE LIGHT NOT TURNED ON. DURING MAINTENANCE REVISION, THE SLAT DISAGREE LIGHT WAS FAILING INTERMITTENT
- [SDR ASMF200501201](https://openairdocs.org/sdr/ASMF200501201), Dec 22, 2005: ENGINE. VIBRATION. CAPTAIN REPORTED THAT DURING FLIGHT WITH EPR BETWEEN 1.0 AND 1.2 IN THE LT ENGINE; VIBRATION AMPLITUDE OCCASIONALLY WITH PEAKS FROM 4 TO 0 AND WHEN THE LT ENGIN
- [SDR ASMF200512007](https://openairdocs.org/sdr/ASMF200512007), Dec 7, 2005: PIN. BROKEN. DURING PUSH BACK THE NOSE LANDING GEAR TOWING FUSE PIN WAS BROKEN. IT WAS REPLACED IAW MM 32-21-14 AND THE NOSE LANDING GEAR AND GENERAL INSPECTIONS FOR EXCESSI
- [SDR GTIA050264](https://openairdocs.org/sdr/GTIA050264), Oct 17, 2005: FRAME. CRACKED. FRAME CANT 1463 AT APPROX LONGERON 19 AND 20 ON AC RT HAS CRACKED WEBBING. INSTALLED PERMANENT REPAIR ON CANTED FRAME FS 1463 BETWEEN R18L AND R25L, IAW EA REV 
- [SDR ASMF200505030](https://openairdocs.org/sdr/ASMF200505030), May 30, 2005: SKIN. CRACKED. CAPTAIN REPORTED THAT HE PERFORMED THE FINAL APPROACH AND LANDING WITH 3450 POUNDS OUT OF BALANCE BETWEEN TANKS. OUT OF BALANCE INSPECTION WAS PERFORMED IAW MM,
- [SDR T48R20050011](https://openairdocs.org/sdr/T48R20050011), Apr 26, 2005: ENGINE. DAMAGED. ENGINE WAS REMOVED FROM N803NK FOR INFLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED THE HPC, HPT AND LPT MODULES HAVE HEAVY IMPACT DAMAGE.
- [SDR GTIA050099](https://openairdocs.org/sdr/GTIA050099), Apr 4, 2005: WEB. PUNCTURED. AT STA 200, NR 1 SEAT TRACK LT FLOOR WEB HAS A PUNCTURE. CUT OUT PUNCTURE FROM FLOOR WEB STA 200, NR 1 SEAT TRACK. FABRICATE DOUBLERS AND FILLERS. TREATED AND P
- [SDR GTIA050076](https://openairdocs.org/sdr/GTIA050076), Mar 26, 2005: WIRE. BROKEN. UPON PREFLIGHT (COCKPIT SETUP) COULD NOT GET RUDDER CONTROL MANUAL LIGHT DURING TEST, AIRCRAFT TAIL SWAP TO 817NK. TROUBLESHOT DOWN TO BROKEN WIRE AT CANT. STA 
- [SDR GTIA050097](https://openairdocs.org/sdr/GTIA050097), Mar 25, 2005: SUPPORT ANGLE. CRACKED. AFT CARGO DOOR FWD UPLOCK SUPPORT ANGLE CRACKED. REMOVED AND FABRICATED NEW ANGLE IAW SRM. TREATED AND PRIMED, INSTALLED SUPPORT ANGLE IAW SRM. (K)
- [SDR GTIA050084](https://openairdocs.org/sdr/GTIA050084), Mar 15, 2005: WEB. CORRODED. CABIN STA 180-200, RBL 54, RBL59, SUB FLOOR CORRODED. REMOVED CORROSION AT WEB. MATERIAL LOSS OUT OF LIMITS. REMOVED FWD AIRSTAIR. REMOVED FLOOR SUPPORT RT STA 
- [SDR GTIA050093](https://openairdocs.org/sdr/GTIA050093), Mar 11, 2005: STRAP. CORRODED. ALUMINUM STRAP ON LOWER SIDE OF L2 DOOR THRESHOLD HAS CORROSION. STRAP CORROSION IS OUT OF LIMITS. FABRICATED NEW STRAP IAW SRM. TREATED AND PRIMED, INSTALLED S
- [SDR GTIA050079](https://openairdocs.org/sdr/GTIA050079), Mar 11, 2005: DOUBLER. CORRODED. G-2 GALLEY, CART ENCLOSURE, AFT LOWER LIP AND (2 EA) DOUBLERS ARE CORRODED. REMOVED LOWER LIP AND DOUBLERS, FOUND LIP AND DOUBLERS OUT OF LIMITS. FABRICATED LIP
- [SDR GTIA050078](https://openairdocs.org/sdr/GTIA050078), Mar 11, 2005: SUPPORT ANGLE. CORRODED. G-2 GALLEY, UPPER SECTION, LOWER EDGE AND SUPPORT ANGLE ARE CORRODED. REMOVED CORROSION ON LOWER EDGE AND SUPPORT ANGLE. FOUND SUPPORT ANGLE OUT OF LIMITS FABRI
