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 CA050620001Engine · failed(CAN) AN AIRCRAFT EXPERIENCED AN ODOR AND WHITE SMOKE IN THE CABIN APPROXIMATELY 3 MINUTES AFTER TAKE OFF. THE CAPTAIN DECLARED AN EMERGENCY AND REQUESTED AN IMMEDIATE RETURN TO BASE. ON GROUND, THE ODOR AND SMOKE WAS CONFIRMED TO BE COMING FROM THE NR 2 ENGSDR AWXA200500722Engine · malfunctionedDURING TAKEOFF AT T/O POWER SETTING, APPROX 1.04 EPR, ACFT VEERED LEFT. REJECTED TAKEOFF BEFORE FURTHER POWER. NO ABNORMAL INDICATIONS NOTED BUT SUSPECTED NR 1 ENG LAGGED NR 2 ENG IN SPOOLING UP. RAN ENGINES UP TO 70 PERCENT N1 PER MAINTENANCE CONTROL. ALLSDR CA050628001Turbine · shutdownA/C EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE NR 1 ENGINE AT FL 120 AFTER TAKEOFF. ITT WENT TO 900 DEGREES C AND THE CREW REDUCED THE THROTTLE AFTER WHICH THE ENGINE SHUTDOWN, UNCOMMANDED. THE AIRCRAFT RETURNED AND LANDED SAFELY WITH NO INJURIES REPORTED. SDR CA050621012Engine · flamed out(CAN) ON DESCENT, THE ENGINE WAS REPORTED TO HAVE EMITTED A NOISE AND SUBSEQUENTLY FLAMED OUT. THE ENGINE WAS SUCCESSFULLY RE-STARTED IN FLIGHT AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCSDR 2005UALA00569Engine · stalledNR 2 ENGINE OVERTEMPTED & STALLED ON TAKEOFF. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADE) FAILURE. THIS IS AN INDUSTRY-WIDE AND KNOWN ISDR SWAA051805Engine · vibrationNR 2 ENGINE HAD NOTICABLE SHUDDER. VIBRATION GAUGE INDICATED 4.5. IDLE DESCENT OK. INCREASE POWER AT 12,000FT & ENGINE VIBRATION INDICATED OFF THE SCALE. REMOVED AND REPLACED NR 2 ENGINE ASSY PER MM.SDR C2XA05CL048Engine · failedCLE FLIGHT 2668 THE CREW REPORTED A LOUD BANG FOLLOWED BY NR 1 ENGINE SHUTDOWN. THE AIRCRAFT RETURNED TO CLE AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 1 ENGINE. OPERATIONAL CHECKS WERE GOOD.SDR CA050621013Engine · shutdown(CAN) DURING LEVEL FLIGHT, THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. THE CREW SECURED THE ENGINE AND FEATHERED THE PROPELLER. SUBSEQUENT INSPECTION REVEALED METALLIC PARTICLES ON THE TURBO MACHINE CHIP DETECTOR AND IN THE ENGINE OIL FILTER. THE ENGINESDR MASA200500467None · noneASH 6169 LAS - ABORTED TAKEOFF DUE TO THE NR 2 ENGINE OVERTEMP ON TAKEOFF ROLL 904 DEG FOR 4 SECONDS. MX FOUND THE ENGINE TO NOT EXCEED AMM LIMITS. MAINTENANCE PERFORMED A COMP WASH.SDR CA050621016Engine · shutdown(CAN) THE ENGINE EXPERIENCED AN IN-FLIGHT SHUTDOWN UNDER UNKNOWN CIRCUMSTANCES. MFG WILL MONITOR THE INCIDENT AND ADVISE OF ROOT CAUSE, ONCE DETERMINED.SDR P5CA0501373Engine · failedAFTER TAKEOFF NR 1 ENGINE FAILED. SHUT DOWN ENGINE AND JETTISON FUEL IAW CHECK LIST. AFTER SHUT DOWN OIL PRESSURE ZERO. NR 1 ENGINE REPLACED