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 DALA107319867Floor Panel · damagedDURING H-CHECK FOUND FLOOR PANEL NR 59 FWD END HAS ELONGATED FASTENER HOLE. REPAIRED IAW SRM 51-10-3, 51-70-4, 51-30-2.SDR DALA107329867Skin · dentedDURING H-CHECK FOUND SKIN DENT AT BS 217 BETWEEN L17R AND L18R. REPAIRED IAW DWG SG09530001.SDR DALA107259867Membrane · damagedDURING H-CHECK FOUND MEMBRANE DAMAGED AT BS 209 RBL10. REPAIRED IAW SRM 53-01 AND SRM 53-20-03-801.SDR DALA107159884Power Supply · inoperativeDURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 14-18 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE EMERGENCY LIGHT POWER SUPPLY AND OPS CHECKED THE SYS.SDR DALA107249867Floor Panel · crackedDURING H-CHECK FOUND FLOOR PANEL NR 20 IS CRACKED IN 3 PLACES AND HAS CORROSION ON TOP AND BOTTOM OF PANEL. REPAIRED IAW SRM 51-10-4.SDR DALA107359868Battery Pack · dischargedPILOT WROTE UP THAT THE EMERGENCY LIGHT SWITCH WAS IN ARM POSITION. FOUND ALL EMERGENCY BATTERIES DEAD. MX R & R ALL EMERGENCY BATTERIES.SDR DALA106969867Floor Panel · corrodedDURING H-CHECK FOUND FLOOR PANEL NR 78 BOTTOM EDGE CORRODED. REPAIRED IAW SRM 51-30-2, 51-10-4, 51-30-2.SDR DALA107059867Floor Panel · corrodedDURING H-CHECK FOUND CORROSION ON CABIN FLOOR PANEL NR 23. REPAIRED IAW SRM 53-23-0, 51-30-2, 51-30-8.SDR DALA107069867Floor Panel · damagedDURING H-CHECK FOUND FLOOR PANEL NR 72 SEVERAL FASTENER HOLES ELONGATED AND TORN OUT ON FWD AND AFT END OF PANEL. REPAIRED IAW SRM 51-70-04, 51-10-03, 51-70-04, 51-30-02.SDR DALA107079867Floor Panel · damagedDURING H-CHECK FOUND FLOOR PANEL NR 55 HAS HOLE ON INBD SIDE. REPAIRED IAW SRM 51-10-2, 51-10-4, 51-10-3, 51-30-2, 51-30-1.SDR DALA107089867Floorbeam · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS180 RBL 22-44. REPAIRED IAW SRM 51-10-4, 51-30-5, 51-20-0.SDR DALA107119867Skin · dentedDURING H-CHECK FOUND DENT IN SKIN AT BS 218 BETWEEN L17R AND L16R. REPAIRED IAW SRM 51-30-1, DWG SG09530001.SDR DALA106979867Floorbeam · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 200 BETWEEN LBL 22-44. REPAIRED IAW 53-01-1, 51-10-4, 51-30-5.SDR DALA106989867Floor Panel · corrodedDURING H-CHECK FOUND FLOOR PANEL NR 61 TOP AND BOTTOM CORRODED. REPAIRED IAW SRM 53-23-0, 51-10-2, 51-10-4, 51-30-2.SDR DALA106999867Seat Track · corrodedDURING H-CHECK FOUND CORROSION ON SEAT TRACK AT BS 200-275 LBL44. REPAIRED IAW SRM 53-05-4.SDR DALA107009867Floor Panel · gougedDURING H-CHECK FOUND FLOOR PANEL NR 73 TOP SKIN HAS HOLE GOUGED IN SURFACE. REPAIRED IAW SRM 53-01-4.SDR DALA107019867Floor