- [SDR GTIA050098](https://openairdocs.org/sdr/GTIA050098), Mar 10, 2005: DOUBLER. CRACKED. HORIZONTAL STABILIZER, RT SIDE IB UPPER BRACKET SUPPORT HAS CRACK ON DOUBLER. REMOVED CRACKED DOUBLER. FABRICATED NEW DOUBLER. TREATED AND PRIMED, INSTALLED DOU
- [SDR GTIA050096](https://openairdocs.org/sdr/GTIA050096), Mar 10, 2005: SKIN. DENTED. DENT ON AFT CARGO DOOR SKIN 21 INCHES FROM AFT EDGE AND 11 INCHES FROM BOTTOM EDGE OF DOOR (X=0.035 INCH, D=1.75 INCH, D/X=50). STRIPPED AREA OF DENT ON AFT CAR
- [SDR GTIA050095](https://openairdocs.org/sdr/GTIA050095), Mar 10, 2005: SKIN. DENTED. DENT ON FUSELAGE SKIN FS421 BETWEEN LONGERONS 19R AND 20R (D=0.5 INCH, X=0.008 INCH, D/X - 62.5 INCHES). REMOVED CARGO DOOR TO FOM IAW SRM. FOUND DENT HAS GOUGE
- [SDR GTIA050082](https://openairdocs.org/sdr/GTIA050082), Mar 10, 2005: CUSP WEB. CORRODED. MID PIT STA 522-636, A LONG 18, RBL 52, FLOOR PANEL UNDER FEDDER CABLES CORRODED. REMOVED CORROSION FROM 522-636, FOUND OUT OF LIMITS. REMOVED WEB STA 503-598, 
- [SDR GTIA050081](https://openairdocs.org/sdr/GTIA050081), Mar 10, 2005: SEAT TRACK. CRACKED. RT OB SEAT TRACK HAS AREA OF CORROSION AT FS 229. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK. FOUND WEB OB OF SEAT TRACK FS 218 CRACKED, 
- [SDR GTIA050094](https://openairdocs.org/sdr/GTIA050094), Mar 7, 2005: FRAME. CRACKED. FROM C/O 0155770 RT WING L/E 2 EA FORMERS ST APPROX STA 351 CRACKED. FABRICATED DOUBLER IAW SRM. HEAT TREATED 2 EA DOUBLER IAW SRM. TREATED AND PRIMED INSTALLED
- [SDR GTIA050083](https://openairdocs.org/sdr/GTIA050083), Mar 4, 2005: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT, STA 1174, LBL 12, MAIN CABIN FLOORBEAM UPPER FLOOR SUPPORT ANGLE IS CORRODED (EXFOLIATION). REMOVED DAMAGED FLOORBEAM AND FOUND OUT OF LI
- [SDR ASMF200503002](https://openairdocs.org/sdr/ASMF200503002), Mar 3, 2005: FUEL CONTROL. FAILED. AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF RIGHT ENGINE WITHOUT ACCELERATION AND PARAMETERS WERE BELOW NORMAL IN IDLE. THE ACCELERATION CHAMBER WAS SERVI
- [SDR GTIA050071](https://openairdocs.org/sdr/GTIA050071), Mar 3, 2005: SKIN. DENTED. SKIN DENT AT STA 1174, BETWEEN LONGERON 17L AND 18L. REMOVED SAF-T-GLO, GALLEY 4 AND SIDE WALL PANEL TO FOM AT LT FS 1184. FOUND DENT TO BE (D=1.5 INCH, X=0.050
- [SDR GTIA050055](https://openairdocs.org/sdr/GTIA050055), Feb 27, 2005: SKIN. DENTED. LT WING FLAP VANE NR 4 HAS DENT TOP SIDE. REMOVED DAMAGED SKIN AND CORE. FABRICATED NEW CORE AND DOUBLER, TREATED DOUBLER AND BONDED CORE IAW 57-50. (K)
- [SDR GTIA050061](https://openairdocs.org/sdr/GTIA050061), Feb 26, 2005: FLOOR SUPPORT. BROKEN. FLOOR SUPPORT STA 1136 BROKEN AFT PIT 28R-28L. REMOVED FLOOR SUPPORT AND LOCATED NEW FLOOR SUPPORT AT STA 1136, 28R-28L. INSTALLED FLOOR SUPPORT FS 1136, 28R-28
- [SDR GTIA050037](https://openairdocs.org/sdr/GTIA050037), Feb 23, 2005: MOTOR. INOPERATIVE. PRIMARY LONG TRIM INOPERATIVE, TAIL SWAP WITH AIRCRAFT 829. REMOVED AND REPLACED LONG TRIM MOTOR AND REPAIRED MOTOR GROUNDS, SYSTEM OPS CHECK GOOD. (K)
