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 CA120823003Engine · failed(CAN) HAD ENGINE FAILURE IN FLIGHT, ENGINE REMOVED AND SENT TO FOR INVESTIGATION.SDR CA120821003Engine · vibration(CAN) APPROXIMATELY 30 MIN AFTER DEPARTURE, THE PILOT FELT A SMALL VIBRATION. 10 MINUTES LATER, THE FOLLOWING CAS MESSAGE WAS SEEN: GEN OFF L. AFTER ANOTHER 45 MIN, DURING APPROACH TO LFPB, OIL PRESSURE RAISED AND THEN DECREASED TO 0 PSI. ENGINE WAS SHUTDOWNSDR UALA2012081304362Engine · failedENGINE VIBRATION, RETURNED TO FIELD. FOUND SMALL METAL PARTICLES IN TAIL PIPE AND ABNORMAL NOISE DURING SHUTDOWN. REPLACED ENGINE.SDR UALA2012081304452Engine · vibrationCREW REPORTED DURING CLIMB POWER, NR 2 ENGINE VIBRATION INDICATION AT 3.0 UNITS, AT APPROXIMATELY 88 PERCENT N1. VIBRATION FELT IN AIRFRAME. VIBRATION LEVEL DID DECREASE WITH REDUCTION IN N1 SPEED. NR 2 ENGINE REPLACED.SDR QMLA2012081112132Engine · making metal20 MINUTES INTO FLIGHT, THE NR 2 ENGINE CHIP LIGHT ILLUMINATED. ACTIVATED THE FUZZ BURNER FOR APPROX 1 SECOND AND THE LIGHT EXTINGUISHED. APPROX 1 SECOND LATER THE CHIP LIGHT ILLUMINATED AGAIN. ACTIVATED THE FUZZ BURNER AGAIN AND LIGHT EXTINGUISHED. APPROSDR UALA2012081304444Engine · overtempLT ENGINE EGT EXCEEDANCE, IN AREA C, BEFORE NEXT FLIGHT ACCOMPLISH VISUAL CHECKS AND HOT SECTION BORESCOPE PER AMM 72-00-00. REPLACED NR 1 ENGINE.SDR UALA2012080904333Engine · faultyLEFT ENGINE FIRE LP2 STATUS MESSAGE DISPLAYED AFTER POWER TRANSFER TO GROUND UNABLE TO CLEAR MESSAGE. REPLACED NR 1 ENG PER MM.SDR CA120821002Engine · power loss(CAN) DURING CLIMB AT 1900 FT, THE PILOT HEARD ABNORMAL NOISES FROM THE ENGINE FOLLOWED BY EXHAUST SMOKE AND POWER LOSS. THE PILOT SECURED THE ENGINE INTO FEATHER MODE. THE ACFT LANDED SAFELY. PRELIMINARY INSPECTION REVEALED SEIZED PROPELLER SHAFT.SDR Q2SA2012080876504Case · crackedNORMAL FLAPS 20 TAKEOFF WITH REDUCED THRUST. AT 1000 AGL, NR 3 FIRE WARNING ILLUMINATED AND FIRE BELL SOUNDED. SHUTDOWN ENGINE PER QRH PROCEDURES. REQUESTED AND RECEIVED VECTORS TO DUMP FUEL OVER THE WATER, DUMPED DOWN TO MAKE 630 LANDING WEIGHT. AFTER ENGISDR BTEA2012F00158Engine · vibrationINTEGRATED INFORMATION DISPLAY SYSTEM, (IIDS), DISPLAYED A "MINOR" ENGINE FAULT "TQ TRIM LVL L" FOR THE NR 1 ENGINE FROM THE DIGITAL ENGINE CONTROL UNIT (DECU). PILOTS CHECK FOR FAULTS FROM THE DECU AND THE IIDS. A MINOR FAULT WAS NOTED ON THE NR 1 ENG; "TQSDR CA120813014Engine · stopped(CAN) REPORTEDLY, THE NR 1 