JASC 7200
Service difficulty reports · 14,730
Reports filed under 7200 · Engine (Turbine/Turboprop), newest first.
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 jasc_code = '7200' 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 jasc_code = '7200' 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 SWIA200211107Engine · overtempDURING TAKEOFF, LEFT ENGINE ITT WENT TO 907 DEGREES, FLASHING RED. ABORTED TAKEOFF. REMOVED AND REPLACED LEFT ENGINE IAW MM 71-00-00.SDR HEEA080639Elbow · leakingENGINE LINE ELBOW LEAKING. REPLACED WITH SERVICEABLE PART.SDR MEX2002247Engine · malfunctionedAIRCRAFT RETURNED TO PLATFORM DUE TO THE RT ENGINE DID NOT ACCELERATE AND ALSO IT HAD A LOW INDICATION OF N2. DURINE THE FAILURE VERIFICATION, THERE WERE OSCILATIONS IN THE INDICATIONS OF N2, EPR AND FUEL FLOW. ENGINE TOOK 20 SECONDS IN ACCELERATE. THE THROSDR SWIA200211093Engine · malfunctionedWHILE EN ROUTE FROM SAN TO LAX, NR 1 ENGINE TORQUE BEGAN TO SURGE AND AIRCRAFT BEGAN TO YAW BACK AND FORTH. FOLLOWED QRH AND SELECT EEC MANUAL PER QRH. FOUR TO FIVE MINUTES LATER NR 1 ENGINE BEGAN TO SURGE AGAIN WITH WIDER PARAMETER SWINGS. ELECTRONIC FUEL SDR UIA02005Engine · failedNR 2 ENGINE HAS AN IN FLIGHT SHUTDOWN, IAW QUICK REFERENCE HANDBOOK MADE AN EMERGENCY LANDING AT KHH. FOUND TRANSFER ACCESSORY GEARBOX TOWER SHAFT HAD FREE ROTATION DURING CHECK.THIS IS THE SECOND SIMILAR EVENT HAPPENING WITHIN A WEEK, THE ENGINE WAS REPAIREDSDR DL72W020883Engine · out of trimREJECTED TAKEOFF. AIRSPEED APPROX 130 KIAS LIGHT BRAKING. EVERYTHING ELSE NORMAL WITH ABORT. COULD NOT GET NORMAL POWER EPR OF 2.06 OUT OF NUMBER 1 ENGINE. N1 AND EGT NORMAL. FIRE DEPT INSPECTED BRAKES, CHECKED OK. REMOVED AND REPLACED EPR TRANSMITTER NRSDR CA020806008Engine · failed(CAN) WHEN ADDING THRUST FOR T/O, HEARD LOUD BANG AND NOTICED PARAMETERS DROPPING. SHUT DOWN AND SECURED NR 2 ENGINE. NR 2 ENGINE AND T/R REPLACED AS PER AMMSDR DL733020877Engine · overtempON TAKEOFF (NORMAL POWER) CLIMBOUT BOTH ENGINE INDICATIONS SHOWED RED LIGHT ILLUMINATED ON DIGITAL READOUT AT 970 DEGREES (C) PLUS ON BOTH ENGINES AT LEAST 5 SECONDS. N1 INDICATES AT ABOUT 96.6. PULLED BACK THROTTLES, RED LIGHT EXTINGUISHED. REMOVED AND REPSDR MALA020438Engine · power lossDURING FLIGHT 3392, EXPERIENCED ROLLBACK AT 21,000 FT. -11 DEGREES CELSIUS, 59 PERCENT TORQUE. IN ICING CONDITIONS NO SHIFT IN ITT OR TORQUE WAS NOTICED. IGNITION LIGHT DID NOT ILLUMINATE. CREW COULD NOT DETERMINE WHICH ENGINE HAS THE ROLLBACK BUT BELIEVE ISDR 02FDEA00523Engine · malfunctionedNR 3 ENGINE OIL TEMPERATURE WENT INTO YELLOW BAND APPROX 10 MINUTES AFTER T/O. STARTED 15 MINUTE TIMING & COMPLIED WITH RED TABS. WHEN THRUST LEVER WAS RETARDED TOWARDS IDLE, OIL TEMP WENT INTO RED BAND. RED TABS DIRECTED AND ENGINE SHUTDOWN. AFTER SHUTDOWSDR SWIA200211067Engine · malfunctionedRIGHT ENGINE AUTO FEATHERED ON THE TAKEOFF ROLL. ABORTED THE TAKEOFF. PERFORMED TWO TAKEOFF POWER RUNS, ALL CHECKS NORMAL.SDR 0202406717Engine · malfunctionedWHILE