Pratt & Whitney JT8D-7B
Service difficulty reports · 753
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 = 'JT8D7B' 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 = 'JT8D7B' 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 GAIA04114Skin · dentedDURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT STA 1055 ABOVE STR 20R. REF FASI NR 86520, ACCOMPLISHED DOUBLER REPAIR IAW WITH SRM 53-30-3, FIG 13.SDR GAIA04115Skin · dentedDURING C-CHECK INSPECTION, FOUND CREASE IN C3 DOOR SKIN AFT EDGE AT STR 21 RT. REF FASI NR 86522, INSTALL DOUBLER REPAIR IAW B727 52-00-3, FIG 3.SDR GAIA04116Skin · dentedDURING C-CHECK INSPECTION, FOUND CREASE IN C-3 DOOR SKIN AFT EDGE AT STR 22, RT. REF FASI NR 86524, CUT OUT DAMAGE AREA DIM 1.50 X 1.25 INSTALL DOUBLER REPAIR IAW SRM 52-003, FIG 3.SDR GAIA04117Skin · crackedDURING C-CHECK INSPECTION FOUND FUSE SKIN CRACKED BS 360, STR 5, LT. REF FASI NR 86545, CUT OUT DAMAGE AREA DIM 2.50 X 1.0 INSTALL DOUBLER REPAIR IAW SRM 53-30-3, FIG 3A.SDR GAIA04118Angle · crackedDURING C-CHECK INSPECTION FOUND RT WING L/E FWD STA 130 OB CHORD ANGLE CRACK. REF FASI NR 86591, STOP DRILLED CRACK AREA AND INSTALL ANGLE REPAIR IAW SRM 57-20-2, FIG 1.SDR GAIA04119Support Angle · crackedDURING C-CHECK INSPECTION FOUND PANEL SUPPORT ANGLE CRACK, RT WING L/E STA 130. REF FASI NR REMOVED, FABRICATED AND REINSTALLED PANEL SUPPORT ANGLE IAW SRM 57-20-2, FIG 1.SDR GAIA04120Panel · crackedDURING C-CHECK INSPECTION, FOUND RT WING L/E STA 349 WEB PANEL CRACKED. REF FASI NR 86603, STOP DRILLED WEB AREA AND INSTALLED DOUBLER REPAIR IAW SRM 51-40-2, FIG 1.SDR GAIA04121Skin · crackedDURING C-CHECK INSPECTION FOUND NR 5 SLAT L/E LOWER TO OB END PREVIOUS REPAIR MISS MATCH. REF FASI NR 86609, REMOVED PREVIOUS REPAIR FROM NR 5 SLAT. INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 1.SDR GAIA04122Rib · crackedDURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86613 REMOVED AND REPLACED NR 6 SLAT INTERIOR RIB IAW SRM 57-50-2.SDR GAIA04123Rib · crackedDURING C-CHECK INSPECTION FOUND NR 6 SLAT INTERIOR RIB CRACKED. REF FASI NR 86614, REMOVED AND REPLACED NR 6 SLAT INTERIOR RIB IAW SRM 57-50-2.SDR GAIA04124Support · crackedDURING C-CHECK INSPECTION FOUND RT WING FRONT SPAR WS 726, NR 8 SLAT ACTUATOR OB PLATE TRUNNION SUPPORT CRACKED. REF FASI NR 86620, REMOVED AND REPLACED NR 8 SLAT SUPPORT PLATES IAW SB 57-0130, REV 3.SDR GAIA04125Skin · crackedDURING C-CHECK INSPECTION FOUND EXISTING FUSELAGE SKIN REPAIR DOUBLER AT STA 410 AND STR 21 RT HAS TOOLING SET MARKS AND DOES NOT COMPLY WITH SRM 53-30-3, FIG 3. REF FASI NR 86628, CUT OUT DAMAGED AREA DIM 13.75 X 10.75. INSTALLED DOUBLER REPAIR IAW SRM 53-3SDR GAIA04126Frame · dentedDURING C-CHECK INSPECTION FOUND DENT IN FUSELAGE FRAME AT STA 1090, STR 25 LT. REF FASI NR 86673, CUT OUT DAMAGED AREA DIM 1.125 X 1.0 INSTALLED SPLICE IAW SRM 51-40-3, FIG 1.SDR