# Pratt & Whitney JT8D-17A

- Type: Engine model (FAA registry)
- Registry code: 51733
- Manufacturer (registry): P & W
- Model: JT8D-17A
- Engine type: Turbo-fan
- Power: 16,000 lb thrust
- Data sheet: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs)
- Holder: Pratt & Whitney
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/pratt-whitney-jt8d-17a

Model codes come from the FAA registry's reference file.

## ADs that may apply (OpenAirDocs)

Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

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

## Registered aircraft (1)

- [N73HK](https://openairdocs.org/aircraft/N73HK): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1979, S/N 21957

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports (2)

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 20111014024599I](https://openairdocs.org/incident/20111014024599I), Oct 14, 2011: Boeing 727-2S2F (N217FE), Des Moines, IA, No damage. On short final, the the crew reported an intermittent indication of smoke in the cargo bay. The intermittent indication then changed to the light and alarm,…
- [Incident 19911224061229I](https://openairdocs.org/incident/19911224061229I), Dec 24, 1991: Boeing 7272S2F (N217FE), Houston, TX. NR2 engine oil filter bypass light came on during takeoff. Returned. Found oil pressure switch bad.

## Service difficulty reports (362, newest 50)

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

- [SDR MJYA20250613003](https://openairdocs.org/sdr/MJYA20250613003), Jun 13, 2025: ENGINE. DAMAGED. 112000 LBS TAKEOFF, FLAPS 1, V1=144 VR=147 V2=153, RIGHT SEAT TAKEOFF. AFTER NORMAL START AND TAXI OUT FROM WILSON AIR CENTER TO RUNWAY 18L WE PROCEEDED TO TAKE
- [SDR CA190221011](https://openairdocs.org/sdr/CA190221011), Feb 21, 2019: TUBE. CHAFED. (CAN) ENGINE OIL CONSUMPTION ABNORMAL (CONSUMPTION INCREASING). CAUSE: #6 BEARING PRESSURE TUBE P/N 761392 CHAFFED. RECTIFICATION: #6 BEARING TUBE P/N 761392 RE
- [SDR MJYA201812076003](https://openairdocs.org/sdr/MJYA201812076003), Dec 4, 2018: HOSE. FAILED. DURING CRUISE FLIGHT PORTION ENROUTE FROM KCKB TO KEWR WE EXPERIENCED AN A SYSTEM HYDRAULIC LOSS. AS SOON AS THE ADVISORY LIGHT ILLUMINATED BOTH THE F.O. AND MY
- [SDR 2017F00024](https://openairdocs.org/sdr/2017F00024), Jan 8, 2017: TRANSMITTER. FAULTY. FLAP ASYMMETRY ISSUE AFTER TAKE OFF. DECLARED AN EMERGENCY AND LAND AT ALTERNATE AIRPORT. AFTER TROUBLESHOOTING IT WAS DISCOVERED THAT THE RT FLAP TRANSMITTER A
- [SDR MJYA20170108001](https://openairdocs.org/sdr/MJYA20170108001), Jan 8, 2017: TRANSMITTER. FAILED. DURING CLIMB, THE PILOT TRIED TO SELECT FLAP UP WITH NO RESPONSE. THE FLAP INDICATION SHOWED THE RT FLAP AT 1 DEGREE AND THE LT FLAP AT 5 DEGREES. WITH NO RESPO