CLIMBING THROUGH FL280, THE NR 4 ENGINE FLAMED OUT FOLLOWED BY THE FIRE WARNING ACTIVATING FOR THE NR 4 ENGINE. COM PROCEDURES WERE FOLLOWED TO SECURE THE ENGINE AND BOTH FIRE BOTTLES WERE DISCHARGED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNEDSDR EIAA2002088Engine · stalledFLT 481 - PANC - WHILE CRUISING AT FL35.0, NR 1 ENGINE COMPRESSOR STALLED, N1 RPM DECREASED AND EGT INCREASED RETARDED THROTTLE NO RESPONSE, SHUTDOWN NR 1 ENGINE. DURING WINDMILLING ATTEMPTED RESTART, EGT OUT OF LIMITS, RETURN TO ANC. (M)SDR MALA020431Engine · malfunctionedDURING FLIGHT 2919, LT ENGINE AND ITT SPIKED TO 980 DEGREES. AIR RETURN TO MSP. MAINTENANCE REMOVED AND REPLACED LT ENGINE.SDR 02FDEA00514Engine · malfunctionedNR 2 ENGINE LOST OIL QUANTITY AND PRESSURE SHORTLY AFTER TAKEOFF, WITH CORRESPONDING LOW OIL PRESSURE/FILTER BYPASS LIGHT ON IN FRONT PANEL. SHUTDOWN ENGINE IAW CHECKLIST AND RETURNED FOR UNEVENTFUL LANDING. REPLACED NR 2 ENGINE. OPS AND LEAK CHECK OK.SDR UPS02438877Engine · malfunctionedINSPECTION TYPE:N/A, WHEN PACK LAND 3 WAS TURNED ON AFTER TAKEOFF OILY SMOKE FILLED THE FLIGHT DECK. PACK 1 AND 3 WAS TURNED OFF AND PACK 2 TURNED ON. SMOKE CLEARED AND FLIGHT CONTINUED TO PHL. REMOVED AND CLEANED NR 1 PACK COALESCER BAG. RAN PACKS FROM APSDR DLM90020837Engine · power lossLEFT ENGINE POWER ROLLED BACK AND EGT 625. CREW FOLLOWED POM AND SHUT ENGINE DOWN. REPLACED NR 1 ENG PER M/M.SDR RAIA00207220Gearshaft · sheared5625-STL- LEFT ENGINE FLAMED OUT DURING CLIMB, UN ABLE TO RESTART. MAINTENANCE FOUND INTERNAL GEAR SHAFT FAILED IN NOSE CASE. REMOVED AND REPLACED GEAR SHAFT OPS AND LK CK OK.SDR 2002UALA01192Engine · power lossPOWER LOSS IN NR 2 ENGINE. THE TEST ON THE FUEL CONTROL UNIT P/N 779100-5, S/N F22470 EXHIBITED SEVERAL PARAMETERS THAT WERE OUT-OF-LIMITS. HOWEVER NONE WERE DEEMED TO HAVE BEEN THE CAUSE OF THE ENGINE SURGE EXPERIENCED ON-WING. FURTHERMORE, THE TESTS FOUNDSDR 2002F00777Engine · surgesDURING THROTTLE MOVEMENT ENGINE PARAMETERS SURGED WITH EEC ENGAGED. WITH EEC NOT ENGAGED, ENGINE STILL SURGED, BUT NOT AS MUCH. ENGINE FLUCTUATED WITH EEC ON OR OFF. PERFORMED TEST 13 TAKEOFF POWER, ALL PARAMETERS ON BOTH ENGINES ARE NORMAL WITHIN LIMITS IAWSDR MALA020406Engine · failedDURING FLIGHT 3313 RT ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE. AIR RETURN TO DTW. NO OTHER INFORMATION IS AVAILABLE AT THIS TIME.SDR DLM90020823Engine · overtempON CLIMBOUT EGT ROSE PAST RED LINE AFTER THROTTLE RETARDED TO DECREASE EGT. ENG AUTO SHUTDOWN. REPLACED ENG DUE TO EGT EXCEEDANCE.SDR CA020726013Engine · failed(CAN) DURING WALKAROUND PILOTS NOTICED GRINDING NOISE COMING FROM LT ENGINE. MAINTENANCE WAS CALLED TO INVESTIGATE. GRINDING NOISE WAS COMING FROM POWER SECTION AREA. OIL FILTER WAS CHECKED AND FOUND TO BE CONTAMINATED WITH METAL CHIPS. ENGINE WAS REMOVED SDR AUS20020750Engine · failed(AUS) ENGINE PROBLEM. LIMITED INFORMATION PROVIDED.SDR RAIA00207215Engine · failedLEFT ENGINE OIL CONTAMINATION LIGHT ILLUMINATED. MAINTENANCE