PER ENGINE CHANGE FORM 00-AA-45. RUN UP OK PER MM 71-00-00 TEST NR 3, 8 AND 9.SDR DXTA200500774Engine · malfunctionedABORTED TAKEOFF, RIGHT ENGINE WOULD NOT MAKE TAKEOFF POWER (97.2) ONLY ACHIEVED 95.3 PERCENT. RAN RIGHT ENGINE TO TAKEOFF POWER [97.2], ALL PARAMETERS WERE WITHIN ACCEPTABLE LIMITS IAW CE 560 MM 71-01-02.SDR UPS05544695Engine · power lossLOSS OF POWER LT ENGINE. LT ENG HIGH EGT AND EPR INDICATION.SDR CA050621009Engine · failed(CAN) DURING CLIMB THE ENGINE EXPERIENCED AN UNCOMMANDED REDUCTION IN TORQUE, ACCOMPANIED BY A SLIGHT BURNING ODOR. SUBSEQUENTLY, ENGINE OIL PRESSURE REDUCED AND A FIRE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINSDR BA05011Line · brokenCREW RECEIVED THE ECAM WARNING ENG 2 EPR MOD FAULT. THE CREW ALSO NOTED THE LOSS OF AUTOTHROUTTLES. DUE TO LACK OF PARTS IN FRA, THE FLIGHT RETURNED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED A BROKEN P4.95 SENSE LINE.SDR UIA0505Engine · failedRT ENGINE IN FLIGHT SHUTDOWN (IFSD) CAUSED BY SURGE MESSAGE SHOW ON EOAP, THEN FOLLOW EGT RAPID INCREASE. AFTER LANDING CHECK FOUND SEVERAL STAGE 4 BLADES MATERIAL MISSING AND BEND WITH DENTS. STAGE 5-12 BLADES BURN. THIS CASE COULD BE IOD IAW AMM 71-00-10.SDR T48R20050012Blade · fracturedENGINE WAS REMOVED FROM 821NK NR 2 POSITION FOR VISIBLE TURBINE DAMAGE. INSPECTION REVEALED THE T-4 BLADES MISSING/FRACTURED AT THE BASE OF BLADE WITH CORRESPONDING DAMAGE TO THE T-3 VANES.SDR 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 DLM88050318Engine · failedLT ENGINE FAILED AT 15K FT AND 300 KNOTS - REPLACED ENGINE FOR INTERNAL FAILURESDR 2005UALA00532Engine · malfunctionedDIVERTED DUE TO RT ENGINE OIL QTY AND PRESSURE IND. RT ENGINE SHUTDOWN. IN CRUISE LOSS OIL QTY & PRESSURE. CREW SHUTDOWN ENGINE. UPON LANDING FOUND EXHAUST OIL WETTED. ENGINE REMOVED. UPON DISASSEMBLY OF ENGINE FOUND NR 5 BEARING BAY HEAVILY COKED & NR 5 SCASDR CHQA200500110Engine · malfunctionedFLIGHT 3201 BUF-LGA - ON INITIAL CLIMB AT APPROXIMATELY 8000 FT, E2 ITT BEGAN TO RISE ABOVE 900 DEGREES. RAN QRH AND THE PROBLEM STILL PERSISTED. THERE WERE NO OTHER ABNORMAL INDICATIONS. THE OIL TEMP AND PRESSURES WERE NORMAL. THE TEMP CONTINUED TO RISE ASDR CA050617008Engine · flamed out(CAN) RT ENGINE ROLLED BACK, FLAMED OUT DURING CRUISE, AT FL380. NO ABNORMAL INDICATIONS SHOWN. CREW DECLARED EMERGENCY, DESCENDED TO FL210 AND RESTARTED ENGINE USING CROSS BLEED. UNEVENTFUL LANDING AT DIVERSION AIRPORT. NO LEAKS FOUND DURING GROUND RUNS. FUELSDR 2005FA0000871Adapter · crackedDURING OVERHAUL OF ENGINE AWN ADAPTER, NDT FOUND .450 INCH TOTAL LENGTH CRACK IN THE BOLT HOLE OF LUG NR 1. IN THE BORE OF LUG, CRACK LENGTH IS .300 OF INCH AND ACROSS