Pratt & Whitney JT8D-15
Service difficulty reports · 2,710
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 = 'JT8D15' 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 = 'JT8D15' 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 TSAA0253152Skin · crackedFOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.SDR PCS2003F00000Line · looseCREW REPORTED NR 2 ENGINE PRECAUTIONARY SHUTDOWN DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE FLUCTUATING IN FLIGHT. AIRCRAFT LANDED AT THE INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR 2 ENGINE OIL PRESSURE LINE LOOSE. THE LINE WAS TISDR AUS20021026Fitting · corroded(AUS) WIRING LOOM STANDOFF CORRODED. STANDOFF IS LOCATED IN RH WING LEADING EDGE ZONE 64 STN 286.897. FOUND DURING CPCP INSPECTION.SDR AUS20021027Support · corroded(AUS) WIRING LOOM CLAMPS CORRODED. CLAMPS AT LOCATED AT UPPER SKINSUPPORT RIBS - ZONE 64 STN 244.217, STN 270.217, STN 298.497 ANDSTN 284.0. FOUND DURING CPCP INSPECTION.SDR AUS20021028Stringer · corroded(AUS) UPPER WING STRINGERS CORRODED. STRINGERS ARE THE SECOND AND THIRD STRINGERS FROM LEADING EDGE LOCATED OUTBOARD OF STN 210.217.FOUND DURING CPCP INSPECTION.SDR 02FDEA00364Engine · failedAFTER 30 MINUTES IN FLIGHT OIL TEMP CLIMBED TO YELLOW BAND DURING RED TAB PROCEDURES WITH ENGINE AT IDLE TEMP CLIMBED ABOVE RED BAND. SHUT DOWN NR 3 ENGINE IN ACCORDANCE WITH RED TABS. REMOVED AND REPLACED OIL TEMP BULB PER M/M 727-200 79-34-021-4, LEAK AND SDR AUS20021025Rib · corroded(AUS) RH WING UPPER SKIN SUPPORT RIB CORRODED UNDER P' CLAMP LOCATED AT OUTBOARD END OF NO6 LEADING EDGE FLAP - ZONE 64 STN WS 330.5. FOUND DURING CPCP INSPECTION.SDR AUS20021029Hinge · corroded(AUS) RH OUTBOARD AILERON ATTACHMENT HINGE CORRODED. CORROSION IS LOCATED AT ZONE 88 WBL 492.0. FOUND DURING CPCP INSPECTION.SDR AUS20021034Hinge · corroded(AUS) LEADING EDGE FLAP LH HINGE FITTING CONTAINED SEVERE EXFOLIATION CORROSION AROUND BUSH. FOUND DURING CPCP INSPECTION.SDR AUS20021033Hinge · corroded(AUS) OUTBOARD AILERON INPUT ROD ATTACHMENT FITTING CORRODED. AILERON UPPER SKIN CRACKED AND LOWER SKIN CORRODED. LOCATED IN ZONE 81WBL 492.0. FOUND DURING CPCP INSPECTION.SDR TSAA0253134Pressure Panel · corrodedFOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR.SDR MYW2002F00000Engine · making metalPRIOR TO DESCENT NR 2 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT ILLUMINATED. ENG NR2 PARAMETERS INDICATION ARE NORMAL OIL PRESS 47 PSI, OIL TEMP 81 DEGREE C, EPR NR 2-165, N1-80.9, EGT-400 DEG. C, N2-85.9, FF-3000PPH, CSD IN TEMP 50 DEG. C, RISE -8 DEG. C. GESDR DL73K020534Connector · damagedA/C RETURNED TO GATE DUE TO NR 2 FUEL FLOW INDICATION BEING ERRATIC. DISCONTINUED T/O AT 70 KTS - GW 117.0. NR 2 ENGINE FUEL FLOW WENT TO MAX THEN ZERO FUEL FLOW. FOUND AFT CANNON PLUG ON FUEL FLOW TRANSMITTER DAMAGED. REPLACED NR 2 ENGINE FUEL FLOW TRANSMSDR TSAA0251130Slat · corrodedFOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0251132Bracket · chafedFOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0251133Skin · gougedFOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0253125Spar · corrodedFOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLER. REPAIR COMPLETEDSDR TSAA0253131Floorbeam · crackedFOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DOUBLER CONTAINING THE CRACKS. FABRICATED ALL