REMOVED AND REPLACED #1 ENGINE.SDR 00034Engine · flamed outAIRCRAFT EN ROUTE FROM ADDISON TX TO WINDSOR CANADA RT ENGINE FLAME-OUT CLIMBING FROM 390 TO 410. RESTART NORMAL, CLIMB BACK TO 410 AND CONTINUED TRIP. PILOT INSPECTED ENGINE FOR FOD DAMAGE AT DESTINATION, NO DAMAGE FOUND. AIRCRAFT MOVED TO MAINTENANCE BASESDR YENA200217Engine · malfunctionedFLT 88 ONT TO JFK, DIVERTED TO SLC DUE NR 1 ENGINE AUTO SHUTDOWN IN FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER AMM 71-00-20 AND OPS CHECK OK PER AMM 71-00-00.SDR CA020918008Engine · flamed out(CAN) DURING ROUTINE FLIGHT AFTER FUELING FROM A SUPPLIED SEALED DRUM OF PRE-MIXED JET FUEL (FSII) ADDED. THE ENGINE FLAMED OUT AND A FORCED LANDING RESULTING IN NO DAMAGE TO THE HELICOPTER.SDR S02172025Engine · failedNR 3 ENGINE A BANG DURING ROTATION, EGT PEAK 661 DEGREE C FOR SHORT TIME, THEN BACK TO NORMAL. EEC BITE NO FAULT MESSAGE FOUND. ENGINE INLET AND EXHAUST VISUALLY CHECKED NORMAL. BLEED VALVE SYS CHECKED NORMAL. BORESCOPE INSPECTION OF LP COMPRESSOR, HP COSDR 2002F00775Gasket · crackedFLIGHT NUMBER 214. 15 MINUTES AFTER CLIMB-OUT PASSING 18,000 FEET, RT ENGINE OVERHEAT EICAS MESSAGE AND RT STRUT OVERHEAT DET 1 STATUS MESSAGE ILLUMINATED. LIGHT EXTINGUISHED AFTER RT BLEED SWITCH WAS TURNED OFF AND THRUST LEVER RETARDED (AFTER 3 MINUTES). MAISDR CHQ000178Engine · malfunctionedRIGHT ENGINE NEEDS REMOVED AND REPLACED DUE TO OIL SMELL AND VAPOR IN COCKPIT. REMOVED AND REPLACED FUEL NOZZLES NO FIX. REMOVED AND REPLACED RT ENGINE ASSY.SDR AWXA200200596Engine · fireFLT 0279 - AFTER LANDING AT IAH INBOUND FROM PHX, AFTER ENGINE SHUTDOWN AT GATE, GROUND CREW OBSERVED FIRE IN THE TAILPIPE OF THE NR 1 ENGINE. FLIGHT CREW MOTORED ENGINE APPROXIMATELY 1 MINUTE BEFORE FLAME EXTINGUISHED, ESTIMATE TAILPIPE FIRE LASTED TOTAL OF 2SDR CA020726016Fadec · failed(CAN) WHILE EN ROUTE LT ENGINE SHUT ITSELF DOWN. AIRCRAFT CONTINUED TO DESTINATION AND MADE UNEVENTFUL SINGLE ENGINE LANDING. TROUBLESHOOTING ISOLATED FADEC ON LT ENGINE AS BEING DEFECTIVE. FADEC IS NOW BEING INVESTIGATED. TSN 3002.4 HRS FADEC 370.12 HRS ON LSDR CNMA200200004Engine · malfunctionedNR 2 ENGINE OR ACFT SHUTTERED, MADE A POP, THEN WENT QUIET. NR 2 ENGINE'S EGT WENT TO 945. REDUCED THROTTLE TO 740 N1 AND N2. CLIMBING TO 2100 FT EGT STABILIZED AROUND 915 - 925 AND OIL FILTER CLOG LIGHT CAME ON NR 2 ENGINE. SHUT DOWN NR 2 ENGINE. RETURNESDR GUU2002F00024Engine · damagedDURING OIL FILTER INSPECTION METAL FLAKES DISCOVERED. FURTHER INSPECTION OF THE RT ENGINE DETERMINED EXCESSIVE DISCOLORED (BLACK OIL). REPLACED THE RIGHT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR.SDR VNAA0207005Engine · surgesDURING TAKEOFF, THE RIGHT HAND ENGINE SURGED AND THE CREW RECEIVED A RIGHT HAND GENERATOR FAIL CAS MESSAGE. THE CREW ABORTED TAKEOFF. THE CREW THEN FOLLOWED THE QUICK REFERENCE HANDBOOK AND THE MESSAGE CLEARED. FLIGHT 4090 WAS THEN CLEARED FOR ANOTHER TAKEOSDR DL764020792Engine · vibrationFAILED VERIFICATION FLIGHT FROM FAN LUBE (BOTH