Support · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 160-200 BETWEEN LBL44. REPAIRED IAW 51-10-3, 53-13-1, 51-10-1, 53-01-1, 51-10-4, 51-30-5.SDR DALA107029867Floor Support · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 218-275 BETWEEN BL 0. REPAIRED IAW 51-10-4.SDR DALA107039867Floor Support · corrodedDURING H-CHECK FOUND CORROSION ON FLOOR SUPPORT AT BS 160-200 BETWEEN RBL 44. REPAIRED IAW 51-10-1, 53-01, 53-30-02, 51-30-5, 51-10-4, 51-10-03.SDR DALA107149878Unknown · odorCABIN CREW REPORTED A STRONG BURNING SMELL THROUGHOUT CABIN AND DESCRIBED IT AS POSSIBLY ELECTRICAL IN NATURE. CREW SECURED THE GALLEY POWER AND THE FUMES DISSIPATED. FLIGHT CONTINUED TO SCHEDULED DESTINATION WITH GALLEY POWER DEACTIVATED. MX COULD NOT FIND ANSDR DALA107049867Web · crackedDURING H-CHECK FOUND CRACK ON FLOOR WEB UNDER FLOOR PANEL NR 98. REPAIRED IAW SRM 53-10-16, 51-10-3, 51-30-2.SDR DALA107109867Floorbeam · corrodedDURING H-CHECK, FOUND CORROSION ON FLOOR SUPPORT AT BS200 BETWEEN RBL 22-44. REPAIRED IAW SRM 53-13-1, 51-30-2.SDR DALA106949859Bulkhead · crackedDURING L-CHECK FOUND LT BULKHEAD WEB CRACKED IN FWD ACCESSORY COMPARTMENT AT BS 69. REPAIRED IAW SRM 53-01-2, 53-10-3, 51-30-2.SDR DALA106599852Battery Pack · inoperativeDURING LINE CHECK, MX FOUND THAT LT OVER WING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHT RETURNED TO AN OPS CONDITION.SDR DALA106749862Skin · corrodedDURING L-CHECK FOUND FUSELAGE SKIN CORRODED AT BS 656 L30R-L27L. REPAIRED IAW DWG 9923434 AND AMI CARD 5331-01180-02.SDR DALA106629862Floor Panel · corrodedDURING L-CHECK FOUND CORROSION ON FWD CARGO CTR FLOOR PANEL RIBS NR 1 THRU NR 6. REPAIRED IAW SRM 51-10-4, 51-60-0, 51-30-5, 51-30-1 & DWG 9B53-35812.SDR DALA106639867Door Frame · crackedDURING H-CHECK FOUND L1 DOOR JAMB WEB CRACKED AT ATTACH POINT TO INTERCOSTAL AT L12L. REPAIRED IAW SRM 53-01-4, 51-10-3, 51-30-2 AND 51-30-5.SDR DALA106509862Longeron · corrodedDURING L-CHECK, FOUND CORROSION ON LONGERON 30 END FITTING AT BS 674. REPAIRED IAW SRM 51-10-4 AND 51-10-3.SDR DALA106519862Floor Panel · damagedDURING L-CHECK FOUND DAMAGE TO CABIN FLOOR PANEL NR 69. REPAIRED IAW SRM 51-30-2 AND SRM 51-30-1.SDR DALA106529862Floorbeam · crackedDURING L-CHECK FOUND FLOOR SUPPORT AT FLOOR PANEL NR 69 HAS CRACKS AROUND RIVETS. REPAIRED IAW SRM 51-10-4, 51-30-2.SDR DALA106409852Unknown · odorTHE FLIGHT RETURNED TO DEPARTURE DUE TO STRONG ELECTRICAL SMELL IN THE FLIGHT DECK. THE FWD LAVATORY SMOKE DETECTOR ALSO WAS SOUNDING. GALLEY POWER WAS SELECTED OFF AND SMELL