REPAIR PARTS. INSTALLED SPLICE ANGLES AND STRAPS WITH NUT PLATES. COMPLETED INSTALLATION OF RSDR TSAA0253128Stringer · dentedFOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT TO THE PRODUCTION SPLICE. FABRICATED NEW STRINGER SEGMENT. INSTALLED STRINGER PER SRM 53-10-3. COMPLETED REPAIR. AIRCRAFT RETURNED TO SERSDR TSAA0253126Bulkhead · crackedFOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PARTS. AIRCRAFT RETURNED TO SERVICE.SDR TSAA0253127Bulkhead · crackedFOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PART.SDR GAIA02039OPBleed Valve · leakingFLT 734- FWA-DFW - NR 3 ENGINE STRUT OVERHEAT ILLUMINATED IN FLIGHT. THE CREW ISOLATED THEN RN 3 BLEED, AND OPERATED AT REDUCED THRUST TO EXTINGUISH THE LIGHT. THE AIRCRAFT CONTINUED ITS FLIGHT AND THE LANDING AT FWA WAS UNEVENTFUL. REPLACED CLAMPS ON NR 3 SDR GTIA020262Fan Blade · damagedFLL - NR 1 ENGINE HAS FOD. FOUND THREE BLADES OUT OF LIMITS. REPLACED 3 AT SET OF C-1 BLADES IAW PWA JT8D FM P/N 773128 723302. PERTINENT DETAILS ARE ON FILE UNDER W/O 3198. (M)SDR CA020403001Isolation Valve · leaking(CAN) A/C ON ROUTINE FLT ON APPROACH PLANNED FLAPS FOR LDG & SELECTED FLAPS ON SCHEDULE. AFTER FLT CREW SELECTED FLAP TO 25 DEGS, MASTER CAUTION HYDRAULIC WARNING LIGHT FLASHED. AT TIME CREW NOTICED 'A' SYS HYDRAULIC QUANTITY READING ZERO - HYDRAULIC PRESSURE SDR CA020328001Spacer · missing(CAN) DURING LINE MAINT IMPACT DAMAGE NOTICED ON LOWER SEGMENT CLEVIS ASSY. SIDE STRUT HAD BEEN OVERHAULED. THE AIRCRAFT JACKED & UPON INVESTIGATION. IT FOUND THAT EXCESSIVE PLAY BETWEEN CLEVIS ASSY & LOWER SEGMENT OF SIDE STRUT. LOWER SEGMENT REMOVED & FWDEDSDR CG8A20020005Engine · vibrationFLT 202 FROM MPTO TO KMIA. DURING CRUISE LEVEL, AT FL310 THE NR 2 ENGINE EXPERIENCE VIBRATION THAT WAS FELT IN THE NR 2 THROTTLE. AT IDLE, THE NR 2 OIL PRESSURE REMAINED NORMAL UNTIL THE OIL PRESSURE/FILTER BYPASS LIGHT ILLUMINATED. A PRECAUTIONARY ENGINE SSDR CA020321002Controller · malfunctioned(CAN) SHORTLY AFTER TAKEOFF WHILE CLIMING THROUGH 31,000 FT, CREW NOTICED THAT CABIN ALTITUDE READING 9,500 FT. A/C DESCENTED TO 14,000 FT. CREW DONNED OXYGEN MASKS, AS PER QRC FOR RAPID DEPRESSURIZATION & PROCEEDED TO SELECT MANUAL CONTROL ON PRESUURIZATION PSDR DL72S020246Compressor · stalledON TAKEOFF NR 3 COMPRESSOR STALLED. AIRSPEED PLUS 130 ENG HEAT WAS ON USING AT 35 PWR WINDS 330/20 GUSTING TO 28. PERFORMED ENGINE COMPRESSOR STALL CHECK INSPECTION. NO DEFECTS FOUND AND ENGINE TAKEOFF POWER RAN NORMAL. AIRCRAFT, OKAY FOR SERVICE.SDR P2EA2002M028Bleed Valve · lack of lubeNR 2 ENGINE COMPRESSOR STALLED AS THE THROTTLES WERE ADVANCED FOR TAKEOFF. LUBED THE NR 2 ENGINE BLEED VALVES IAW AMM 75-31-0. RAN ENGINE, OPS CHECKED GOOD.SDR AUS20020240Balance Weight · corroded(AUS) RH ELEVATOR TAB CENTRE BALANCE WEIGHT SPLIT OPEN DUE TO CORROSION.SDR CA020218001Control Unit · malfunctioned(CAN) AT FLAP EXTENSION FOR LANDING, NR 3 LEADING EDGE SLAT SHOWS YELLOW AT FLAP 1 WITH OVERHEAD PANEL CAUTION "LE FLAP INTRASIT" LIGHT STAYING YELLOW UNTIL FLAP 15 IS SELECTED. OCCURS IN FLT BUT SEEMS TO WORK FINE ON GROUND. "MAINT INSPECTION FOUND NR 3 SLAT SDR AUS20020241Panel · corroded(AUS) HORIZONTAL STABILISER PANEL LOCATED ABOVE BAY THREE CORRODED IN AREA OF REAR AUXILIARY SPAR LH SIDE.SDR AUS20020250Door · corroded(AUS) MAIN CARGO DOOR STRUCTURE CORRODED AT THE