GAIA04127Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 380 DENTED ABOVE STR 7 LT. REF FASI NR 86676, CUT OUT DAMAGED AREA, DIM 1.0 X 3.0 INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1.SDR GAIA04128Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 400 DENTED ABOVE STR 8, LT. REF FASI NR 86677, CUT OUT DAMAGED AREA DIM 1.0 X 3.50, INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1.SDR GAIA04129Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 380 DENTED ABOVE STR 7 AND 6 RT. REF FASI NR 86678 CUT OUT DAMAGED AREA DIM 1.0 X 3.50 AND 1.0 X 3.0. INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG 1.SDR GAIA04130Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BA 400 ABOVE STR 7 AND 6 RT DENTED. REF FASI NR 86679, CUT OUT DAMAGED AREA DIM 1.0 X 2.125 AND 1.0 X 4.0. INSTALLED ANGLE REPAIR IAW SRM 53-10-4, FIG.SDR GAIA04131Frame · dentedDURING C-CHECK INSPECTION FUND MAIN CABIN FRAME AT BS 500 ABOVE STR 17 RT DENTED. REF FASI NR 86680, CUT OUT DAMAGED AREA DIM 1.0 X 2.0. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04132Frame · dentedDURING C-CHECK INSPECTION, FOUND MAIN CABIN FRAME AT BS 520, ABOVE STR 17 RT, DENTED. REF FASI NR 86681, CUT OUT DAMAGED AREA DIM 1.0 X 2.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04133Frame · dentedDURING C-CHECK INSPECTION, FOUND BS540 FRAME WITH DENTS INTO THE RADIUS. REF FASI NR 86682, ACCOMPLISHED ANGLE REPAIR IAW SRM 51-40-9, FIG 1.SDR GAIA04135Frame · dentedDURING C-CHECK INSPECTION, FOUND MAIN CABIN FRAME AT BS580 ABOVE STR17,STR16 RT, DENTED. REF FASI NR 86684, CUT OUT DAMAGE AREA DIM 1.0 X 6.0, INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04136Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 600 ABOVE STR 17 RT, DENTED. REF FASI NR 86685, CUT OUT DAMAGED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04137Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME BS 640 ABOVE STR 17, STR 16, RT DENTED. REF FASI NR 86686 CUT OUT DAMAGED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04138Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 660 ABOVE STR17,16 RT, DENTED. REF FASI NR 86687, CUT OUT DAMAGED AREA DIM 1.0 X 2.25 AND 1.0 X 2.25. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04139Skin · crackedDURING C-CHECK INSPECTION FOUND LT WING L/E CAVITY WS110-130 FWD. SKIN BUCKLED AND CRACKED. REF FASI NR 86706, STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 12.SDR CA040910005Turbine Blades · damaged(CAN) AFTER TAKEOFF POWER WAS SET A LOUD BANG AND VIBRATION WAS EXPERIENCED FROM THE NR 1 ENGINE. TAKEOFF REJECTED. ENGINE SECURED AND AIRCRAFT RETURNED TO RAMP. VISUALINSPECTION UP TAILPIPE REVEALED ENGINE HAD FAILED INTERNALLY. TURBINE BLADES MISSING.SDR C7WA200400041Transmitter · frozenEXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSMITTER FROZEN. REMOVED AND REPLACED TRANSMITTER AND REPAIRED WIRES AT D224 IB FLAP INDICATOR CONNECTOR OPERATIONAL CHECK GOOD IAW MM.SDR C7WA2004000BBAccessory Unit · inoperativeRED LT GEAR, RT GEAR, NOSE GEAR AND AMBER TAIL SKID LIGHTS ON PILOTS FRONT PANEL REMAINED ILLUMINATED AFTER GEAR HANDLE WAS RAISED ON TAKEOFF. FLIGHT ENGINEERS ANNUNCIATOR LIGHTS REMAINED OUT. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX IAW MM. OPS CHECSDR C7WA2004000CCDuct · brokenAFTER TAKEOFF NR 3 ENGINE FIRE WARNING WENT OFF. EMERGENCY CHECK LIST ACCOMPLISHED. WHEN NR 3 THROTTLE WAS RETARDED FIRE WARNING LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND NR 3 ENGINE ANTI-ICE DUCT BROKEN. REMOVED AND REPLACED NR3 ENGINE ANTI-ICE DUCT IAWSDR C7WA2004000AASwitch · inoperativeENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ASSOCIATED EMERGENCY PROCEDURE IAW AOM. LIGHTS STAYED ON UNTIL ENGINE SHUTDOWN ON THE GROUND. REMOVED AND REPLACED NSDR NACA20040026Filter · carbonedNR 3 ENGINE SHUT DOWN DUE TO LOW OIL PRESSURE/BYPASS LIGHT ILLUMINATED ON CLIMBOUT. REMOVED NR 3 ENGINE OIL SCREEN, INSPECTED AND FOUND CARBON ON FILTER. REPLACED FILTER WITH NEW. OP AND LEAK CHECK GOOD.SDR 04FDEA02186Seat Track · damagedCORROSION SEAT TRACK BS 870, LBL 45, WL 208. REMOVED CORROSION ON SEAT TRACK STA 870 LBL 45, WL 208. REMOVED .040, 1 INCH X 1 INCH FROM .080. OUT OF LIMITS. REMOVED DAMAGED SEAT TRACK, LOCATED AND DRILLED, ALODINED AND PRIMED NEW SEAT TRACK, INSTALLED NEW SEASDR CA040520002Control Cable · broken(CAN) MAINTENANCE FOUND THE WSB2 CABLE BROKEN WHEN INVESTIGATING A REPORT OF SPOILER FLOAT. THE CABLE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA040513006Flap Track · contaminated(CAN) DEPARTING, THE CREW OBSERVED A DIAGEEMENT BETWEEN IB AND OB FLAP POSITION. THE AIRCRAFT CONTINUED TO YFB BYPASSING YSR. MAINTENANCE IN YFB FOUND SIGNIFICANT CONTAMINATION DUE TO POOR RUNWAY CONDITION AT YRB (SLUSH AND MUD) AND SUSPECT FLAP SYSTEM FOULED SDR NACA20040019Gasket · wornNR 1 ENGINE STRUT OVERHEAT LITE CAME ON DURING CLIMB. RETARDED THROTTLES AND LITE WENT OUT. RE-APPLIED CLIMB POWER AND LITE CAME BACK ON. REPLACED WING ANTI-ICE HIGH PRESSURE SHUT-OFF VALVE GASKETS. CHECKED GOOD.SDR NACA20040016Line · looseNR 2 ENGINE SHUT DOWN DUE TO OIL QUANTITY AND PRESSURE WENT TO ZERO. FOUND NR 2 ENGINE OIL PRESSURE TRANSMITTER PRESSURE LINE LOOSE. REMOVED AND INSPECTED LINE, NO DEFECTS FOUND. RE-INSTALLED PRESSURE LINE. LEAK & OP CHECKED GOOD.SDR CA040409002Switch · malfunctioned(CAN) ON CLIMB OUT NR 5 KREUGER FLAP INTRANSIT LIGHT ILLUMINATED. A/C RETURNED ANC. SWITCH REPLACED AND OVERWEIGHT LANDING INSPECTION C/W.SDR 2004FA0000309Turbine Wheel · wornT-1 DISC RUB ON INNER TURBINE NOZZLE CASE SEAL. SEAL COMPLETELY RUBBED OFF.SDR CA040325002Actuator · leaking(CAN) ON APPROACH INTO CYVR SELECTED FLAPS 2, AMBER IN-TRANSIT LIGHT STAYED ON. NR 7 SLAT DID NOT EXTEND. HYDRAULIC SYSTEM (A) LOW PRESSURE LIGHTS ILLUMINATED AND HYDRAULIC (A) SYSTEM