Pratt & Whitney JT8D-219
Service difficulty reports · 1,944
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 = 'JT8D219' 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 = 'JT8D219' 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 WX0A2017091873288Engine · failedRIGHT ENGINE LOW OIL PRESSURE MESSAGE. TEMP ROLLED BACK TO ZERO, EMERGENCY DECLARED. R & R THE NR 2 ENGINE.SDR DALA2017081006124Gcu · failedDURING SHORT FINAL, TOTAL ACFT ELECTRICAL FAILURE OCCURRED. LANDED ON EMERGENCY POWER. RAN QRH AND LEFT GENERATOR RESET. RIGHT GENERATOR VOLTS AND FREQUENCY READ ZERO. LEFT GCU HAS GCU FAULT. REPLACED LEFT AND RIGHT GCUS IAW AMM 24-20. RAN BOTH ENGINES AND SDR DALA2017080405961Transmitter · failedCREW DECLARED AN EMERGENCY DUE TO THE RIGHT ENGINE OIL PRESSURE READING HIGH. MAINTENANCE REPLACED THE OIL PRESSURE REGULATING VALVE, THE OIL PRESSURE TRANSMITTER, AND THE OIL PRESSURE TRANSMITTER CONNECTOR PLUG. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA2017072805726Connector · failedDIVERTED DUE TO NR 1 ENGINE OIL PRESSURE HIGH. NR 1 THROTTLE AT IDLE WITH OIL PRESSURE IN RANGE. MAINTENANCE REPLACED THE SYSTEMS DISPLAY PANEL, PLUG P1-813, OIL PRESSURE TRANSMITTER. TAKEOFF POWER RUNS CONFIRMED OIL PRESSURE NOW NORMAL.SDR DALA2017071905534Engine · making metalLEFT ENGINE OIL STRAINER CLOGGED. EMERGENCY DECLARED. CHIP DETECTOR CLEAN AND FILTER CHECKED GOOD. FOUND METAL IN OIL TANK AND REPLACED ENGINE.SDR WX0A201707143274Engine · unknown(EMERGENCY DECLARED) CPT SHUTDOWN #1 ENG DUE TO LARGE THROTTLE SPLIT BETWEEN ENG1 & ENG2.SDR WX0A2017070873271Engine · failed(EMERGENCY DECLARED) LT ENGINE FAILED AFTER LOUD BANG. R&R LT ENGINE.SDR DALA2017062805042Warning System · false activationDIV TO BHM DUE TO NO 2 ENGINE OIL STRAINER CLOGGED MESSAGE CAUSING ENGINE TO REMAIN AT IDLE. ENGINE WAS NOT SHUT DOWN. CONTRACT MAINTENANCE REMOVED FILTER AND CONFIRMED CLEAN. REMOVED FILTER AND FOUND CLEAN. REPLACED FILTER AND FORWARDED INDICATION TO MEL 79-0SDR DALA2017062104858Anti-Ice Valve · failedLEFT ENGINE ANTI-ICE VALVE CIRCUIT BREAKER TRIPPED WITH ODOR AND SMALL AMOUNT OF SMOKE. DISCONNECTED THE VALVES FROM B1-43, MEGGED WIRES FROM B1-43 TO PL809. ALL GOOD IAW WDM 75-11-00. REPLACED THE CIRCUIT BREAKER B1-43. FOUND COWL ANTI ICE VALVE BAD.SDR DALA2017052404150Duct · blownPERFORMED AN IFSD AND AN ATB, DUE TO A REPORTED FIRE WARNING ON THE NR 2 ENGINE. AFTER REDUCING THE THROTTLES, THE WARNING EXTINGUISHED. VIBRATIONS WERE REPORTED IN THE AFT CABIN. IAW QRH, THE NR 2 ENGINE WAS SHUTDOWN. THE NR 2 ENGINE FIRE BOTTLE WAS DISCHARGSDR DALA2017042503380Anti-Ice Valve · failedANTI-ICE VALVE RIGHT ENGINE LEFT CIRCUIT BREAKER FOUND TRIPPED ON ARRIVAL TO AIRCRAFT. WHEN RESET, CIRCUIT BREAKER SPARKED AND SMOKE CAME OUT. RT ENG LEFT ANTIICE VALVE LOCKED OPEN AND CONNECTER REMOVED AND STOWED. THE CIRCUIT BREAKER REMAINS IN. REMOVED FWDSDR AALA20170411002Connector · damagedCREW REPORTED LEFT HAND ENGINE OIL TEMP EXCEEDED LIMITS. CREW DECLARED EMERGENCY AND FOLLOWED QRH PROCEDURES BY SHUTTING DOWN THE LEFT ENGINE. THE FLIGHT RETURNED TO MSY WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME APPROXIMATELY 19 MINUTES. MAINTENANCE REMOVEDSDR WX0A2017031073238Bullet · damagedDURING