ENGINES). LEFT ENGINE VIBES TO 4.3. PERFORMED AVM TRIM BALANCE. CHECKS GOOD.SDR AALA20020969Engine · failedIND - FLT 772 - EN ROUTE DFW-LGA - DURING CRUISE AT 37,000 FEET, RIGHT ENGINE FAILED. N2 SUDDENLY WENT TO ZERO AND OIL PRESSURE WENT TO ZERO. OIL QUANTITY WAS OVER 12 QUARTS. NO FIRE INDICATIONS. DIVERTED AND LANDED IND WITHOUT INCIDENT. REPLACED NR 2 ENGSDR 2002UALA01133Engine · power lossABORTED TAKEOFF AT 90-100 KNOTS DUE TO NR 1 ENGINE NOT PRODUCING ENOUGH THRUST.SDR MALA020388Engine · overtempLT ENGINE ITT WENT TO 930. INSPECTED ENGINE INLET AND FOUND DEBRIS THAT CAUSED BLOCKAGE. FOUND NO DAMAGE.SDR 2002UALA01114Engine · flamed outFLAME-OUT OF NUMBER 2 ENGINE. INADEQUATE FUEL SUPPLY PROVIDED TO NR 2 ENGINE. CONDUCTED EXTENSIVE ENGINE AND FUEL SYSTEM DIAGNOSTIC TESTING. DISCOVERED NO INDICATION OF MECHANICAL OR ELECTRONIC SYSTEM FAULTS. CAREFULLY TRACKED AIRPLANE OPERATION AFTER INCISDR CA020718011Engine · failed(CAN) AFTER TAKEOFF ON A SCHEDULED TRIP FROM THE FIRE CAMP, THE PILOT LEELLED THE AIRCRAFT AND REDUCED POWER TO NORMAL CRUISE POWER. AT THIS MOMENT HE HEARD A LOUD BANG AND FELT A PRONOUNCED YAW. THE NR 1 ENGINE OUT LIGHT ILLUMINATED AND ALL NR 1 ENGINE INSTRUSDR HEEA079925Engine · failedWHEN PLACED IN MANUAL, GOVERNOR ENGINE COMPRESSOR STALLED AT APPROXIMATELY 70 & N1 SPEED. FLAME CAME OUT OF EXHAUST STACK. ENGINE REMOVED FOR OVERTEMP INSPECTION. REPLACED WITH SERVICEABLE PART.SDR AWXA200200587Engine · malfunctionedFLT 0662 - AFTER BEING CLEARED FOR TAKEOFF AND RELEASING THE BRAKES BOTH ENGINES SPOOLED UP EVENLY. SELECTED THE TOGA BUTTON AND THE NR 1 ENGINE ACCELERATED NORMALLY, NR 2 ENGINE DID NOT RESPOND TO THRUST LEVER MOVEMENT. WAITED 2 TO 3 SECONDS FOR NR 2 ENGINESDR 2002UALA01075Engine · vibrationRETURNED TO ORD UNDER AMBER ALERT DUE TO NR 2 ENGINE VIBRATION.SDR C1HA200292007Engine · leakingDURING CLIMB THROUGH FL280 NR 2 ENGINE OIL TEMP INDICATED BEYOND REDLINE RADIAL. NR 2 ENGINE SHUTDOWN 2 GALLONS OF OIL LOST, OIL PRESSURE 5PSI DURING DESCENT. OIL TEMP BACK IN GREEN AND AFTER SHUTDOWN NR 2 ENGINE WINDMILLED FOR 21 MINUTES. REMOVED AND REPLACSDR 377PA0006EngineAt rotation had a loud engine vibration on Left engine. Inspected eng. intake, exhaust; opened cowlings & inspected; close cowlings; BITE AVM per MM77-31-00. Eng. Insp. per MM71-00-47. Ran eng. Parameters & fan blade damage within limits.SDR GLBA200287Engine · overtempLEFT HAND ENGINE OVER TEMPED ON TAKEOFF.SDR SWAA021404Engine · malfunctionedINFLIGHT SHUT DOWN, DIVERSION, DURING CRUISE NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED, LIGHT REMAINED ON EVEN AT IDLE. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR CA020626016Engine · failed(CAN) WHILE PERFORMING THE 5TH TOUCH AND GO DURING A TRAINING FLIGHT, THE AIRCRAFT PULLED TO THE LT AS ENGINE POWER WAS INCREASED TO TAKEOFF. THE CREW APPLIED RT RUDDER TO CENTER THE AIRCRAFT. THE CO-PILOT NOTED N1 ON THE LT ENGINE TO BE APPROX. 1-3 PERCENT AN
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