- [SDR CA151218005](https://openairdocs.org/sdr/CA151218005), Dec 16, 2015: WIRE. BURNED. (CAN) FOUND LT WING ANTI-ICE VALVE OPEN WHEN ACFT WAS ON THE GROUND. FAULT WAS FOUND TO BE BURNED WIRING CAUSING THE VALVE TO OPEN AND THE CIRCUIT BREAKER TO OP
- [SDR PCSA2014122201](https://openairdocs.org/sdr/PCSA2014122201), Dec 20, 2014: ENGINE. MAKING METAL. ENGINE NR 3 HAD A COMPRESSOR STALL & A FLAMEOUT AT FL320. METAL FOUND IN TAIL PIPE.
- [SDR CA140908023](https://openairdocs.org/sdr/CA140908023), Sep 7, 2014: OVERHEAT LOOP. OPEN. (CAN) AT THE TOP OF DECENT, OUR ACFT ILLUMINATED AN ENGINE OVERHEAT INDICATION ON NR 1 ENGINE. THE CREW FOLLOWED THEIR NON-NORMAL CHECKLIST WHICH SAID TO RETURN
- [SDR CA140806001](https://openairdocs.org/sdr/CA140806001), Aug 1, 2014: LINE. LEAKING. (CAN) 1 ENGINE OVERHEAT ILLUMINATED. SHUTDOWN NR 1 ENGINE BOTH EXTINGUISHER BOTTLES DISCHARGED. UPON INVESTIGATION MAINTENANCE FOUND NR 1 ENGINE, 13TH STAGE BLE
- [SDR 2WAA20140728001](https://openairdocs.org/sdr/2WAA20140728001), Jul 26, 2014: ENGINE. POWER LOSS. LOST THRUST ON LT ENGINE AFTER TAKEOFF. RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE. OPS CHECKED NORMAL. ACCOMPLISHED NR 1 ENGINE DFGC INTERMIX WIRI
- [SDR CA131213006](https://openairdocs.org/sdr/CA131213006), Dec 11, 2013: ENGINE. FAILED. (CAN) THE FLIGHT CREW REPORTED HEARING A LOUD BANG FROM THE NR 1 ENGINE AND LOSS OF THRUST. THE ACFT LANDED AND THE ENGINE WAS SHUTDOWN ON THE RUNWAY. MAINTENAN
- [SDR CA130905007](https://openairdocs.org/sdr/CA130905007), Jul 28, 2013: DUCT. DISCONNECTED. (CAN) AIR RETURN DUE TO HIGH, OFF SCALE, ENGINE OIL TEMPERATURE INDICATION. CREW FOLLOWED THE NON-NORMAL CHECKLIST AND ATTEMPTED TO SHUTDOWN THE ENGINE. CREW WA
- [SDR FDEA201209293509](https://openairdocs.org/sdr/FDEA201209293509), Sep 29, 2012: BLADES. DAMAGED. DURING CRUISE FLIGHT, NR 2 ENGINE THROTTLE LEVER BEGAN VIBRATING WITH ASSOCIATED MILD ACFT VIBRATION FELT. RAN QRH AND REDUCED NR 2 THROTTLE TO IDLE. SHORTLY AF
- [SDR SROM2011010](https://openairdocs.org/sdr/SROM2011010), Jul 20, 2011: CASE. CRACKED. REPLACED NR 1 ENGINE FAN INLET CASE DUE TO CRACKED FLANGE B WELD WITH OVERHAULED ASSEMBLY; FAN CASE P/N 786269, S/N DX6417, NR 1 BEARING HOUSING P/N 765471, S/N
- [SDR CA110412006](https://openairdocs.org/sdr/CA110412006), Apr 12, 2011: BLADE. FAILED. (CAN) SUSPECT T1 BLADE FAILURE, PRELIMINARY REPORT ONLY, MORE TO COME ONCE ENGINE IS TORN DOWN.
- [SDR TSAA1179002](https://openairdocs.org/sdr/TSAA1179002), Feb 18, 2011: OIL FILTER. SEPARATED. FLT 40. AFTER ADVANCING THE THROTTLES THE CREW NOTED THE NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATE FOLLOWED BY A DECREASE IN NR 2 ENGINE OIL QUANTITY. THE C
