Pratt & Whitney JT8D-9A
Service difficulty reports · 1,388
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 = 'JT8D9A' 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 = 'JT8D9A' 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 CA051101008Fitting · corroded(CAN) THE CORROSION TASK C53-107-01-01.7 IS INSPECTING THE CABIN SEAT TRACKS. THE CORROSION WAS FOUND ON THE UPPER DECK CARGO G NET FITTING P/N 65-62157-505. THE FOLLOWING INSPECTIONS OF THIS FITTING HAVE BEEN INCORPORATED IN THE MAINTENANCE PROGRAM 1) ADDITISDR CA051101009Hinge Fitting · corroded(CAN) NO CPCP CORROSION TASK COVERS THIS AREA, BUT DUE TO THE FINDINGS THE MAINTENANCEPROGRAM IS BEING AMENDED TO REDUCES THE CORROSION FINDINGS IN THIS AREA. THE CO RROSION WAS FOUND ON THE AFT AIRSTAIRS UPPER HINGE FITTING ON THE LOWER FOLDING SECTION. THE FSDR TSAA0575031Bleed Valve · defectiveON TAKE-OFF NR 2 ENGINE COMPRESSOR STALL ON INITIAL RUN-UP FROM IDLE. R & R NR 2 ENG PRBC IAW MM 75-31-11. BLEED VALVE SCHEDULING COMPLETED PER P&W MM 72-00-00. R.I.I. COMPLETED FOR NR 2 ENG PRBC VALVE CHANGE IAW MM 75-31-11. DID NOT FIX OFF IDLE STALL. LSDR TSAA0575029Bleed Valve · defectiveRUNNING UP ENGINES FOR TAKE-OFF, GOT STEADY BANGING. RPM BARELY PAST IDLE. FLIGHT ATTENDANTS GUESS THE NR 2 ENGINE. TAKE-OFF ABORTED. R&R PRBC IAW MM 75-31-11 OPS CHECK OK ON NR 2 ENGINE. BLEED VALVE SCHEDULING COMPLETED PER PWA MM 72-00-00. LUBED 8TH ANSDR C7WA0500109Line · looseAIR TURNBACK: ENGINE SHUTDOWN, NR 1 ENGINE OIL FILTER BYPASS LIGHT CAME ON AT 8000 FT, DURING CLIMB OUT. COMPLETED PRECAUTIONARY SHUTDOWN CHECKLIST. DURING INSPECTION OF NR 1 ENGINE, FOUND LOOSE LINE B-NUT AT OIL PRESSURE SWITCH. TIGHTENED B-NUT. OPERATIOSDR XN0A1245Engine · failedENGINE NR 2 WOULD NOT START. REMOVED AND REPLACED NR 2 ENGINE, OPS CK GOOD REF MM 74-11. (ORIG/CLOSED)SDR TSAA0526026Element · failedDURING PUSHBACK AND PRIOR TO ENGINE START, THE CREW NOTED NR 2 ENGINE OVERHEAT INDICATION ILLUMINATED. THE CREW COMPLETED THE ENGINE OVERHEAT AND ENGINE FIRE CHECK LISTS AND DISCHARGED BOTH ENGINE FIRE EXTINGUISHER BOTTLES. AFTER DISCHARGING THE BOTTLES, THESDR TSAA0526025Connector · dirtyON CLIMB BETWEEN 11,000 FT AND 13,00 FT, PILOTS REPORTED NR 2 ENGINE OVERHEAT LIGHT FLICKERING AND THEN BECOMING STEADY. THE ENGINE OVERHEAT CHECKLIST WAS COMPLETED AND LIGHT WAS EXTINGUISHED. ENGINE WAS NOT SHUTDOWN, EMERGENCY DECLARED, AND THE AIRCRAFT RETSDR 193Bulb · malfunctionedDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN, NR 1 ENGINE SHUTDOWN.SDR RYAN20050018Warning System · activatedDURING CLIMB, ENGINE NR 1 HAD HIGH OIL PRESSURE AND SHORTLY THEREAFTER NR 1 OIL TEMPERATURE STARTED CLIMBING TOWARDS REDLINE. ON RETURN NR 1 ENGINE WAS SHUTDOWN.SDR CA050617005Valve · stuck(CAN) DURING CLIMB OUT, THE CREW NOTICED THAT NR 2 ENGINE OIL TEMPERATURE WAS INCREASING. TEMP CONTINUED TO INCREASE DURING CLIMB AND ENGINE WAS SHUT DOWN. AIRCRAFT RETURNED TO BASE. INVESTIGATION FOUND THAT THE NR 2 ENGINE FUEL HEAT VALVE WAS STUCK IN THE OPSDR CA050614010Engine · failedDURING CLIMB AND AFTER DEPARTURE, NR 2 ENGINE HIGH OIL TEMP WAS EXPERIENCED. HIGH OIL TEMP SUP PROCEDURES ACCOMPLISHED, FOLLOWED BY THE ENGINE FAILURE/SHUTDOWN CHECKLIST. A/C RETURNED TO BASE. MAINTENANCE TROUBLESHOOTING FOUND 2 SNAGS. FUEL ANT-ICE VALVE P/NSDR 72300221Tee Fitting · corrodedCORROSION ON T-ANGLE.SDR 72300215Frame · corrodedA 2 X 2 INCH AREA OF CORROSION ON FRAME.SDR 72300214Stringer · corrodedA 1 X 14 INCH AREA OF CORROSION