DISSIPATED. LANDING WAS UNEVENTFUL. MX COULD NOT DUPLICATE THE ELECTRICAL SMELL OSDR TSAA1077005Skin · crackedDURING SCHEDULED 2B CK INSP A 3 CIRCUMFERENTIAL CRACK AT BS 540 BETWEEN S-0 AND S-1L WAS DISCOVERED. CONFIRMED WITH EDDY CURRENT INSP. MX ACTION CUTOUT DAMAGE CRACK, USE A .50" RADIUS CUT AT CORNERS, MAINTAINED 2DMINIMUM EDGE DISTANCE, LAY-OUT DOUBLER AND TRIPSDR 2010FA0000187Battery Pack · inoperativeCENTER CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.SDR TSAA1077004Transmitter · inoperativeABORTED TAKEOFF, WHEN ADVANCING POWER FOR TAKEOFF NR 1 EPR MOVED SLOWLY AND ONLY WENT TO 1.50. ON TAXI BACK NR 1 EPR WOULD NOT MOVE. R & R NR1 ENGINE EPR TRANSMITTER IAW MM 77-11-21. GROUND RUN UP OPS & LEAK CK OK. ACFT RETURNED TO SERVICE.SDR FOTR20006NR4879Nose Cowl · chafedNR 3 ENGINE AFT T/E FROM 2-3 O`CLOCK POSITION CHAFED AND HOLE WORN THRU AS MARKED A NOSE COWL. REPAIRED ON FASI WO 20006, N/R 04879. REPAIRED NR 3 ENGINE NOSE COWL T/E FROM 2 TO 3 O’CLOCK POSITION IAW B727 SRM 54-10-3 FIG 3, REV 102. MATERIAL USED: ANGLE- 2SDR FDEA201001270270Compressor · stalledCLIMBING THROUGH 16,000 FT VERY LOUD "THUMP" WITH ASSOCIATED AIRFRAME SHUDDER. COMPLIED WITH QRH ENGINE COMPRESSOR STALL/LIMIT/SURGE AND RETURNED TO DEPARTURE. DID A WALK AROUND OF AFT. NO AIRFRAME DAMAGED NOTED. ALL CONTROL SURFACES ACCOUNTED FOR. R & SDR CA100121008Bellcrank · broken(CAN) DURING OPENING OF THE MAIN CARGO DOOR, THE FWD CLEVIS ON THE BELLCRANK ASSY WAS FOUND FRACTURED.SDR FDEA201001050009Transmitter · failedNR 2 EPR GAUGE FAILED ON T/O. ABORTED T/O. RAN REJECTED T/O CHECKLIST. WAITED REQUIRED 16 MINUTES FOR BRAKE COOLING. AFTER SUBSEQUENT T/O EPR GAUGE BEGAN TO OPERATE NORMALLY 20 MINUTES INTO FLIGHT. NR 2 ENG EPR LINE PURGED WITH NITROGEN IAW MM REF: 77-11-SDR DALA1100989855Doubler · crackedMAIN PASSENGER CABIN RT STA 256, WINDOW DOUBLER FWD TOPCORNER CRACK BELOW FASTENER. CUTOUT DAMAGED AREA AND NDT VERIFIED DAMAGE REMOVED IAW NDT SPM 06-10-01. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05.SDR 2010F00000Spar · corrodedDURING CPCP, THE INSPECTOR PERFORMED VISUAL INSPECTION AND FOUND CORROSION ON RT WING FRONT SPART LOWER CHORD PLATE AT WS 482. AFTER REPAIRING TO THE FRON SPAR LOWER CHORD PLATE, FORM 337 WILL BE SUBMITTED TO FAA FOR FINAL RESULT OF CORRECTIVE ACTIONS DETAIL.SDR CA100104005Spindle · cracked(CAN) SPINDLE BROKE IN AREA OF AD 2003-24-08 PRIOR TO THE INSP THRESHOLD OF 3000C. UNIT HAD BEEN O/H, FAILED PART IS CURRENTLY WITH QA AND WILL BE SHIPPED TO MFG UNLESS OTHERWISE INSTRUCTED. FLAP