- [SDR TSAA1072014](https://openairdocs.org/sdr/TSAA1072014), Sep 9, 2010: ELEMENT. FALSE ACTIVATION. CREW NOTED THE NR1 ENGINE OVERHEAT LIGHT ILLUMINATED. CREW FOLLOWED QRH PROCEDURES AND SHUTDOWN THE NR 1 ENGINE. CREW LANDED WITHOUT FURTHER INCIDENT. MX REPLAC
- [SDR FDEA201009023245](https://openairdocs.org/sdr/FDEA201009023245), Sep 2, 2010: A/C PACK. 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 FDEA201008263156](https://openairdocs.org/sdr/FDEA201008263156), Aug 26, 2010: UNKNOWN. ODOR. AIR TURNBACK, SMOKE IN COCKPIT, SMOKE APPEARED TO ORIGINATE FROM THE THROTTLE QUADRANT. VISIBLY CHECKED FWD NOSE COMPARTMENT WIRING, LIGHT BALLAST AND UNDER QUA
- [SDR EE4Y100180](https://openairdocs.org/sdr/EE4Y100180), Jun 1, 2010: ANGLE. CORRODED. ((EE4Y)) LT WING NR 2 SLAT OTBD MAIN TRACK AREA LOWER ANGLE WITH CORROSION. (W/O Y10122, SUB JOB 5, ITEM 18).
- [SDR CA100526002](https://openairdocs.org/sdr/CA100526002), May 25, 2010: GEARBOX. LEAKING. ENGINE WAS LEAKING OIL FROM AROUND THE BANJO FITTING, ENGINE APPROX 70HRS SINCE SHOP VISIT - GEARBOX TO BE REPLACED. THIS IS A PRELIMINARY REPORT ONLY
- [SDR FDEA201005071486](https://openairdocs.org/sdr/FDEA201005071486), May 7, 2010: GEARBOX. LEAKING. DURING CRUISE NR 3 LOW OIL FILTER BYPASS LITE ILLUMINATED. OIL PRESSURE INDICATED 28PSI QTY WAS 3.5 GALLONS AND TEMP WAS 95 DEG, OPERATED 2 MIN AT IDLE SHUTDOWN
- [SDR FDEA200906182154](https://openairdocs.org/sdr/FDEA200906182154), Jun 18, 2009: OIL SYSTEM. LOW PRESSURE. LOW OIL PRESSURE LIGHT ILLUMINATED, OIL PRESSURE ON S/O'S PANEL INDICATED YELLOW ARC, PREFORMED ENG FAIL/SHUTDOWN CHECKLIST. DURING CHECKLIST OIL QUANITY DROPPE
- [SDR CA100215002](https://openairdocs.org/sdr/CA100215002), Apr 22, 2009: GCU. SMOKE. (CAN) DURING ENGINE START THE GCU STARTED TO SMOKE, THE CREW REMOVED THE GCU, MX INSTALLED A SERVICEABLE GCU. (TC 20100215002)
- [SDR PCSA2008111101](https://openairdocs.org/sdr/PCSA2008111101), Nov 11, 2008: TRANSMITTER. FAILED. ON DESCENT IN SDQ OIL QUANTITY GAUGE NR 3 BLED SLOWLY DOWN TO ZERO QUANTITY. OIL PRESSURE AND TEMPERATURE NORMAL BUT WERE VERY LIGHT SO A PRECAUTIONARY ENGINE S
- [SDR NWAA084589881](https://openairdocs.org/sdr/NWAA084589881), Oct 10, 2008: FUSE. FAILED. AFTER THE ACFT WAS PUSHED BACK FOR DEPARTURE AND FOLLOWING ENGINE START, THE RT HYDRAULIC SYSTEM LOST ALL FLUID. COM PROCEDURES WERE COMPLIED WITH AND THE ACFT 
- [SDR SROM20080023](https://openairdocs.org/sdr/SROM20080023), May 23, 2008: ENGINE. BIRD INGESTION. INGESTED LARGE BIRD ON APPROACH TO AKU, SHUT-DOWN ENGINE AND COMPLETED MISSED APPROACH. DIVERTED TO SCC AND MADE UNEVENTFUL LANDING. REMOVED AND REPLACED NR 1 E
- [SDR CA080630001](https://openairdocs.org/sdr/CA080630001), May 22, 2008: ENGINE. FAILED. (CAN) - ON DESCENT, A "BUZZING" SOUND WAS HEARD IN THE FLIGHT DECK FOR APPROX 5-10 SEC. THIS WAS FOLLOWED BY 1 OR 2 "POPS" AND THEN A LOUD "BANG" AT WHICH TIME 
