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 GTIA010864Engine · leakingDTW - FLT 1691 - F/A'S REPORTED SMOKE IN CABIN, FOLLOWED QRH, LANDED AT 128,000 NR TURNED OFF L PACK. SMOKE PERSISTED. TURNED LEFT AND RETURNED OFF LATER TURNED OFF NI SMOKE. FOUND OIL IN 13TH STAGE DUCT REPLACED NR 2 ENGINE. (M)SDR DLM88011475Engine · failedAT 10 - 15 MIN AFTER T/O AT 14,000 FT HAD AN AIRFRAME VIB. CLIMBED TO 20,000 FT AND THE OIL CLOG LIGHT CAME ON WITH HARD KNOCKING ON THE FLOORBOARD OF COCKPIT. PULLED POWER BACK BUT CLOG LIGHT STAYED ON. SHUTDOWN THE ENG, HAD POSITIVE OIL PRESSURE THROUGHOSDR DLM88011472Engine · making metalLEFT ENG OIL STRAINER CLOG MSG IN FLIGHT PROCEEDED BY VIBRATION IN AIRCRAFT. SHUTDOWN ENGINE PER POM. ALL ENGINE INDICATIONS WERE NORMAL FOR CLIMB POWER. FOUND METAL IN ENG OIL FILTER. REPLACED ENGINE.SDR 01FDEA00795Engine · shutdownINFLT SHUTDOWN OF NR 2 ENG IN DESCENT THROTTLES RETARDED.SDR GXPA0119Tube · faultyNR 1 ENGINE MAKING 1-44 EPR. MAXIMUM NEEDED 1-54 FOR TAKEOFF. EGT WAS 690 DEGREES. REPLACED SHORT TUBE ON ENGINE TO AIRFRAME. OPS CHECKED GOOD AT OUTSIDE TEMPERATURE 21 DEGREES. CALL FOR 1-54 EPR, MAKES 1-59 EPR.SDR DLM88011461Engine · making metalLEFT OIL STRAINER CLOGGED MESSAGE CAME ON 1 HR INTO FLT. ENGINE SHUTDOWN. FOUND METAL ON CHIP DETECTOR AND MAIN OIL FILTER. REPLACED ENGINE.SDR DL738011423Engine · failedLEFT ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED ON FINAL APPROACH. THROTTLE WAS PULLED TO IDLE, LIGHT DID NOT GO OUT, ENGINE WAS SHUT DOWN. OIL QUANTITY WAS 0, PRESS WAS 1 PSI. NR 1 ENGINE CHANGED.SDR 2001F00268Engine · failedAT FLT 310, NR 2 ENGINE FAILED. PROCEEDING FAILURE CREW COULD SMELL OIL SMELL, THEN ENGINE QUIT. N2 WENT TO ZERO ALSO ZERO OIL PRESSURE. N1 APPROXIMATELY 22 PERCENT. A/C DIVERTED TO BKK. (M)SDR C2XA01TY102Engine · malfunctionedAVL FLIGHT 3664. CREW REPORTED THAT THEY RECEIVED ENGINE NR 2 ATTCS NO MARGIN MESSAGE ON TAKE-OFF ROLL. MAINTENANCE INSPECTED THE ENGINE AND AFTER SEVERAL ATTEMPTS TO CORRECT THE DISCREPANCY THE AIRCRAFT WAS FERRIED TO TYS. THE RIGHT HAND ENGINE WAS REMOVESDR 2001F00605Bearing · failedENGINE MAKING METAL. BEARING FAILED. (M)SDR ALG2001F00025Engine · making metalDURING RUN UP NR 2 ENGINE CHIP LIGHT ILLUMINATED. METAL SAW FOUND IN OIL SYSTEM CHIP PLUGS. ENGINE WAS REMOVED AND REPLACE.SDR 2001UALA01981Check Valve · leakingACARS DISPLAYED A STRUT OVERHEAT LIGHT ON NUMBER 1 ENGINE. *S/D* FOUND SENSE LINE LEAKAGE AT 6TH STAGE CHECK VALVE. REPLACED AND WRENCHED CHECKED LINES. OPERATIONS CHECK NORMAL.SDR MWEA011144Engine · overtempON TAKE OFF LEFT ENGINE REACHED 605-610 DEGREES CELSIUS AFTER V1, ABOUT 40 SECONDS AFTER TAKE OFF POWER WAS REDUCED TO BRING TEMP BACK TO 590 DEGREES CELSIUS AT A NORMAL CLIMB, POWER SETTING ENGINE TEMP WAS 545 DEGREES CELSIUS MCI TEMP 37 DEGREES CELSIUS EPR 1SDR AC2A075840Engine · damagedDURING