Pratt & Whitney JT8D-17
Service difficulty reports · 1,680
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'JT8D17' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE engine_model_key = 'JT8D17' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR C8GA20010019Bolt · missingFLT 201 FROM MIA TO CCS. AFTER TAKEOFF NR 1 ENGINE STAYED AT FULL POWER AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. ACCOMPLISHED NR 1 ENGINE SHUTDOWN AND AIR TURNBACK TO MIA AND LANDED WITHOUT ANY INCIDENT. INVESTIGATION FOUND THE LOWER THRUST CRANK BOLT WASDR BJN2001F00004Latch · unlatchedDURING FLIGHT, THE SR FLIGHT ATTENDANT NOTIFIED THE CAPTAIN THAT A PIECE OF COWLING WAS LOOSE. THE CAPT CONFIRMED THAT THE NACELLE FAIRING THAT LIES BETWEEN THE WING AND THE ENGINE COWLING WAS LOOSE, THE COWLING LATCH HAD COME UNDONE AND THE FAIRING WAS AJAR SDR BJN2001F00000Connector · disconnectedEMERGENCY ESCAPE PATH MARKING SYSTEM INOPERATIVE FROM ROW 1 TO ROW 15. FOUND FLOOR CONNECTOR UNPLUGGED, RECONNECTED, OPS CHECK GOOD, OK FOR SERVICE.SDR CA020121008Spar · cracked(CAN) RT ELEVATOR REAR SPAR AT TRIM TAB ATTACHMENT POINT FOUND CRACKED. ELEVATOR REMOVED FOR REPAIR, LOCATION OF DAMAGED LOCATED AT STATION 66.54 REPLACED ELEVATOR. DAMAGE REPAIRED AS PER SRMSDR BJN2001F00001Light · inoperativeL2 DOOR EMERGENCY EXIT PORTABLE LIGHT INOPERATIVE. REMOVED AND REPLACED PORTABLE EMERGENCY EXIT LIGHT ON L2 DOOR, OPS CHECKED NORMAL.SDR CA011010002Uplock Sensor · failed(CAN) SHORTLY AFTER TAKEOFF DUE TO UNSAFE LT MLG INDICATION. CREW REPORTED ON CLIMB OUT LEFT MAIN GEAR RED UNSAFE LIGHT ILLUMINATED AFTER GEAR LEVER SELECTED UP. DECISION MADE TO RETURN TO YEG & A/C LANDED W/O INCIDENT. MAINTENANCE INSPECTION REVEALED PROBLEM SDR CA011018005Control Cable · failed(CAN) NOSE GEAR WHEEL WELL DOORS LOWER CABLE REPLACED IN ACCORDANCE WITH MAINTENANCE MANUAL. GEAR SWING CARRIED OUT AND CHECKED SERVICEABLE.SDR CA011114010Controller · failed(CAN) PRESSURE CONTROLLER FAILED ON CLIMB OUT FROM YYC. A/C RETURNED TO YYC. O2 MASKS DEPLOYED. CABIN PRESSURE CONTROLLER FAILED FUNCTION TEST ON GROUND. REPLACED O2 MASKS AND REPLACED PRESSURE CONTROLLER. FUNCTION CHECK CARRIED OUT AND A/C RETURNED TO SERVICESDR 2001UALA02084Actuator · failedUNSCHEDULED LANDING UNDER AMBER ALERT DUE TO A RED GEAR LIGHT INDICATION. FLIGHT CREW REPORTED AFTER TAKEOFF, AT LANDING GEAR RETRACTION WITH GEAR HANDLE IN OFF POSITION HAD RIGHT MAIN GEAR RED UNSAFE LIGHT INDICATION. DURING TROUBLESHOOTING FOUND RIGHT GEARSDR 2001UALA01984Skin · damagedAIRCRAFT HAS 32 INCH CREASE IN RIGHT SIDE OF FUSELAGE WITH CENTER 18 INCH PUNCTURE BETWEEN STATIONS 907R-947R CROSSING STRINGERS 22R AND 23R. MAJOR REPAIR ACCOMPLISHED. SPLICED SECTIONS OF S22R AND S23R. REPAIRED SHEAR TIE STA 927. REPAIR SKIN WITH TRIPLER SDR 2001UALA01922Bulkhead · crackedSTATION 178 WEB CRACKED AT LBL 5, 7 AND WL 200. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR C1HA200196014Warning System · malfunctionedON T/O ROLL AT 40 KNOTS APT ARMED FOLLOWED BY AUTO PACK TRIP AND ENG FAIL LIGHTS ILLUMINATED, ABORTED T/O RETURN TO GATE. INSPECTED AND CHECKED ENGINES RAN ENGINE AT TAKE-OFF EPR AND OPS CHECK NORMAL.SDR 2001UALA01915Bulkhead · crackedBULKHEAD BODY STATION 178, RBL 7, WL 224 CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.SDR CA010907014Tire · separated(CAN) RECAP SEPARATED FROM TIRE ON TAKEOFF FROM YVR WAS NOT NOTICED UNTIL AIRCRAFT ARRIVED IN YLW. NO OTHER REPORTABLE DAMAGE AS A RESULT OF THIS INCIDENT.SDR 2001UALA01887Doubler · gougedFOUND GOUGE ON INTERNAL DOUBLER OF SKIN AT BODY STATION 787 STRINGER 6L. MAJOR REPAIR ACCOMPLISHED INSTALLED DOUBLER REPAIR.SDR 2001UALA01888Stringer · crackedSTRINGER 6-L CRACKED AT BODY STATION 787. MAJOR REPAIR ACCOMPLISHEDINSTALLED REPAIR DOUBLER.SDR 2001UALA01876Linkage · damagedNR 1 ENGINE SHUTDOWN DUE TO THROTTLE CONTROL PROBLEM. *S/D* FOUND THE THROTTLE LINKAGE DISCONNECTED. REINSTALLED THE LINKAGE AND TRIMMED THE FUEL CONTROL.SDR COOSDR010075Skin · delaminatedLEFT WING, GROUND SPOILER NR 4, PN 6579952-5 DHL, MD-364 UPPER SKIN DELAMINATED.SDR COOSDR010077Skin · delaminatedLEFT WING, SLAT NR 1, PN 65-46421-165, SN 132 UPPER SKIN DELAMINATED.SDR COOSDR010076Skin · delaminatedRIGHT WING, FLIGHT SPOILER NR 8 PN 65-79952-7, MA-532, UPPER SKIN DELAMINATED.SDR COOSDR010078Longeron · crackedENGINE NR 2, FORWARD FIREWALL-LONGERON, PN 65-53558-54 CRACKED.SDR COOSDR010079Skin · delaminatedRIGHT WING, OUTBOARD AFT FLAP PN 65-46435-236, SN 333, UPPER SKIN DELAMINATED.SDR COOSDR010081Skin · delaminatedLEFT WING, INBOARD AFT FLAP, PN 65ND27301-1, SN BN-2. LOWER AND UPPER SKIN DELAMINATED.SDR COOSDR010082Skin · delaminatedRIGHT WING, INBOARD AFT FLAP PN 65ND-27301-2, SN BN2, LOWER AND UPPER SKIN DELAMINATED.SDR CA010921007Engine · failed(CAN) ENROUTE FROM YVR TO YYC EXPERIENCED COMPRESSOR STALL ON NR 1 ENGINE. UPON ESTABLISHING CRUISE POWER SETTNG, CREW HEARD LOUD POP, FOLLOWED 20 SEC LATER BY ANOTHER POP (SEVERE COMPRESSOR STALL) & ASSOCIATED NR 1 ENGINE PRESSURE RATIO (EPR), N1 POWER SURSDR 2001UALA01720Transmission · failedLANDED UNDER AMBER ALERT DUE TO STUCK TE FLAPS. SUPPLEMENTAL DATA UPDATE REPLACED THE #4 TRAILING EDGE FLAP TRANSMISSION.SDR CA010905007Module · shorted(CAN) ON LANDING IN YHZ LOWER PANEL CAUTION LIGHTS CAME ON & WOULD NOT EXTINGUISH. FOUND SCREW SHORTING TERMINAL OF LANDING GEAR WARNING INDICATION MODULE SOCKET. REMOVED SCREW AND CHECKED INDICATION SYSTEM & ASSOCIATED SYSTEMS. ALL INDICATIONS & OPEATIONS NOSDR COOSDR010100Skin · delaminatedFUSELAGE SKIN FROM BS 847 TO BS 867 BETWEEN STR 22R AND STR 23R WITH DELAMINATION.SDR COOSDR010101Skin · crackedFUSELAGE SKIN FROM BS 500B+6 TO BS 500B+10 AT STR 19R UPPER SKIN WITH CRACK INDICATION.SDR COOSDR010102Doubler · debondedFUSELAGE SKIN FROM BS 335 TO BS 350 BETWEEN STR 24L AND STR 25L WITH DOUBLER DEBONDED.SDR COOSDR010103Skin · corrodedFUSELAGE SKIN AT BS 340 AT STR 24L WITH CORROSION.SDR COOSDR010104Skin · delaminatedFUSELAGE SKIN FROM BS 950 TO BS 955 BETWEEN STR 5R AND STR 6R DELAMINATED.SDR