- [SDR SROM2008017](https://openairdocs.org/sdr/SROM2008017), Apr 6, 2008: BRACKET. CRACKED. LEFT HAND ENGINE TAILPIPE CRACKED AT BRACKET MOUNT (3 O'CLOCK POSITION). REPAIRED LEFT HAND ENGINE TAILPIPE BRACKET MOUNT (3 O'CLOCK POSITION) IN ACCORDANCE WIT
- [SDR 2008032701](https://openairdocs.org/sdr/2008032701), Mar 27, 2008: TURBINE BLADES. FAILED. FLT 433 MIA-BLA - CREW REPORTED, LOSS POWER ON NUMBER NR 3 ENGINE ON TAKEOFF. THE CAPTAIN REJECTED TAKEOFF ROLL AT APPROXIMATELY 10 KNOTS. AIRCRAFT RETURNED BAC
- [SDR CA080225014](https://openairdocs.org/sdr/CA080225014), Feb 22, 2008: CLUTCH. DISENGAGED. DEPARTING YOW THE AIRCRAFT EXHIBITED AN UNCOMMANDED ROLL TO THE LEFT REQUIRING 2-3 UNITS OF RUDDER TRIM TO CORRECT. THE CREW OBSERVED NO ASSYMMETRY INDICATION I
- [SDR CA080121003](https://openairdocs.org/sdr/CA080121003), Jan 2, 2008: WIRE. INOPERATIVE. (CAN) TAIL 523 ON JAN 2ND APPROACH BACK COURSE ON RWY 15 YELLOWKNIFE 1040FT ASL 350FT AGL LEVEL FLIGHT 140K IN THIS CASE THE FLIGHT CREW EXPERIENCED A TAWS GENE
- [SDR DHL2007763001](https://openairdocs.org/sdr/DHL2007763001), Nov 10, 2007: WEB. CRACKED. A-6 CHECK, DISCREPANCY: AFT AIR STAIRS RT FWD LWR LIGHTING HOLE TORQUE BOX SKIN AREA IS CRACKED. ROUTED OUT CRACK IAW SRM 51-10-1 FABRICATED REPAIR DOUBLER FROM
- [SDR CA071106012](https://openairdocs.org/sdr/CA071106012), Nov 4, 2007: CIRCUIT BREAKER. FAILED. (CAN) ENROUTE AT FL300, THE CREW EXPERIENCED AN AUTO PILOT DISENGAGEMENT AS WELL AS THE LOSS OF THE FOLLOWING, YAW DAMPER, MACH TRIM, CAPTS. PITOT STATIC, NR 1 
- [SDR 1014200701](https://openairdocs.org/sdr/1014200701), Oct 14, 2007: OVERHEAT LOOP. OUT OF POSITION. AT CRUISE FL 310 AMERIJET FLIGHT 875 NUMBER 3 STRUT OVERHEAT LIGHT ILLUMINATED. LIGHT WENT OUT AFTER 2 MINUTES AND REMAINED OUT WITH ENGINE AT IDLE ONLY. THE FL
- [SDR SROM200725](https://openairdocs.org/sdr/SROM200725), Oct 5, 2007: WIRE. BURNED. DURING CLIMB SPARKS AND SMOKE EMITTED FROM THE AREA OF THE NR 1 START SWITCH. LOW IGNITION CB POPPED AT WHICH TIME THE SPARKS AND SMOKE CEASED. FLIGHT CREW RETU
- [SDR DHLA200700045](https://openairdocs.org/sdr/DHLA200700045), Sep 22, 2007: ENGINE. POWER LOSS. NUMBER ONE ENGINE DID NOT MAKE TAKEOFF THRUST, TAKEOFF REJECTED. ABNORMAL PROCEDURE COMPLETED N1 INDICATION 86 PERCENT ALL OTHER ENGINE PARAMETERS NORMAL.
- [SDR SROM200700018](https://openairdocs.org/sdr/SROM200700018), Aug 18, 2007: SKIN. NICKED. NICK STA 907 STR 22 LT. NICK AT STA 907, STR 22L REPAIRED IAW SRM 53-30-3, FIG 48. NICK BEYOND LIMITS AND DAMAGE REMOVED. HFEC IAW NDT PART 6, 53-30-00, FIG 4 O
- [SDR SROM200700019](https://openairdocs.org/sdr/SROM200700019), Aug 18, 2007: SKIN. NICKED. NICK STA 887 STR 24L-25L LT. DAMAGED AREA OF SKIN REMOVED AND REPAIR PLATES FABRICATED IAW SRM 53-30-3, FIG 48. INSTALLED REPAIR IAW 51-30-2.