A DAILY SERVICEABILITY CHECK THE NR 2 ENGINE WAS FOUND TO BE DAMAGED. SUSPECT CAUSE OF DAMAGE WAS THE FAILURE OF CAMLOC BLADE ASSY P/N: 40G2-1. THE ENGINE WAS DISASSEMBLED . THE COMPRESSOR WAS REMOVED AND DISASSEMBLED, THE TURBINE ASSY REMOVED. THSDR HEEA075551Solenoid · stuckSTUCK OPEN CAUSING HIGH T.O.T. REPLACED WITH SERVICEABLE PART.SDR NACA20010030Engine · power lossDISCRPANCY: Power loss #1 engine @ T.O. power @ 95 kts. BMEP & M.P. massive drop.CORRECTIVE ACTION: Performed engine run to field barometric and T.O. power settings multiple times. All parameters found to be satisfactory per NAC DC-6 Ops manual.SDR 2001F00501Engine · failedAPPARENT CATASTROPHIC FAILURE OF ENGINE WHILE ON DESCENT TO LAND RESULTING IN ENGINE SHUTDOWN. (M)SDR MALA010657Engine · failedRT ENGINE INFLIGHT SHUTDOWN. CREW HEARD LOUD POPPING SOUND FROM RT ENGINE DURING CLIMBOUT. REDUCED POWER TO 20-30 PERCENT ITT CONTINUED TO INCREASE, BUT OVERTEMP LIGHT PROCEEDED TO ACCOMPLISH ENGINE SHUTDOWN. MAINTENANCE COMPLETED WORK PACKAGE DATED 8/18/01SDR CHQ00019Engine · fluctuatesLEFT ENGINE FLUCTUATIONS.SDR SABA010041Engine · malfunctionedAIRCRAFT 961 ON FLIGHT 5121 CLT TO HKY. DURING TAKEOFF ROLL THE LEFT ENGINE WOULD NOT DEVELOP MORE THAN 60 PERCENT TORQUE. TAKEOFF WAS ABORTED. NO EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO THE GATE WITH NO OTHER PROBLEMS. MAINTENANCE PERFORMED GROUND RSDR ARWA0010809Engine · vibrationNR 2 ENGINE VIBRATION SPIKED AT 2.8 SHUT DOWN ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT.SDR ABXA010447Engine · vibrationCLIMB READING WAS 2.7, CRUISE READING WAS 1.3, ENGINE PARAMETERS NORMAL. OTHER INDICATION WAS AUDIBLE NOISE AND VIBRATION FOLLOWING THRUST CHANGE. CLEANED AND INSPECTED HOLD OPEN RODS FOR FAN COWL IAW B767 MM 77-11-10-2. VIBRATION LEVELS WERE FOUND TO BE WISDR CA010921007Engine · failed(CAN) ENROUTE FROM YVR TO YYC EXPERIENCED COMPRESSOR STALL ON NR 1 ENGINE. UPON ESTABLISHING CRUISE POWER SETTNG, CREW HEARD LOUD POP, FOLLOWED 20 SEC LATER BY ANOTHER POP (SEVERE COMPRESSOR STALL) & ASSOCIATED NR 1 ENGINE PRESSURE RATIO (EPR), N1 POWER SURSDR AWXA0002166Engine · failedDEN - IN FLIGHT SHUTDOWN / UNSCHEDULED LANDING - FLT 534 - ORIG OPEN - EN ROUTE FROM PHX TO CLE THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL AND WENT TO IDLE, UPPER ECAM DISPLAYED ENG OIL FILTER (1) AND WAS SHUT DOWN. THE FLIGHT WAS DIVERTED TO DEN AND ON DSDR SWIA200110107Engine · malfunctionedRIGHT ENGINE WOULD NOT POWER UP FOR TAKEOFF. RAN BOTH ENGINES THROUGH ALL PARAMETERS WITH EEC'S ON AND ALSO WITH EEC'S OFF. NO FAULTS NOTED. OPS CHECK GOOD.SDR SWIA200110113Engine · malfunctionedON APPROACH, LEFT ENGINE EXPERIENCED A SEVERE POWER LOSS. TRIPLE CHIME ''ENGINE CONTROL'' AND WHITE ''MANUAL'' LIGHT ILLUMINATED. INITIATED A GO-AROUND TO AVOID TERRAIN CONTACT. ON GO-AROUND, REGAINED SOME POWER ON LEFT