FACE OF LUG, THE CRACK LENGTH IS .150 OF INCH. ILLUSTRATION DEPICTS LOCATION AND SCHEMATICSDR ASMF200506012Engine · fodDURING TRANSIT TO PLATFORM WITH APU OUT OF SERVICE AND THE LEFT ENGINE DID OPERATE, IT HAD AN FOD DUE TO INGESTION OF WOOD CHOCK. DURING REVISION WERE DETECTED FOUR BLADES AND NOISE SUPPRESSOR WITH LEAST DAMAGES AND THERE WERE REWORKED IAW 72-33-22. BOROSCOPSDR CA050621008Engine · failedDURING AN STC FLIGHT TEST, THE AIRCRAFT WAS FLOWN TO A 45 DEGREE ANGLE FOLLOWED BY A PUSH-OVER RESULTING IN A ZERO GRAVITY CONDITION. THE LOW ENGINE OIL PRSSURE WARNING ANNUNCIATED AND BOTH PROPELLERS FEATHERED. ENGINE POWER WAS REDUCED AND OIL PRESSURE STABISDR PNSA050602Engine · malfunctionedLT ENGINE HAD AUTO IGNITION EVENT DURING CRUISE IN CLOUDS ANTI-ICE SYSTEM WAS ON. NO VISIBLE ICE NOTED BY CREW HOWEVER THERE WAS ICE FORECAST. CREW REPORTED ONE IGNITION RELIT AND CONFIRMED IGNITION LIGHTS ON. ALL OTHER PARAMETERS NORMAL. CREW ELECTED TO RSDR 2005UALA00536Engine · stalledNR 1 ENGINE EXPERIENCED TWO COMPRESSOR STALLS, ONE IN CRUISE AND ONE AT TOP OF DESCENT. ENGINE WAS CHANGED AND AIRCRAFT CONTINUED FLYING AFTERWARDS WITHOUT FURTHER INCIDENT. COMPRESSOR STALL WAS CAUSED BY HIGH-PRESSURE COMPRESSOR (HPC) BLADE DAMAGE PRIMARILYSDR PNSA050601Engine · malfunctionedLT ENGINE HAD AUTO IGNITION EVENT DURING CRUISE IN CLOUDS WITH ANTI-ICE SYSTEM ON. NO VISIBLE ICE NOTED BY CREW HOWEVER THERE WAS ICE FORCAST. CREW REPORTED 1 IGNITION RELIT AND CONFIRMED IGNITION LIGHTS ON. ALL OTHER PARAMETERS NORMAL. CREW ELECTED TO RETSDR 2005UALA00509Engine · failedLOUD BANG ON CLIMBOUT FROM NR 1 ENGINE. OIL QUANTITY AND PRESSURE WENT TO ZERO, EGT RED LINED. ENGINE WAS REPLACED AND AIRCRAFT CONTINUED FUTHER FLYING WITHOUT INCIDENT. THE ENGINE FAILURE WAS CONFIRMED AS A HIGH PRESSURE COMPRESSOR 3RD STAGE BLADE (R3 BLADSDR DHL2005801012Mec · malfunctionedAT FL.360. NR 1 ENGINE FLAMED OUT. NR 1 MAIN FUEL QUANTY GUAGE WAS SHOWING 2000 LBS. W/INTERMITTED FUEL SELECTED. THERE WAS NO MASTER CAUTION OR NR 1QT.LOW LIGHT. REPLACED NR 1 ENGINE MEC PER CFM 56 M/M CH. 73-21-10. OPS CHECKS NORMAL ON ENGINE RUN. FAULT 5SDR PIDA20050050Engine · bird ingestionINGESTED BIRD IN RIGHT ENGINE AT ROTATION. VIBRATION INDICATION 4.0 UNITS AT POWER REDUCTION. INSPECTED ENGINE PER MM 71-00-47. UNSHINGLED BLADES NR 20, 21, 22, 23, AND 24. ALL ENGINE PARAMETERS AND VIBRATION CHECKS NORMAL ON ENGINE RUN.SDR MASA200500436Engine · overtempASH 6322 PHX - PHX TO GJT ABORTED TAKEOFF DUE TO THE RT ENGINE ITT OVERTEMP. MAINTENANCE REPLACED NR 2 ENGINE.SDR GTIA050162Engine · failedRT ENGINE FAILURE DURING CLIMB THROUGH 22,000 FT, COMPRESSOR STALLED, EGT 710 FEET ENGINE ROLLED BACK