- [SDR SROM200700020](https://openairdocs.org/sdr/SROM200700020), Aug 18, 2007: SKIN. NICKED. NICK STA 847 STR 21 LT. NICK AT STA 847 STR 21L FOUND TO BE BEYOND LIMITS. NICK REMOVED AND AREA AT STA 847 STR 21L REPAIRED IAW SRM 53-30-3, FIG 48.
- [SDR SROM200700014](https://openairdocs.org/sdr/SROM200700014), Aug 10, 2007: FLOORBEAM. CORRODED. NR296-CORROSION ON FLOORBEAM UPPER FLANGE AT STA 294 AND RBL 43 TO 53. FLOORBEAM UPPER FLANGE FROM RBL 6 (EXISTING SPLICE) TO RBL 60, STA 294 REMOVED AND REPLAC
- [SDR SROM200700007](https://openairdocs.org/sdr/SROM200700007), Aug 7, 2007: FLOORBEAM. CRACKED. NR228-CRACK IN FLOORBEAM AND WEB STA 660 BL0. CRACKED FLOORBEAM AND WEB AT STA 660 BL0 REPAIRED IAW MFG SB 737-57-1210, REV 1, DATED AUG 27/07.
- [SDR SROM200700022](https://openairdocs.org/sdr/SROM200700022), Aug 3, 2007: FRAME. CORRODED. NR145-LIGHT CORROSION ON FRAME AT STA 783 STR 25R. REPAIRED FRAME IAW MFG MESSAGE NR 1-518342007-2, DATED AUG 1, 2007 AND PRODUCTION DRAWINGS FOR PN 65-47959-47
- [SDR 07FDEA00130](https://openairdocs.org/sdr/07FDEA00130), Jan 18, 2007: ENGINE. FAILED. NR 2 ENGINE FAILED DURING CLIMB-OUT AT APPROX 1500 FT ABOVE GROUND. NOTED HIGH EGT (AROUND 780 C), EPR 0, N1 AND N2 WINDMILLING. OIL QTY 3 GALS ENGINE FAILED WI
- [SDR SROM200600021](https://openairdocs.org/sdr/SROM200600021), Dec 21, 2006: LANDING GEAR. CONTAMINATED. UPON DEPARTURE DURING HEAVY SNOW CONDITIONS WITH GRAVEL SKI EQUIPPED AIRCRAFT THE NOSE GEAR UNLOCK LIGHT REMAINED ON AFTER LANDING GEAR RETRACTION. LANDING GEAR
- [SDR SROM200600017](https://openairdocs.org/sdr/SROM200600017), Nov 9, 2006: ACCESSORY UNIT. FAULTY. DURING DEPARTURE, UPON LANDING GEAR RETRACTION RT MLG INDICATION REMAINED RED. MOVED LANDING GEAR HANDLE TO OFF AND THEN BACK TO UP, RED INDICATOR LIGHT REMAINE
- [SDR DHL2006783004](https://openairdocs.org/sdr/DHL2006783004), Nov 1, 2006: BATTERY. INOPERATIVE. EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERIES. OPS CK NORMAL IAW MM 33-50-71 PN-MISC062.
- [SDR DHL2006770517](https://openairdocs.org/sdr/DHL2006770517), Oct 16, 2006: STRINGER. CORRODED. BS 950F, STR 29R, OB STR CLIP HAS CORROSION. REMOVED FASTENERS FOR CORROSION REMOVAL IAW SRM 51-30-2. AFTER CORROSION REMOVAL IAW SRM 51-10-6 ON STR CLIP FOUND 
- [SDR DHL2006770519](https://openairdocs.org/sdr/DHL2006770519), Oct 11, 2006: TAB. DELAMINATED. LT WING, IB AILERON, TAB HAS T/E DAMAGE LWR IB SURFACE. REMOVED TAB IAW MM 27-10-11. CUT OUT DAMAGED AREA ON LWR SURFACE OF AILERON TAB APPOX 4.25 INCH BY 4.25 
- [SDR DHL2006513](https://openairdocs.org/sdr/DHL2006513), Oct 2, 2006: STRINGER. GOUGED. ASTAR NR 111564, DISCREPANCY: BS 334, STR 4L HAS DEEP GOUGE ON STRINGER, ABOVE AND AFT OF L1 DOOR EXIT LIGHT. CUT OUT DAMAGED AREA APPOX SIZE 2 INCH LENGTH IAW 