LAP JOINT LOCATED ATSTN 620. CORROSION LOCATED AT ZONE 2-48, STN 620 TO STN 623,STRINGER 4LH TO STRINGER 5.SDR AUS20020251Door · corroded(AUS) MAIN CARGO DOOR STRUCTURE LAP JOINT CORRODED AT STN 620.CORROSION IS LOCATED AT ZONE 2-48, STN 620 TO STN 623, STRINGER 9LH TO STRINGER 11.SDR AUS20020252Skin · corroded(AUS) MAIN CARGO DOOR SUPPORT STRUCTURE TOP FORWARD CORNER CORRODED.CORROSION LOCATED AT ZONE 2-24, STN 48D, STRINGER 1LH TO STRINGER 3.SDR CA020131001Nut · missing(CAN) SCHEDULED MAINTENANCE DURING REGULAR SCHEDULED OVERNIGHT MAINTENANCE; AD:99-26-07 (A)(2),INSPECTION OF NR 1 ENGINE AFT MOUNT CONE BOLT SECONDARY SUPPORT, WESTJET ENGINEER FOUND THE SECONDARY SUPPORT NUT, P/N:84821CD-524 MISSING. MAINTENANCE REPLACED THE SDR AUS20020246Support · corroded(AUS) LH MAIN LANDING GEAR DOOR SEQUENCING STRIKER FRAME CORRODED.LOCATION OF CORROSION ZONE 1-35, STN 880, STRINGER 20LH, WL 152,BL70LH.SDR AUS20020248Structure · corroded(AUS) UPPER RT WING TOP CHORD CORRODED. CORROSION LOCATED AT ZONE 6-76, WS 351RT TO WS 355 RT.SDR AUS20020249Spar · corroded(AUS) LT REAR WING SPAR UPPER AND LOWER CHORDS CORRODED IN AREA LOCATED BEHIND THE VERTICAL STIFFENER. CORROSION LOCATED AT ZONE 6-72, WS 437 TO WS 438 LT.SDR AWXA200200085Transmitter · reads lowAT TAKEOFF FROM PHX ENROUTE TO SLC, NR 1 ENGINE OIL PRESSURE READ 26 PSI AT 80 KTS, ALL OTHER ENGINE INDICATIONS WERE NORMAL, ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND REPLACED THE NR 1 ENGINE OIL TRANSMITTER. ENGINE RUN OPERATIONAL CSDR AUS20020247Stiffener · corroded(AUS) LT MAIN LANDING GEAR BAY STIFFENER CHORD CORRODED IN SEVERAL AREAS INCLUDING ATTACHMENT TO PRESSURE DECK. CORROSION LOCATED IN ZONE 1-35, STN 870, STRINGER 20 LT TO STRINGER 17, WL 208 TO WL184, BL 67 LT.SDR AUS20020253Skin · corroded(AUS) SKIN CORRODED IN AREA BELOW TOILET SERVICE DOOR. CORROSIONLOCATED AT ZONE 2-11, STN 350 TO STN 370, STRINGER 18RH.SDR AUS20020245Frame · corroded(AUS) RH MAIN LANDING GEAR WHEEL WELL DOOR SEQUENCING STRIKER FRAME CORRODED. FRAME LOCATED IN ZONE 1-36, STN 880, STRINGER 520RH,WL157, BL70RH.SDR AUS20020244Plate · corroded(AUS) CARGO DOOR HINGE SUPPORT PLATE CORRODED. PLATE IS LOCATED IN ZONE 2-48, STN 520 TO STN 530, STRINGER 55LH.SDR AUS20020242Track · corroded(AUS) FORWARD CARGO TIEDOWN TRACK CORRODED.SDR AUS20020243Track · corroded(AUS) CARGO TRACK CORRODED. TRACK IS LOCATED IN ZONE 1-13 SECTION 43, STN 540 TO STN 600 WL 156, BL16.SDR CA020108001Tire · failed(CAN) A/C ON TAKEOFF CLIMB RADIOED MAINT CONTROL THAT ATC REPORTED TIRE DEBRIS ON RWY AFTER THEIR DEPARTURE: CREW ALSO REPORTED SEVERE WHEEL VIBRATION THROUGH AIRFRAME UPON ROTATION. A/C RETURNED ON SUSPICION OF TIRE FAILURE. FLY BY CONDUCTED WITH NO NOTABLESDR AUS20020110Structure · corroded(AUS) EXFOLIATION CORROSION FOUND AT NO3 CARGO DOOR UPPER FORWARD SIDEAT STN 1090, STRINGER 20R. FOUND DURING CPCP INSPECTION.SDR PCS2002F00004Fire Detector · false activationCAPTAIN REPORTED DURING CLIMB OUT, FIRE INDICATION IN AFT CARGO ILLUMINATED. CREW NOTED THE INDICATION OCCURRED AFTER SELECTING ON THE WING ANTI-ICING. AIRCRAFT RETURNED BACK WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED AFT CARGO COMPARTMENT PNEUMATIC DUCTSDR AUS20011461Nut · corroded(AUS) VERTICAL STIFFENER ANCHOR NUT ATTACHMENT POINT CORRODED BEYOND LIMITS.
Back to Pratt & Whitney JT8D-15