SPINDLE CRACK OCCURRED AT CRITICAL "A" AREA SPECIFIED IN ASB 73SDR TSAA0975015Duct · failedNON-ETOPS CARGO FLIGHT, DURING CLIMB, THE CREW NOTED THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATE. NR1 ENGINE EGT REMAINED WITHIN LIMITS. THE NR 1 THROTTLE WAS RETARDED TO IDLE AND THE OVERHEAT LIGHT EXTINGUISHED. ENGINE WAS KEPT AT IDLE AND THE CREW RETURNED SDR CA091022001Screw · wrong part(CAN) FUEL PANELS HAD BEEN OPEN FOR MAINTENANCE, WHEN IT CAME TIME FOR RE-TORQUE OF THE SCREWS, THE SCREWS BOTTOMED OUT, AS THEY WERE THE WRONG LENGTH. MAINTENANCE CONTRACTOR HAS BEEN ADVISED. PROPER SCREWS HAVE BEEN INSTALLED (TC 20091022001)SDR NWAA093189874Seal · blownDURING CLIMB AT APPROX 800FT ENGINE NR 2 FLAMED OUT. FLIGHT CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT PERFORMING AN UNEVENTFUL LANDING. MAINTENANCE FOUND BLOWN SEALS AT THE FUEL IN LINE TO THE P&D VALVE.SDR TSAA0932009Shutoff Valve · inoperativeON TAXI-OUT, THE "ANTI-SKID INOP" LIGHT ILLUMINATED AND THE "FAIL WARN AND PARK BRAKE" CIRCUIT BREAKER POPPED. RETURNED TO RAMP. MX REMOVED AND REPLACED THE PARKING BRAKE SHUT OFF VALVE IAW MM 32-44-21. OPS AND LEAK CHECK OK. ACFT RETURNED TO SERVICE.SDR TSAA0977008Probe · obstructedON TAKEOFF ROLL, HAD HIGH EPR FOR 2 ENG. ALL OTHER INDICATIONS MATCHED NR 1 ENGINE. ABORTED TAKEOFF "UNEVENTFUL" AND RETURNED TO RAMP. MX FOUND BUG IN THE NR 2 ENG PT2 PROBE. CLEARED PROBE; OPS CHECK OK. ACFT RETURNED TO SERVICE.SDR I5PA20090719Line · crackedAFTER 30 MINUTES OUT, CREW CALLED IN DUE TO RAPID LOSS OF OIL QUANTITY ON NR 1 ENGINE. ON LANDING, OIL QUANTITY INDICATED 1.5 GALLONS. MX RAN ENGINE, FOUND LEAK IN TAIL PIPE, FOUND SCAVENGE LINE NR6 BEARING LEAKING. REMOVED AND REPLACED SCAVENGE LINE. ALSOSDR CA090716006Seal · leaking(CAN) AFTER A CHANGE OF GEARBOX FOR ONE REMOVED SERVICEABLE FROM ANOTHER ENG, THE ENG STARTED LEAKING OIL IN FLIGHT, WHICH GAVE INDICATIONS OF OIL FLUXUATION. ENG WAS SHUTDOWN AS A PRECAUTION. SEAL WHEN REMOVED WAS FOUND FULL OF CARBON. SEAL WAS REPLACED, ASDR TSAA0926005Fire Loop · malfunctionedFLT 42, ENG NR 1 (OVERHEAT WARN) LIGHT FLICKERING DURING TAXI. RETURNED TO BLOCK. TRIED FIRE CONTROL MODULE, FIRE DETECTION UNIT AND DISCONNECTED NR1 ENG FIREWALL CONNECTOR, LIGHT STILL FLICKERING. RE-INSTALLED ORIGINAL COMPONENTS AND CONNECTOR. REMOVED ANDSDR CA091002004Accumulator · out of tolerance(CAN) PART WAS INSTALLED WHEN NOT IN COMPLIANCE WITH AD 2003-11-03 THIS AD EFFECTIVE O3-JULY-03 STATES THAT PN 2660 472M2 MAY NOT BE INSTALLED ON ANY ACFT.
Back to Pratt & Whitney JT8D-17