COOSDR010105Bulkhead · crackedBULKHEAD WEB SECTION CRACKED, AT LBL 10, BETWEEN WL 237.25 AND WL 230.5.SDR COOSDR010106Bulkhead · crackedBULKHEAD WEB SECTION CRACKED, RBL 10, BETWEEN WL 237.25 AND WL 230.5SDR COOSDR010107Doubler · delaminatedFUSELAGE SKIN DOUBLER FROM BS 639 TO BS 663 BETWEEN STR 9L AND 10L WITH DELAMINATION.SDR COOSDR010108Skin · delaminatedFUSELAGE SKIN SECTION FROM BS 635 TO BS 663 BETWEEN STR 14R AND 15R WITH DELAMINATION.SDR COOSDR010109Rib · crackedLEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 267, NR3 SLAT INBOARD MAIN TRACK SUPPORT.SDR COOSDR010110Rib · crackedLEFT WING LEADING EDGE RIB CRACKED, LOCATED AT FSS 394, NR2 SLAT OUTBOARD MAIN TRACK SUPPORT.SDR COOSDR010111Skin · debondedFUSELAGE SKIN SECTION FROM BS 330 TO BS 350 BETWEEN STR 21L AND 23L WITH DISBONDING.SDR CA010906019Valve · failed(CAN) TWO AIR TURN BACK DUE TO A #1 START VALVE OPEN LIGHT ILLUMINATED DURING FLIGHT. ACCOMPLISHED #1 ENGINE FAILURE SHUTDOWN TWICE.AFTER THE FIRST INCIDENT, THE STARTER, START VALVE AND ACTUATOR PRESSURE SWITCH WERE CHANGED, & THE SECOND TIME THE START VALVE SDR 2001UALA01481Stringer Clip · damagedSTRINGER CLIP DAMAGED, AT BS500B, STR1L. REPLACED STRINGER CLIP. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01477Door Frame · damagedFWD CARGO DOOR FRAME DAMAGED AT LOWER FORWARD CORNER. REPLACED FRAME. MAJOR REPAIR ACCOMPLISHED.SDR CA010724026Wheel · cracked(CAN) DURING SERVICE CHECK, NR 1 MAIN WHEEL TIRE PRESSURE FOUND TO BE 40 PSI PRESSURE DETECTED TO BE LEAKING AT WHEEL HUB. NR 1 AND 2 MAIN WHEEL ASSEMBLIES REPLACED, NO FURTHER FAULTS AFTER 8 FLIGHT SEGMENTS.SDR 2001UALA01360Skin · wornLH WING LE SKIN WORN AT NUMBER 2 SLAT CENTER STOP. MAJOR REPAIR ACCOMPLISHED.INSTALLED DOUBLER.SDR 2001UALA01361Floorbeam · corrodedFLOORBEAM T CAP CORRODED. STA 967, RBL 4 TO RBL 45. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED TCAP SPLICE REPAIR.SDR 2001UALA01362Stringer · corrodedSTRINGER CORRODED. STR 6L, STA 767. MAJOR REPAIR ACCOMPLISHED.INSTALLED STRINGER SPLICE AND REPLACED TIE CLIP.SDR 2001UALA01348Track · out of adjNR 6 SLAT WOULD NOT RETRACT. *S/D* ACCOMPLISHED ADJUSTMENT OF THE NR 6 SLAT AUXILIARY TRACKS. EXTENDED AND RETRACTED SLATS SEVERAL TIMES. NO BINDING NOTED. OPERATION SMOOTH, ALL INDICATIONS NORMAL.SDR C1HA200186007Engine · fod#2 eng EPR dropped from 2.19 to 2.12 after liftoff #2 power lever @ firewall 3 to 4 inches further than 1 or 3. Air return/Return to block.Action Taken:Inspection found internal compressor damage. Removed and replaced #2 engine.SDR C1HA200183004Fitting · looseENGINE NR 1 OIL QUANTITY GAUGE ROLLED DOWN TO ZERO EN ROUTE. TEN MIN LATER LOST PRESSURE AND LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN. FOUND LOOSE FITTING ON BOTTOM OF GEARBOX. RETORQUED PER JT8D MANUAL, INSPECTED MAIN OIL FILTER AND NO DSDR C1HA200182009Engine · failed#3 Engine Failed on takeoff.ACTION TAKEN:Inspected and found #3 engine turbine failure. R&R'd #3 engine.
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