All 362: https://openairdocs.org/engine/pratt-whitney-jt8d-17a/reports.md

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

Approved for this engine model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

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

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first.

- [E741346](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186556581720260305201741.0001): Lock- Compressor Blade. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 741346 · Oct 31, 2024
- [811086](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID172993763520260305193806.0001): Housing Assy – Gearbox, Front. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 811086 · Oct 31, 2024
- [774403](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170344065020260305193807.0001): Blade – Turbine Rotor, 3 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 774403 · Oct 31, 2024
- [E655421](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID161625986720260305201740.0001): Washer – Key, Turbine Rotor, 2 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 655421 · Oct 31, 2024
- [466750](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID151358703220260305193807.0001): Ring – Oil Sealing, Compressor Rear Bearing. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 466750 · Oct 31, 2024
- [739585](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148214395320260305193808.0001): Seal Option (Interchange-ability Control No). Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 739585 · Oct 31, 2024
- [761519](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139626019620260305201741.0001): Bushing Option (Interchangeability Control No.). Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 761519 · Oct 31, 2024
- [809808](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125934943520260305193807.0001): Blade – High Pressure Compressor,    8 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 809808 · Oct 31, 2024
- [629886](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID112406865020260305193806.0001): Ring – Sealing, #3 Bearing. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 629886 · Oct 31, 2024
- [783852](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID106240135920260305193807.0001): Vane – Turbine Stator, 2 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 783852 · Oct 31, 2024
- [761518](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187972602620260305165918.0001): Boss Option(InterchangeabilityControl No.). Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 761518 · Oct 28, 2024
- [803915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181955192720260305211430.0001): Counterweight–Compressor. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 803915 · Oct 28, 2024
- [506503CL2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181748401820260318212721.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL2 · Oct 28, 2024
- [506503CL6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID181091118320260318212723.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL6 · Oct 28, 2024
- [822404](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180536206620260305211431.0001): Blade – TurbineRotor, 4 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 822404 · Oct 28, 2024
- [735330](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180290137320260318212719.0001): Fairing – Fuel Nozzle Support. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 735330 · Oct 28, 2024
- [474948P3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180277325820260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P3 · Oct 28, 2024
- [474948P12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176258339120260318212721.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P12 · Oct 28, 2024
- [761812](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173772421120260318212719.0001): Case – Turbine Exhaust Assembly of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 761812 · Oct 28, 2024
- [506503CL5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170888580720260318212723.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL5 · Oct 28, 2024
- [628777](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166995481720260318212719.0001): Spacer – Plate Combustion Chamber Duct Support. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 628777 · Oct 28, 2024
- [791047](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165505708420260305170150.0001): Duct Seg FanDifsr Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 791047 · Oct 28, 2024
- [506503CL1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID164114275620260318212721.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL1 · Oct 28, 2024
- [474949](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157358752120260305211424.0001): Stud – Plain, .190-24-32 x 1.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474949 · Oct 28, 2024