QUANTITY INDICATED ZERO QUANTITY. AIRCRAFT WAS VECTORED AND CREW PERFORMED HSDR MWEA040024Engine · vibrationLEFT ENGINE VIBRATION. COMPLIED WITH VIBRATON TEST, INLET HAS A VIBRATION OF 1.0 MILS, TEST 1 VIBRATION CHECKED OK FOR SERVICE.SDR NACA20040013Fitting · leakingNR 2 ENGINE SHUT DOWN DUE TO LOSS OF OIL PRESSURE AND OIL QUANTITY. REPLACED NR 2 ENGINE OIL LINE FITTING AT LT SIDE OF GEARBOX. INSPECTED NR 2 ENGINE CHIP DETECTORS AND MAIN OIL SCREEN. OP AND LEAK CHECK GOOD.SDR C7WA200400039Hydraulic Line · chafedAT FLIGHT LEVEL 20.0 A-SYSTEM QUANTITY AND PRESSURE WENT TO ZERO. REPLACED CHAFED HYDRAULIC HOSE AT NR 2 ENGINE DRIVEN HYDRAULIC PUMP OPERATIONAL AND LEAK CHECK NORMAL.SDR ROSS0401Switch · intermittentUPON EXTENDING GEAR, NOSE GEAR DOWN LIGHTS DID NOT ILLUMINATE, OTHER SWITCHING STUCK IN AIR MODE. NOTE: NO NOSE UNSAFE LIGHT ILLUMINATED, AFTER LANDING TAPPED ON NOSE GEAR DOWNLOCK SWITCH LIGHTS CAME ON. REMOVED AND REPLACED SWITCH AS PER DC9 MM CH 32-60-00 SDR NACA20040008Duct · crackedNR 3 ENGINE FIRE WARNING LIGHT ON APPROACH. RETARDED THROTTLE AND LIGHT WENT OUT. FOUND 13TH STAGE BLEED DUCT CRACKED IN HALF AT COWL ANTI-ICE VALVE. REPLACED DUCT. FOUND 8TH STAGE CHECK VALVE LEAKING, AND 8TH STAGE DUCT IN STUB WING LEAKING. REPLACED DSDR CA040113007Hinge · cracked(CAN) DURING SERVICE CHECK, FOUR CRACKS WERE FOUND ON THE NR 7 GROUND SPOILER SUPPORT HINGE. HINGE REPLACED WITH NEW PART. ALL HINGES INSPECTED FOR CRACKS, NO FAULTS FOUND.SDR CA040109004Fire Detector · malfunctioned(CAN) ON APPROACH, THE ENGINE FIRE WARNING BELL SOUNDED CONTINUOUSLY, THERE WERE NO ENGINE WARNING LIGHTS ON. ON THE GROUND MAINTENANCE INSPECTED ALL ENGINES NO FAULTS WERE FOUND. MAINTENANCE WAS UNABLE TO DUPLICATE PROBLEM AGAIN ON THE GROUND. THE FIRE DETECSDR NACA20030126Fire Loop · out of adjustNR 3 ENGINE FIRE DETECTOR LIGHT ON IN FLIGHT. ADJUSTED NR 3 ENGINE FIRE LOOP AWAY FROM COWLING, LIGHT EXTINGUISHED. FIRE LOOP WAS REPLACED ON PREVIOUS LOG SHEET/FLIGHT. CHECKED GOOD.SDR 2004F00034Helicoil · damagedDURING CRUISE, ENGINE NR 3 LOST ALL OIL PRESSURE AND ALL OIL QUANTITY. PERFORMED NR 3 ENGINE INFLIGHT SHUTDOWN CHECKLIST. DIVERTED TO STL. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED HELICOIL AT OIL FILTER BYPASS UNISDR CA031118011Rib · cracked(CAN) DURING ACCOMPLISHMENT OF AD 2002-12-13 AND ENGINEERING ORDER 7-5510-7-5001PT1 INSPECTION OF THE ELEVATOR HINGE SUPPORT RIBS FOR CRACKS IN THE FLANGES ON AIRCRAFT WITH KNOWN 7079-T6 MATERIALS. A CRACK WAS FOUND IN A NON-TYPICAL AREA NOT COVERED BY THE ADSDR DHL2003726012Engine · failedDURING T/O FROM ATL, ENGINE NR 2 EGT CLIMBED TO 620 C WITH EPR SET AT 1.95, N1 = 94 PERCENT, REDUCED THRUST TO 1.72 EPR, N1 = 89.5, EGT = 580 C, N2 = 92.8, FF = 6800, PERFORMED EGT OVER TEMPERATURE ABNORMAL PROCEDURE IAW 727 A.O.M. SHUTDOWN NR 2 ENGINE. ENGINE
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