ENGINE. BROUGHT POWER BACK TO LEVELSDR 2001F00565Engine · flamed outDURING POWER ASSURANCE CHECK, AT 1000 FEET AGL NR 1 ENGINE WAS PULLED OFFLINE. JUST POWER TO IDLE DETENT. NR 1 ENGINE FLAMED OUT. ATTEMPTED AIR START, ENGINE WOULD NOT START. AIRCRAFT WAS LANDED SINGLE ENGINE. AFTER THE LANDING, THE ENGINE WAS STARTED WISDR S01271023Engine · malfunctionedB18771 NR 2 ENGINE SPOOL DOWN AT LEVEL 39000 FT N DRIFT DOWN TO 35000 FT N RESTART SUCCESSFULLY BEFORE RESTART N1 31 N N2 24.55 OIL PRESS AS NML RESTART IS 30000 FT. C/A:1. NR 2 ENGINE CHECK IAW FIM 71-01-00 PG 8 N 209 ALL NML. 2.ENG INLET N EXHAUST CK NML.SDR RAIA00108016Engine · power loss5360-BWI-LEFT ENGINE DID NOT ACHIEVE TARGET TORQUE DURING TAKEOFF, CREW ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE LEFT ENGINE.SDR DL757011314Engine · malfunctionedRT ENG SEC CONTROL STATUS MSG THEN AFTER LEVEL OFF RT ENG STATOR CAUTION MSG, ENG SHUTDOWN. C/A REPLACED ENGINE, FCU, &EEC PER MM,PERFORMED TEST 7 14 AND 15 FROM PFHB. OPS CHKD AND LEAK CHKD OKSDR 2001F00283Engine · malfunctionedWHILE ON DESCENT TO KLRD FROM MMQT, WHILE PASSING FL180 A SMALL REDUCTION IN POWER WAS MADE. THE NR 1 ENGINE ROLLED BACK. AFTER 15-30 SECONDS THE NR 1 ENGINE SPOOLED BACK UP. THE AIRCRAFT CONTINUED ON TO KLRD WITH NO OTHER PROBLEMS AND MADE A NORMAL LANDINGSDR RAIA00108009Engine · malfunctioned5422-EWR-CREW PERFORMED LEFT ENGINE SHUTDOWN ON SHORT FINAL, RPM ROSE TO 104.9 AND WAS CLIMBING UPON SHUTDOWN. MAINTENANCE INSPECTED AND PERFORMED FULL POWER RUN IAW ALLIED SIGNAL MM.SDR ZW0A0106504Engine · making metalAT 600 FEET IN DESCENT THE RT ENGINE PRODUCED SMOKE IN THE CABIN AND A PHYSICAL VIBRATION. ENGINE WAS SHUT DOWN. FOUND METAL IN THE TAIL PIPE. CHANGED THE ENGINE.SDR ALG2001F00023Engine · making metalENGINE CHIP LIGHT ILLUMINATED ON LANDING. FOUND LARGE FLAKE ON BOTTOM CHIP PLUG. REPLACED ENGINE ASSEMBLY.SDR 2001UALA01650Engine · stalledNR 1 ENG STALLED DURING DECELERATION TEST AFTER FMU REPLACEMENT. STABLIZED AT IDLE FOR 10 MIN. ENG STALLED ON SECOND ATTEMPT AT APPROX 80 PERCENT N1 ON DECELERATION.SDR EVA004Engine · broken1. A/C B-16408 :Captain report: In cruise found No.1 Engine Vibration 3.0 and EGT higher than other engine.2. On ground check found some metal chips in tail pipe. Request BSI.3.BSI found No.1 Engine HPC Stage 6 had several blades severe damage. 4.Engine ChangeSDR CA020628004Blade · damaged(CAN) COMPRESSOR STALL ON TAKE OFF IN LRM, ON ENGINE NR 2 , MTCE FOUND AFTER VISUAL INSPECTION, 2 BLADES DAMAGED. FURTHER INSPECTION C/OUT IN ACCORDANCE WITH AMM 72-00-00 P.600, REVEALED DAMAGE ON HIGH PRESSURE COMPRESSOR. NUMEROUS BLADES NICKED, CURLED, TORN SDR DL76L011289Engine · leakingON T/O FROM BRU REPORTED SMOKE IN CABIN.CLEARED AFTER 15 MINUTES OF FLT.ATL MTC FOUND OIL LEAKING FROM SPINNER. REPLACED ENGINE.SDR C1HA200196013Engine · flamed outUPON DESCENT