ENGINE HAD A SUDDEN STOPPAGE IN FLIGHT. THE ACFT LANDED SAFELY. FSR REQUESTING FURTHER DETAILS. MFG IS FULLY COMMITTED TO ADDRESS THIS ISSUE PROACTIVELY AND WE WILL KEEP OPERATORS INFORMED OF OUR PROGRESS.SDR CNMA2012080001Engine · overtempTEMP LT ENGINE HIGH 179 ON BOTH LT AND RT EICAS COMPUTERS QRH FOLLOWED THRUST ON LT ENGINE REDUCED TO IDLE DUE TO OTHER INDICATIONS NORMAL ENGINE SHUTDOWN AND SECURE.SDR SWAA2012080906612Engine · seizedINFLIGHT SHUTDOWN / AIR TURNBACK -- AT APPROX 9000FT MSL ON CLIMBOUT WITH FLAPS UP, CLIMB THRUST SET, 340 KTS (+) NR 2 ENGINE SEIZURE OCCURRED. REMOVED AND REPLACED NR 2 ENGINE IAW MT.SDR UALA2012080704256Liner · damagedRIGHT ENGINE HAS A HOLE IN THE ACCOUSTIC LINER AT THE 6 O'CLOCK POSITION. ATTRITION LINER DAMAGED AT THE 6 O'CLOCK POSITION, 1 INCH HOLE BY 3 INCH DELAMINATION. RT ENGINE HAS A THREE QUARTER INCH CHUNK OF HONEYCOMB MISSING AT THE 1730 POSIT NEXT TO FAN. OK SDR UALA2012080604195Engine · unknownON ENGINE START NR 1 OIL PRESSURE 121, NR 2 152, EGT 480 AND CLIMBING NO ROLL BACK ON NR 1. ACCOMPLISHED NORMAL START. ALL PARAMETERS NORMAL AT IDLE.SDR KCSA20120806009Engine · malfunctionedCLIMBING THRU FL 26.0 NR 3 ENGINE EXPERIENCED A LOUD BANG FOLLOWED BY VIBRATION. ENGINE WAS SHUTDOWN IAW QRH PROCEDURES, NO FIRE LIGHT ILLUMINATED. AFTER SHUTDOWN, OIL PRESSURE READS 6 PSI AND N2 RPM 21%. TOTAL FLIGHT TIME ENGINE WINDMILLED 58 MINUTES. TIMESDR UALA2012080604185Engine · faultyREF L ENG EGT EXCEEDANCE. REPLACED NR 1 ENGINE IAW AMM 72-00-00 PAGE 623 CONFIG 2.SDR REXA2012080401224Engine · odorDURING CLIMB-OUT, FLIGHT 4416, FLIGHT ATTENDANT NOTICED POSSIBLE SMOKE IN CABIN. SMOKE ODOR IN COCKPIT. NO FIRE INDICATIONS. AIR RETURNED TO DEPARTURE. FLIGHT ATTENDANT STATED THAT IS SEEMED TO COME FROM THE FLOOR VENTS. REMOVED AND REPLACED RIGHT ENGISDR CA120813008Engine · vibration(CAN) ON A REVENUE FLIGHT, THE FLIGHT CREW REPORTED THAT THE NR 2 ENGINE VIBRATION GAUGE WAS NOTED TO BE BETWEEN THE GREEN AND YELLOW BAND BUT THE VIBRATION COULD NOT BE FELT. THE PILOT THROTTLE BACK THE POWER TO IDLE WITH NO CHANGE ON THE VIBRATION INDICATIOSDR A6WA201240760Engine · malfunctionedAPPLICATION OF TAKE OFF POWER, FELT VIBRATION IN AIRFRAME FOLLOWED BY LT ENGINE LOW OIL PRESSURE CAS MESSAGE. ABORTED TAKE OFF AT LESS THAN 20 KTS. PULLED ACFT OFF RUNWAY, NOTICED ITT WAS FULL SCALE AND N1 AND N2 VIB MESSAGES APPEARED. LEFT ENGINE REPLACEMESDR UALA2012080304153Warning Message · illuminatedNR 