- [756505](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID155445952020260318212718.0001): Blade – Compressor Rotor 5 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 756505 · Oct 28, 2024
- [776616](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID150494846020260305211430.0001): Fairing – RearCompressor FanDuct, Assy Of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 776616 · Oct 28, 2024
- [811872](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145954136220260313172447.0001): Compressor Stator – 12 Stage, Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 811872 · Oct 28, 2024
- [810503](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142395769320260305211431.0001): Blade – LowPressureCompressor, 3 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 810503 · Oct 28, 2024
- [664236](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID141599681420260318212719.0001): Box & Cable – Thermocouple Assembly of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 664236 · Oct 28, 2024
- [768363](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136844616120260318212657.0001): Switch - Differential Pressure. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 768363 · Oct 28, 2024
- [525148](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136825413920260305211430.0001): Strut - FanExhaust. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 525148 · Oct 28, 2024
- [328419](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135955459520260305211424.0001): Seal .424 ID x .103 DIA - Round. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 328419 · Oct 28, 2024
- [506503CL3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135562819320260318212722.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL3 · Oct 28, 2024
- [474948](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135310988920260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948 · Oct 28, 2024
- [806748](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131570016020260313172447.0001): Case CC, Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 806748 · Oct 28, 2024
- [474948P9](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID131069181420260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P9 · Oct 28, 2024
- [505509](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID124953493420260305211430.0001): Shield - Heat,NR4 Bearing,Assy Of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 505509 · Oct 28, 2024
- [506503CL4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123460851220260318212722.0001): Metering Plug – Bleed Control. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 506503CL4 · Oct 28, 2024
- [616313](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121922278920260318212724.0001): Duct – Fan Combustion Chamber & Turbine Assy Of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 616313 · Oct 28, 2024
- [474948P6](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121155195220260318212720.0001): Stud – Plain .190-24-32 x 2.188 Long. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 474948P6 · Oct 28, 2024
- [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
- [AA134S-1KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184879292020230503123547.0001): Igniter Plug. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces AA134S-1 · Apr 27, 2023
- [RD1010](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119262724320230824100842.0001): Ring, Cut. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 709237 · Apr 18, 2023
- [1058V0400-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192781976020231218190434.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 804848 Original 6/19/89 · Apr 7, 2023
- [1058V0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179125890820240306163131.0001): Start Bleed Control Valve. Goodrich Corporation · PMA PQ1352NM · Replaces 793304 Rev. B (10-18-82) · Apr 7, 2023
- [1058V0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177996651520231218190434.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 793304 Rev. B (10-18-82) · Apr 7, 2023
- [1058V0400-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116398550720240306163132.0001): Start Bleed Control Valve. Goodrich Corporation · PMA PQ1352NM · Replaces 804848 Original 6/19/89 · Apr 7, 2023
- [1058V0400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198502891520230914183258.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 802211 Rev. ORIGINAL (6-21-85) · Mar 29, 2023
- [1058V0400-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125479340120230914183259.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 806146 Rev. Original (7-1-88) · Mar 29, 2023
- [1058V0600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115763985220230914183300.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 814099 Rev. Original (4-29-93) · Mar 29, 2023

All of them: https://openairdocs.org/engine/pratt-whitney-jt8d-17a/pma.md

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