CLIMB, THE LT ENGINE WAS NOT PRODUCING FULL POWER, CLIMB RATE WAS ABOUT 500 FPM. EMERGENCY DECLARED. R & R ENGINE NOSE BULLET AND PT2 FLEX LINE IN PYLON. (ORIGINAL SUBMISSION DATE: 03-31-2017)SDR DALA2017033002553Engine · vibrationAIRCRAFT LEVELED AT 370 AND POWER RETARDED, AIRCRAFT DEVELOPED A SMALL VIBRATION. VIBRATION FELT IN FLOOR AND YOKE AND WOULD CHANGE WITH POWER CHANGES. ALL PARAMETERS NORMAL. WHEN LEFT ENGINE WAS SHUT DOWN AT GATE AND DECELERATED VIBRATION GOT WORSE AND AIRSDR 2WAA2017032800001Engine · power lossAFTER T/O AT 2000FT LOST THRUST ON NR 2 ENGINE. NR 2 ENGINE SHUTDOWN IN ACCORDANCE WITH TO WAA POLICIES AND PROCEDURES.SDR WX0A073232Engine · failed(EMERGENCY DECLARED) ON APPROACH INTO DAY. AT 14000 FT & 280 KTS, PILOTS RECEIVED A SLAT OVERSPEED WARNING. THE PILOTS RAN A CHECK LIST AND SUDDENLY THE FIRE WARNING CAME UP FOR THE NR 2 ENGINE. THE CAPTAIN DEPLOYED 1ST FIRE BOTTLE AND AFTER 30 SECONDS THE 2NDSDR DALA2017031702180Indicator · missingRIGHT HYDRAULIC SYSTEM PRESSURE/QUANTITY LOSS REQUIRED USE OF ALTERNATE GEAR EXTEND PER QRH. MAINTENANCE FOUND THE RIGHT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE SIDE FILTER MODULE DIFFERENTIAL PRESSURE INDICATOR (DPI) MISSING. RETAINING SCREWS SHEARED FROM MODULSDR AALA201703099017Compressor · stalledAIRCRAFT WAS GROUNDED. COMPRESSOR STALL ON APPLICATION OF TAKEOFF POWER. ABORTED TAKEOFF BELOW 30 KNOTS. REMOVED AND REPLACED LEFT ENGINE. ACCOMPLISHED ENGINE RUN-UP IAW MCM 71-91-99. OPERATIONAL CHECK GOOD.SDR WX0A2017030673229Cone Bolt · not reportedDURING T/O ROLL FELT A ABRUBT JOLT IN A/C, REJECTED T/O AT 90 KNOTS. NOTICED NR 1 ENG INDICATIONS WERE NOT NORMAL. R&R FWD UPPER, LOWER CONE AND AFT CONE BOLTSDR DALA2017022301493Support · crackedCRACKED CONNECTOR SUPPORT ON FIRE LOOP AT FLANGE "J" BTW 6 TO 7 HRS POSITION, RT NACELLE. FIRE DETECTOR LOOP SUPPORT ASSY WAS REMOVED IAW AMM 26-10-04 AND REPLACED IAW AMM 26-10-04. TESTED IAW AMM 26-00-00-201.SDR DALA2017020801092Reservoir · defectiveAFTER TAKE-OFF BOTH LEFT AND RIGHT HYDRAULIC SYSTEMS FAILED. BOTH SYSTEMS CAME UP NORMAL ON DEPARTURE. AFTER RAISING THE LANDING GEAR AND TURNING OFF THE AUXILIARY AND TRANSFER HYDRAULIC PUMPS, BOTH SYSTEM PRESSURES REDUCED TO ZERO. QUANTITY LEVEL WAS 19L AND SDR DALA2016123010179Engine · malfunctionedDIVERTED TO TYS DUE TO NR 1 ENGINE ISSUES. ENGINE ROLLED BACK AND SHUT DOWN. MTC FOUND FUEL PUDDLED IN TURBINE SECTION. ENGINE REPLACED.SDR DALA2016102507565Blade · damagedRETURNED TO SGF DUE TO NR 1 ENGINE COMPRESSOR STALL WITH A REDUCED THRUST. CABIN CREW VERIFIED COMPRESSOR STALL AND CABIN ODOR. MTC FOUND FAN BLADE TIPS BENT FORWARD INDICATING ENGINE INGESTED SOFT FOD. MTC FOUND 2ND STAGE VANES PULLING FROM CASE. ENGINE WSDR DALA2016102507543Turbine · damagedRETURNED TO OKC DUE TO A RIGHT ENGINE FAILURE. THE CREW REPORTED THAT AT FL200 THE ENGINE FAILED WITH AN ASSOCIATED EGT RISE. THE QRH WAS FOLLOWED AND THE ENGINE WAS SHUT DOWN. MAINTENANCE FOUND TURBINE DAMAGE AND METAL IN THE TAILPIPE. THE ENGINE WAS REPLSDR DALA2016101907383P&D Valve · leakingFLT 0377 RETURNED TO ATL AFTER THE LT ENGINE FAILED AFTER TAKE-OFF. THE CREW REPORTED THAT ON CLIMB OUT THAT THE ENGINE ROLLED BACK AND SHUT DOWN. MAINTENANCE