2 ENGINE EIU FAULT REPORTED ON LOWER ECAM MAINT STATUS MESSAGES. REPLACED 2KS. CHECKED OK AFTER ENGINE RUN.SDR CHQA20120803230Engine · leakingCREW REPORTED A BURNING OIL SMELL IN THE COCKPIT DURING FLIGHT. THE AIRCRAFT LANDED WITHOUT INCIDENT AT ITS INTENDED DESTINATION. MAINTENANCE REPLACED THE NUMBER 1 ENGINE. OPERATIONAL CHECKS WERE GOOD WITH NO DEFECTS OR SMELLS NOTED.SDR CA120813003Engine · shutdown(CAN) IT IS REPORTED THAT THE ENGINE SUFFERED AN IN-FLIGHT SHUTDOWN FOLLOWING TAKEOFF AND LANDED SAFELY. FEW OTHER DETAILS ARE KNOWN AT THIS TIME. FSR FOLLOW UP.SDR COEA2012080201700Engine · power lossAIR TURNBACK GEG FLIGHT 8903: SHORTLY AFTER TAKEOFF AND BELOW 900FT AGL TAKEOFF POWER SLOWLY DECREASED. EMERGENCY POWER LEVER WAS USED TO RETURN SAFELY TO GEG. NO EMERGENCY WAS DECLARED. UNABLE TO DUPLICATE THE PROBLEM ON THE GROUND. AS A PRECAUTION ENGINSDR UIEA2012080200340Warning Light · illuminatedAFTER ENGINE START, EICAS WARNING MESSAGE "RT ENG EEC PROBE", AND "ENG MACH PROBE" ILLUMINATED.SDR AALA20120801009Engine · failedDFW - CREW REPORTED RIGHT ENGINE FIRE. RIGHT ENGINE SEIZED AND UNCOMMANDED SHUTDOWN (SINGLE ENGINE TIME 12 MINS). EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. UPON INSPECTION FOUND TURBINE BLADES MISSING ANSDR UALA2012073104126Engine · unknownAT FL360, IN SMOOTH AIR, FOR ABOUT 15 MINS, BOTH ENG HAD FLUCTUATING PARAMETERS. LEFT ENG EPR RAPIDLY CHANGED FM LESS THAN 1.0 TO 1.45, N1 +--4%, EGT +-- 6, FF +--.4. CHECKED LEFT PIMU EEC CH A REVERSER RNG FAIL DISPLACED CHECKED ASSOCIATED WIRING PLUGS AND SSDR EHAA20120731006Engine · power lossDURING CLIMB, NR 2 ENGINE EGT DROPPED TO ZERO AND ENGINE LOST POWER.SDR UALA2012073104127Actuator · failedECAM REPORTS NR 1 ENGINE FADEC B FAULT. NR 1 ENGINE STALL. STEADY STATE CLIMB, 8 MINUTES AFTER TAKEOFF. REPLACED NR 1 ENGINE LPC BLEED SLAVE ACTUATOR. REPLACED LOW PRESSURE COMPRESSOR BLEED MASTER ACTUATOR, REF EM3454-1. REPLACED ACTUATOR IAW AMM.SDR ASOA20120730066CEngine · failedTHE CREW REPORTED ENGINE NR 1 FAILURE IN FLIGHT. ACFT LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.SDR UALA2012073004099Engine · vibrationNR 1 ENGINE VIBRATION UP TO 8.1 HAD TO REDUCE EPR TO 1.05 TO GET VIBRIATION UNDER 5.0. REMOVED AND REPLACED NR 1 ENGINE REF MT 71-017.SDR ASOA20120729065Engine · leakingTHE CREW REPORTED SMOKE VISIBLE IN CABIN AT 6000 FT. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX REPLACED THE NR 2 ENGINE, OPS CHECKED GOOD.SDR FDEA201207272719Engine · firePUSH CREW REPORTED NR 1 ENGINE EMITTING FLAMES ON START. START VALVE CLOSED AT 33 PERCENT N2, EARLY INDICATIONS 510 F/F, 168 EGT. CONTINUED TO MOTOR ENGINE WITH FUEL LEVER OFF FOR REJECTED START. FLAMES WERE REPORTED AT THIS TIME. TAILWIND OF 10 KTS. SUSDR CA120802010Engine · unknown(CAN) NR 2 ENGINE TORQUE STARTED TO DECREASE FOLLOWING THE FUEL FLOW, WF, DECREASE PASSING BY 3000 FT SHORTLY AFTER TAKEOFF. THE POWER PLANT WENT TO AUTOFEATHER AND ENGINE WAS STABILIZED. NO DETAIL OF PARAMETER WERE GIVEN. THE PILOT TRIED TO RESTART THE ENSDR FDEA201207262710Engine · failedUPASSING 3000 ON T/O, FELT ABNORMAL VIBRATION WITH UNUSUAL NOISE. NOTICED N1 VIB AT 1.4 AND N2 VIB AT 2.4 ON ENG 1. WHILE TROUBLESHOOTING RECEIVED ENG 1 EPR MODE FAULT AND ATS LEVER KICKED OFF. NOTICED ENG 1 EGT GAUGE INOP AT "0". ENG 1 N1 BEGAN UNCOMSDR ASMF201207008Engine · making metalCAPTAIN REPORTED THAT DURING DESCENT, THE RT ENGINE OIL FILTER BYPASS LIGHT TURNED ON. MX PERSONNEL REMOVED THE FILTER ASSY AND CHIP DETECTOR ABG/TGB, DETECTED METAL PARTICLES. RT ENGINE NR 2 WAS REPLACED AND TESTED IAW AMM 71-00-02 AND IAW AMM 71-00-00, ALLSDR CA120802012Engine · power loss(CAN) IT WAS REPORTED THAT THE NR 1 ENGINE ROLLED BACK DURING CRUISE. TROUBLESHOOTING ONGOING.SDR CA120802007Engine · power loss(CAN) DURING REVENUE FLIGHT, PILOT EXPERIENCED A 11 PERCENT N1 ROLLBACK AT 43000FT. THE CREW REPORTED THAT THE ENGINE RETURNED TO RATED POWER AFTER 2 MINUTES AND 15 MINUTES LATER THE AMBER LIGHT FOR VIBES CAME ON AND WENT OUT TWICE. TROUBLESHOOTING IS ON-GOISDR CA120801007Engine · failed(CAN) DURING CLIMB, PILOT REPORTED A LOUD RUMBLE FOLLOWED BY A YAW, NR 1 ENGINE ITT WENT IN TO THE RED WITH NP AND TQ FLUCTUATING. PILOT SHUTDOWN THE NR 1 ENGINE. ACFT SAFELY RETURNED. ENGINE REMOVED AND SENT TO MFG FOR INVESTIGATION. ENGINE CHANGE COMPLETEDSDR HALA2012072400180Engine · power lossON INITIAL THROTTLE UP FOR TAKE OFF PUSHED THROTTLES UP TO APPROX 23 PERCENT N1 RT ENG SPOOLED UP NORMAL, LEFT ENG LAGGED APPROX 2-3 SECONDS BEFORE SPOOLING UP FOR NORMAL THROTTLE POSITION. ACCOMPLISHED TEST NR 4 - GROUND TEST FOR TAKEOFF POWER, ACCELERATION SDR UALA2012072404017Liner · damagedNR 1 ENGINE ACOUSTICAL LINER HAS SOME DAMAGE. REF MT78-010 FOR ALLOWABLE DAMAGE. DAMAGED AREA IS ON THRUST REVERSE R SLEEVE INNER WALL. AREA IS APPROXIMATELY 7 INCHES WIDE BY 31. 