- [SDR GTIA050056](https://openairdocs.org/sdr/GTIA050056), Feb 20, 2005: SUPPORT ANGLE. CORRODED. THRESHOLD SUPPORT ANGLE, STA 1212, ON DOOR JAMB BEAM IS CORRODED. REMOVED CORROSION AT SUPPORT ANGLE. MATERIAL LOSS OUT OF LIMITS. REMOVED SUPPORT ANGLE AT STA 
- [SDR GTIA050064](https://openairdocs.org/sdr/GTIA050064), Feb 20, 2005: SKIN. DENTED. FUSELAGE SKIN DENTED AT FS 304 BETWEEN LONGERON 28L-29L. (D=0.5 INCH, X=0.015 INCH D/X= 33.3). DENT WAS FOUND TO BE LESS THAN 1.0 INCH FROM FRAME REQ A CUT OUT 
- [SDR GTIA050053](https://openairdocs.org/sdr/GTIA050053), Feb 19, 2005: SKIN. DENTED. DENT AT FS 245, LONGERON 18L (D=1.250 INCH, X=0.054 D/X=23.14). REMOVED AIRCRAFT SKIN AT STA FS 245, LONGERON 18L (20 INCHES X 14 INCHES). FABRICATED REPAIR PAR
- [SDR GTIA050052](https://openairdocs.org/sdr/GTIA050052), Feb 18, 2005: STIFFENER. CORRODED. AFT CARGO COMPARTMENT, STA 1338, 27L-27R AFT SIDE OF FALSE BULKHEAD, LOWER STIFFENERS ARE CORRODED. REMOVED CORROSION AT STIFFENER STA 1338L, 29L. MATERIAL LOSS

All 235: https://openairdocs.org/engine/pratt-whitney-jt8d-217a/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

## 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
- [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
- [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
- [819771WD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127249453620260805175346.0001): Bearing, Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces 819771 · Jul 21, 2022
- [ST2273JP-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176398738120230330123014.0001): Pin. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces ST2273-07 · Jul 6, 2021
- [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
- [741313WA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID559712470220210611172347.0001): Rivet-Tubular. Wencor LLC · PMA PQ1370NM · Replaces 741313 · 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
- [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
- [H29220-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167914324120240703182958.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 639299 · Apr 1, 2020
- [K50772-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165710741720240703183047.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 770229 · 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
- [H29118-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139990913620240703182936.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 618097 · Apr 1, 2020
- [H29117-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127118184120240703182952.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 638672 · Apr 1, 2020
- [F2000-4PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125358427520240703183022.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 710826 · Apr 1, 2020

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

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