FOUND FUEL LEAKING AT THE P&D VALVE FLANGE. THE P&D VALVE WAS REPLACED. THE MAGNETIC CHIP DETECTOSDR DALA2016101007135Engine · making metalTHE NUMBER 2 ENGINE SHUTDOWN AT FL340 AND THE FLIGHT WAS DIVERTED. MAINTENANCE FOUND METAL ON THE CHIP DETECTOR. THE NUMBER 2 ENGINE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.SDR DALA2016092706900Turbine · damagedFLIGHT RETURNED TO DEPARTURE WITH A REPORTED ENGINE ISSUE. PILOT REPORTED BANG ON TAKEOFF. NR 1 ENGINE PARAMETERS DECLINED TO ZERO WITH EGT INCREASING. ENGINE SHUTDOWN. MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. ENGINE CHANGE COMPLETED.SDR DALA2016082806258Engine · failedAT TAKEOFF ROTATION, THE LEFT ENGINE FAILED. REPLACED THE NR 1 ENGINE IAW SPC 88-7110-9-0010.SDR DALA2016091406609Engine · failedRETURNED TO DEPARTURE WITH A REPORTED NR 1 ENGINE FAILURE. THE COMPRESSOR STALLED DURING CLIMB. THE CREW REPORTED THAT AFTER THE COMPRESSOR STALL, THE ENGINE PARAMETERS WERE NORMAL AT IDLE. THE AIRCRAFT RETURNED WITH THE NUMBER 1 ENGINE AT IDLE POWER. MAINTENSDR AALA20160731005Bearing · failedDURING FLIGHT THE LT ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. POWER REDUCED TO IDLE AND LIGHT REMAINED ILLUMINATED. ENGINE REMAINED AT IDLE THROUGH LANDING AND SHUT DOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. MAINTENANCE FOUND SDR WX0A2016072273178Relief Valve · failedEMERGENCY DECLARED, AFTER TAKEOFF, OIL PRESSURE CLIMBED ABOVE 55 PSI REACHING A PSI OF 80, FOLLOWED EMERGENCY QRH PROCEDURES. REPLACED NR 2 ENGINE OIL PRESSURE REGULATOR OPS AND LEAK CHECKS GOOD IAW MM 79-20-03-2-0. REMOVED & REPLACED NR 2 ENGINE OIL PRESSURSDR DALA2016062704947Attach Fitting · crackedCRACK AT INNER ATTACH FITTING ON RT ENGINE BULLET. STOP DRILL ACCOMPLISHED, CRACK WAS WELDED, WELDED AREA WAS BLENDED OUT AND STRESS RELIEVE WAS ACCOMPLISHED IAW ER/A 547807, REV ORIGINAL, FITTING WAS REMOVED AND REINTALLED IAW SRM 51-30-2.SDR AALA20160626004Compressor · stalledAIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL. DURING CLIMB THE NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. NR 2 ENGINE POWER REDUCED TO IDLE AND ACFT RETURNED TO FIELD. ENGINEERING REPORTS FAN BLADES WITH LEADING EDGE FOREIGSDR DALA2016062704946Nose Cowl · crackedCRACKED LT NOSE COWLING LIP INTERNAL STRUCTURE. SERVICEABLE NOSE COWL WAS INSTALLED IAW AMM 71-10-01-201.SDR DALA2016062104812Skin · crackedSEVERAL CRACKS ON OUTER SKIN OF THRUST REVERSER UPPER DOOR AT ENGINE NR 1. OUTER SKIN OF THRUST REVERSER WAS REPAIRED IAW AMM 78-30-07-801, FIG 803 AND SRM 51-10-3, PAR 14 AND 21.SDR DALA2016053104189Turbine · failedRETURNED TO DEPARTURE DUE TO A RT ENGINE TURBINE FAILURE DURING CLIMB AT AT 800-1000 FT. RT ENGINE WAS SHUTDOWN IFSD. CREW NOTED MAXIMUM EGT 800DEG. MAINTENANCE FOUND TURBINE DAMAGE AND AN ENGINE CHANGE WAS REQUIRED. ENGINE WAS REPLACED AND SUBSEQUENT CHECSDR DALA2016052704188Start Valve · malfunctionedFLT 1515 RETURNED TO DEPARTURE DUE TO RT ENGINE START VALVE SHOWING OPEN AND RT ENGINE OIL TEMP RISING. R & R START VALVE IAW AMM.SDR AALA20160521007Compressor Blade · damagedAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING ROTATION RT ENG EXPERIENCED COMPRESSOR STALL LIGHT ENG COMPRESSOR STALL AFTER TAKEOFF, ROUTED