5 LONG. LOOSE MATERIAL TRIMMED AND INTERIM REPAIR ACCOMPLISHED BY APPLYING SPESDR QMLA2012072012118Engine · making metalENGINE WAS INSTALLED AT ACFT TT 2647+57 ENGINE TT 3996+36. THIS ENGINE WAS RECENTLY REPAIRED. FIRST CHIP EVENT AT ACFT TT 2660+27 ENG TT 3508+56 FOUND CAT.( A) DUST. PERFORMED DRAIN AND FLUSH OF OIL SYS WITH FILTER CHANGE AT FLUSH AND AGAIN AFTER 15 MINUTES GSDR CA121105013Engine · power loss(CAN) DURING THE ROLLING TAKE OFF, THE ENGINE NR 2 DID NOT PRODUCE THE TAKE OFF POWER REQUESTED BY THE CREW. THE CREW ABORTED TAKE OFF AND SUBSEQUENT GROUND TEST CONFIRMED THE ISSUE ON THE NR 2 ENGINE. BLEED VALVE AND ITS TORQUEMOTOR WAS SUSPECTED.SDR DXTA201207190553Engine · odorAFTER TAKEOFF, SMELLED A BURNING SMELL AND THERE WAS WHAT APPEARED TO BE A MIST IN THE CABIN. PERFORMED AN EMERGENCY RETURN TO DEPARTURE. INSPECTED RT ENGINE AND FOUND EVIDENCE OF OIL IN THE EXHAUST DUCT AND COWLS. INSPECTED ENGINE INLET WITH BORESCOPE IAW SDR AALA20120717007Engine · failedJFK - CREW REPORTED RIGHT ENGINE OIL LOSS AND UNCOMMANDED ENGINE SHUTDOWN. EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE AT JFK ON 07/17/2012. SYSTEM GROUND CHECK NORMAL OPERATION.SDR CA120723008Engine · malfunctioned(CAN) WHILE THE ACFT WAS ON CRUISE FLIGHT AT 1000 FT. WITHOUT ANY WARNING OR ABNORMAL BEHAVIOUR THE ENGINE SHUTDOWN. A RE-START WAS ATTEMPTED WITHOUT SUCCESS AND THE PILOT PERFORMED A DEAD STICK LANDING ON A FLAT FIELD. PILOT UNINJURED BUT THE ACFT SUSTAISDR CA120723005Engine · flamed out(CAN) DURING REPOSITIONING FLIGHT, THE CREW HEARD LOUD BANGS FROM RT ENGINE AT 43000 FEET. ONCE THROTTLE WAS PULLED BACK THE ENGINE FLAMED OUT. THE RELIGHT WAS SUCCESSFUL AND PILOT ELECTED TO DIVERT. REST OF FLIGHT WAS UNEVENTFUL.SDR UALA2012071703864Engine · failedAFTER TAKE OFF HEAVY VIBRATION 5.0 UNITS ENG1 SN.727667, THROTTLE PULLED BACK TO IDLE POWER TILL LANDING, FOUND EXTENSIVE DAMAGE TO SEVERAL FAN BLADES, INLET COWL, EXIT GUIDE VANES. NR 1 ENGINE HAS DAMAGE TO FAN EXIT OUTER CASE ALUMINIUM CASTING DAMAGED ON FSDR UALA2012071803901Liner · damagedNR 1 ENGINE MISSING 1.5 INCH BY 1.5 INCH SECTION IN THE FAN CASE ATTRITION LINER AT 1 O'CLOCK POSITION. REPAIRED PER MT 72-017 REF PTT 6822015 AND PTT 6822019.SDR WI5R2012071600001Spinner · fracturedON ENGINE, DURING CLIMB AT 94 PERCENT N1, THE PILOTS HEARD A THUMP AND A LOW PITCH NOISE. ON GROUND TROUBLESHOOTING REVEALED A MISSING SECTION OF THE SPINNER AND DAMAGE TO THE FAN, INLET AND FAN STATOR.
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