ON STRINGER.SDR 72300220Stringer · corrodedCORROSION ON STRINGER ANGLE.SDR 72300225Stiffener · corroded6 X 3 AREA OF CORROSION ON STIFFENERSDR 72300213Floorbeam · corrodedA 1 X 8 INCH AREA OF CORROSION ON FLOORBEAM.SDR 72300194Shear Tie · corrodedA 4 X 1 INCH AREA OF CORROSION ON SHEAR TIE.SDR 72300219Intercostal · corrodedCORROSION ON INTERCOSTAL REPLACEMENT.SDR 72300192Angle · corrodedA 3 X 2 INCH AREA OF CORROSION.SDR 72300193Shear Tie · corrodedA 6 X 1 INCH AREA OF CORROSION.SDR 72300187Structure · corrodedA 10 X 1 INCH AREA OF CORROSION.SDR 72300188Structure · corrodedA 1 X 1 INCH AREA OF CORROSION.SDR 72300189Structure · corrodedA 1 X 1 INCH AREA OF CORROSION.SDR 72300212Frame · corrodedA 1 X 2 INCH AREA OF CORROSION ON BULKHEAD FRAME.SDR 72300210Shear Tie · crackedA 1 INCH CRACK ON SHEAR TIE.SDR 72300211Shear Tie · crackedA 2.5 INCH CRACK ON SHEAR TIE.SDR 72300191Angle · corrodedA 1 X 2 INCH AREA OF CORROSION.SDR CA050510006Gcu · shorted(CAN) AFTER STARTING THE NR 1 ENGINE, THE CREW TURNED ON POWER FROM THE NR 1 ENGINE. THEY IMMEDIATELY NOTICED SMOKE COMING FROM THE GCU. THEY TURNED THE POWER OFF AND RETURNED TO GATE FOR MAINTENANCE. MAINTENANCE SWAPPED THE NR 1 GCU WITH THE APU GCU AND CARRSDR CA050509001Oven · smoke(CAN) DEPARTING, DURING CLIMB, SMOKE/HAZE WAS OBSERVED EMINATING FROM THE AFT CABIN AREA. THE AIRCRAFT DECLARED AN EMERGENCY AND RETURNED TO POINT OF DEPARTURE, LANDING WITH NO FURTHER INCIDENT. THE SOURCE OF THE SMOKE WAS DETERMINED TO BE THE CONTENTS OF A GSDR 72300177Stringer · cracked.5 INCH CRACK BETWEEN FASTENER HOLES IN STRINGER.SDR 72300182Frame · corrodedA 1 X 1 INCH AREA OF CORROSION ON FRAME.SDR 72300209Stringer · corrodedA 8 X 3 INCH AREA OF CORROSION ON STRINGER.SDR CA050504006Controller · inoperative(CAN) ON DEPARTURE, A/C WAS CLIMBING THROUGH FL210 WHEN THE CREW NOTICED THE CABIN DIFFERENTIAL WAS AT MAXIMUM AND THE CABIN RATE OF CLIMB WAS EXCEEDING 3000 FPM (UP). THEY IMMEDIATELY INITIATED A RAPID DESCENT AND STABILIZED THE CABIN ALTITUDE AT AN A/C ALTISDR 72300175Fitting · cracked.5 INCH CRACK ON STRINGER END FITTING.SDR 72300172Stringer · corrodedSEVERAL AREAS OF CORROSION ON STRINGER.SDR 72300207Stringer · corrodedA 8 X 2 INCH AREA OF CORROSION ON STRINGER.SDR 72300208Stringer · corrodedA 1 X 6 INCH AREA OF CORROSION ON STRINGER.SDR 72300171Shear Tie · corrodedA .75 X .75 INCH AREA OF CORROSION ON BOTTOM OF SHEAR TIE.SDR CA050425002Engine · leaking(CAN) AFTER T/O, SMOKE ACCUMULATED IN THE CABIN. THE FWD AND AFT SMOKE DETECTORS LOCATED IN THE LAVS ACTIVATED. SUCCESSFULLY RETURNED TO AIRPORT. MX CARRIED OUT ENG GROUND RUNS & COULD NOT DUPLICATE DEFECT ON GROUND. A TEST FLT ORDERED & AND IN FLT SMOKE PRSDR GAIA05020OPLight · inoperativeDURING PREFLIGHT, EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (K)SDR 72300186Fitting · crackedA 1 INCH CRACK ON STRINGER FITTING.SDR 72300205Stringer · corrodedA .75 X .5 INCH AREA OF CORROSION ON STRINGER.SDR 72300206Stringer · corrodedA 20 X 3 INCH AREA OF CORROSION ON STRINGER.SDR 72300178Stringer · corroded8 INCH BY 3 INCH AREA OF CORROSION ON STRINGER.SDR 72300179Stringer · corroded1 INCH BY 4 INCH AREA OF CORROSION ON BOTTOM OF STRINGER.SDR 72300167Floorbeam · corroded3 INCH BY .75 INCH AREA OF CORROSION ON FLOORBEAM UPPER CHORD.SDR 72300184Fitting · corrodedA 1 X 1.5 INCH AREA OF CORROSION ON FITTING.SDR 72300204Stringer · corrodedA 2 X 2 INCH AREA OF CORROSION ON STRINGER.
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