TO HANGAR TO COMPLETE 71-91-16. BORESCOPE INSPECTION FOUND DAMAGSDR AALA20160509008Anti-Ice Valve · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF THE NR 2 ENG HEAT VLV BEGAN FLASHING BLUE. TAKEOFF WAS ABORTED AT APPROX 80 KNOTS. R & R THE NR 2 ENG LT & RT ANTI-ICING VLVS & THE COWL ANTI-ICING VLV IAW AMM 75-10-0. ACCOMPLISHED OPERATIONAL & LEAK CHECK SYS. CHECKED SDR AALA20160509009Anti-Ice Valve · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF THE NR 2 ENG HEAT VLV BEGAN FLASHING BLUE. TAKEOFF WAS ABORTED AT APPROX 80 KNOTS. R & R THE NR 2 ENG LT & RT ANTI-ICING VLVS & THE COWL ANTI-ICING VLV IAW AMM 75-10-01. ACCOMPLISHED OPERATIONAL & LEAK CHECKS. SYSTEM CHESDR AALA20160509010Anti-Ice Valve · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF THE NR 2 ENG HEAT VLV BEGAN FLASHING BLUE. TAKEOFF WAS ABORTED AT APPROX 80 KNOTS. R & R THE 2 ENG LT & RT ANTI-ICING VLVS & THE COWL ANTI-ICING VLV IAW AMM 75-10-01. ACCOMPLISHED OPERATIONAL & LEAK CHECKS. SYS CHECKED SSDR DALA2016042003119Pump · failedRIGHT HYDRAULIC QTY DROPPED TO 2 QTS AND AFTER GEAR AND FLAPS WERE LOWERED QTY WENT TO 0 QTS. FOLLOWED BY PRESSURE DROPPING TO 0 PSI. REPLACED RT ENGINE DRIVEN HYD PUMP.SDR AALA20160418008Bullet · leakingAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER WAS DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB, OBSERVED AN EPR SPLIT BETWEEN NR 1 & 2 ENGS. FOUND PT2 LINE DISLODGED INSIDE OF BULLET ON NR 1 ENG. R & R BULLET IAW AMM 77-11-03. ACCOMPLISHED SDR AALA20160411015Warning System · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SOV IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONAL CHECKS SDR AALA20160518008Shutoff Valve · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL, THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SOV IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONAL CHECKESDR AALA20160518009Shutoff Valve · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SHUT OFF VLVS IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONSDR AALA20160518010Shutoff Valve · faultyAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL THE LT ENG ANTI-ICE LIGHT ILLUMINATED. TAKEOFF WAS ABORTED AT APPROX 70 KNOTS. R & R ALL 3 LT ENG ANTI-ICE AIR SHUT OFF VLVS IAW AMM 75-10-01. R & R LT ENG WARNING CIRCUIT ASSEMBLY IAW AMM 75-10-07. LEAK & OPERATIONSDR WX0A2016041273132Epr System · not reportedAT 6000 FT IN LEVEL FLIGHT, THROTTLES AT LOW LIM IDLE, ERP'S READ L 1.32, R 1.23. THIS CAUSES SPEED TO INCREASE TO APPROX 275 KTS WITH 250 KTS SELECTED. COMPLETED EPR SYS INDICATION TEST OF LT & RT ENGS IAW TC 77-071-002 & 77-072-002. NO DEFECTS NOTED. PERSDR AALA20160331005Connector · faultyAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB RT ENG OIL TEMPERATURE INCREASED TO 200 DEGREES. FOUND LOOSE WIRE & BACK SHELL ON CONNECTOR FOR TEMPERATURE SENSOR. REPLACED OIL TEMPERATURE CONNECTOR SDR WX0A2016040173121Sense Line · rupturedRIGHT ENG EPR READS UP TO 0.3 HIGH ERRATICALLY DURING FLIGHT. WITH HIGHER ALTITUDE CORRESPONDING TO GREATER DEVIATION. QRH 72.10 YIELDS NO HELP. FOUND NR 2 ENG PT2 LINE RUPTURED. R & R PT2 LINE IAW AMM 71-00-00-4-13B 40. LEAKED CHECKED SYS, FOUND SYS SATI
Back to Pratt & Whitney JT8D-219