INTO DFW NR 2 ENG FLAMED OUT. FOLLOWED RE-LIGHT PROCEDURE. ENG CONFIRMED TO OPERATE NORMALLY WITH NO FURTHER PROBLEMS. TROUBLESHOT IAW JT8D MM TROUBLE SHOOTING -07A CH. 72-00 STEPS 1, 2, 3 REQ'D SKIP TO STEP 27. CHECKED FUEL PUMP AND FCU FILTESDR 2001UALA01619Engine · vibrationLEFT ENG VIB IND FLUCTUATES BETWEEN 1.0 & 1.5 IN CRUISE AT 350. VIB FELT THROUGHOUT AIRCRAFT AND INCREASES INVERSELY WITH THROTTLE. FOUND METAL IN THE TAILPIPE.SDR 2001F00260Engine · failedDURING CLIMB-OUT FROM HNL, CREW NOTED AIRCRAFT VIBRATION FOLLOWED BY NR 2 ENGINE FAILURE. COMPLIED WITH EMERGENCY PROCEDURES CHECK LIST FOR ENGINE SHUT DOWN. JETTISONED FUEL. RETURNED TO HNL AND LANDED WITHOUT INCIDENT. EMERGENCY WAS DECLARED AND EQUIPMENTSDR 2001UALA01602Engine · failedNR 2 ENGINE INFLIGHT SHUTDOWN. ENG IND SHOWED LOW OIL PRESS AND NO N1 OR N2 ROTATION. IFSD OCCURRED IN CRUISE FLT.SDR 2001UALA01627Engine · malfunctionedIN CRUISE LEFT ENG EPR APPROX 1.3 EPR HIGHER THEN RT ENG WITH ALL OTHER PARA EQUAL. IN CLIMB WITH THROTTLES EQUAL RT PARA'S MUCH HIGHER THEN LEFT. LOUD RESONANCE SOUND ROWS 19-24 DURING PWR CHANGES. *S/D* THE NR 2 ENGINE WAS REPLACED FOR DIFFERENCES IN EPRSDR DL72S011271Engine · making metalNR 1 ENG OIL FILTER BYPASS LT ILLUM. C/W POM PROCEDURE. LT DID NOT GO OUT. ENG SHUTDOWN. CA REPLACED NR 1 ENG OIL FILTER, LK CK GOOD. FOUND METAL ON MAIN OIL CHIP DET. PERFORMED ENG PENALTY RUN PER M/M. ON RE-INSP OF CHIP DET FOUND METAL AGAIN. REPLACED NR 1 ESDR HNAA0100043Engine · smokeCREW REPORTED SMOKE/MIST FORMED IN THE CABIN AND COCKPIT. WHEN ENGINE BLEEDS WERE TURNED OFF SMOKE DISSIPATED. REPLACED #1 ENGINE.SDR XNA01016Engine · overtempNR 2 OIL TEMP GAUGE INDICATED 130 DEGREES. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN AS PER CHECK LIST.SDR C2XA01BT133Engine · faultyEWR/BTV---CO3626, CREW REPORTED "AIRCRAFT FILLED WITH FUMES DURING FLIGHT. A CONSTANT LIGHT SMELL OF FUEL/OIL SOMETIMES IT GOT STRONG"...MAINTENANCE TROUBLESHOT TO INTERNAL ENGINE OIL LEAK AIRCRAFT MAINTENANCE FERRIED TO BTV FOR ENGINE CHANGE. REMOVED AND REPLSDR 2001FA0000227Engine · failedLEFT ENGINE SHUT DOWN DUE TO CHIP DETECTOR LIGHT ON ENGINE SURGING AND OIL PRESSURE FALLING OFF. ON INITIAL INSPECTION SUSPECTS COMPRESSOR, NR1 OR NR 2 MAIN LINE BEARING FAILURE.SDR ABXA010419Engine · vibrationDURING CLIMB, RIGHT ENGINE VIBRATION 2.0 TO 2.2, SOME VIBRATION FELT. DURING ALL OTHER PHASES OF FLIGHT, NO VIBRATION FELT. OPENED COWLING AND CHECKED FOR LOOSE DUCTS, ETC. NO DEFECTS. PERFORMED BITE OF AVM AND EEC, NO DEFECTS NOTED AND NO MAINTENANCE MESSSDR 2001UALA01626Blade · fracturedVIBRATION ON NR 1 ENGINE, EEC MODE EICAS ILLUMINATED, EGT FLUCTUATED BETWEEN 120 AND 180 AT IDLE, EPR INDICATION LOST, N1 & N2 INDICATIONS NORMAL. CREW ELECTED TO SHUT DOWN ENGINE AND RETURN TO FIELD. *S/D* 1 EA T2 BLADE FAILED AT THE PLATFORM. 2 EA ADJACE
Back to JASC 7200