AND SHUTDOWN. FOUND TURBINE SECTION FAILED. REMOVED AND REPLACED NR 2 ENGINE. OPS CHECK AND LEAK CHECK GOOD. (M)SDR MASA200500421None · noneASH 6087 PHX - ABORTED TAKEOFF DUE TO THE ENGINE 2 OVERTEMP ON TAKEOFF ROLL. WITHIN LIMITS PER MANUALSDR 05FDEA01488Case · crackedNR 2 ENGINE, LEFT HAND CASE APPROXIMATELY 7 - 8 O' CLOCK POSITION, FOUND CRACKED. REPAIRED PER AMM 72-33-00-300-801.SDR 05FDEA01489Case · crackedNR 2 ENGINE, RIGHT HAND CASE APPROXIMATELY TWO O' CLOCK POSITION CRACKED, FOUND ON FLANGE AT BORE COOLING VALVE LOWER FASTENER HOLE. COMPLIED WITH FEDEX EA 1-7223-90165.SDR CA050531003Engine · making metal(CAN) DURING ENGINE START, ENGINE FAILED TO ACHIEVE APPROPRIATE RPM. START ABORTED. TROUBLESHOOTING FOUND DEBRIS IN THREE CHIP DETECTORS. ENGINE WILL BE CHANGED AND SHIPPED BACK TO OVERHAUL FACILITY FOR INVESTIGATION.SDR CA050609013Engine · failed(CAN) OPERATORS REPORT OF FOD TO LP IMPELLER. INSPECTION REVEALED THAT REMAINING COMPONENTS IN COLD AND HOT SECTION SUFFERED MINIMAL DAMAGE WITH EXCEPTION OF ONE LP TURBINE BLADE. MOST FOREIGN MATERIAL HAD HIT LP IMPELLER EXITED BACK OUT THROUGH INTAKE. A MINISDR CA050923002Engine · overheated(CAN) MFG HAS RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. THE FLIGHT CREW REJECTED TAKE-OFF WHEN THEY NOTICED THE AIRCRAFT VEERING TO THE RT ASSOCIATED WITH ENGINE NR 2 OIL PRESSURE AND ITT ABNORMALITIES. TAKE-OFF WAS ABORTED AT APPROXIMATELY 100 SDR VTZA200500090Engine · shutdownRT ENG SHUTDOWN ON TAKEOFF ROLL AT ROTATION.SDR CA050527032Engine · shutdownDURING CLIMB, THE ENGINE EXPERIENCED AN UNCOMMANDED SHUT-DOWN COINCIDENT WITH THROTTLE INPUT FOR POWER REDUCTION. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. PWC WILL MONITOR THE INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR CA050705004Bearing · fractured(CAN) ENGINE ORIGINALLY OVERHAULED IN 2002, FIRST RUN. AT THAT TIME, A PROCESS TO CLEAN OIL JET NOZZLE 3 AND 4 WAS UTILIZED AS PER OEM MANUAL. OTHER OPERATORS HAD EXPERIENCED DIFFICULTY WITH THE 3/4 OIL NOZZLE AND IT WAS FOUND THAT PROPER AND THOROUGH CLEANINGSDR CA050621004Engine · failed(CAN) BEFORE ACHIEVING TAKE-OFF POWER, THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A LOW OIL PRESSURE WARNING ANNUNCIATION. THE CREW ABORTED TAKE-OFF AND SHUT THE ENGINE DOWN. SUBSEQUENT INSPECTION REVEALED SEIZURE OF THE LOW PRESSURE ROTOR. MFG WILL MONSDR CA050527031Engine · shutdownON TRANSITION BETWEEN CLIMB AND CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED SHUT-DOWN. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. PWC WILL MONITOR THE INVESTIGATION OF THE EVENT AND ADVISE OF ROOT CAUSE, ONCE ESTABLISHED.SDR ASMF200505027Engine · failedCAPTAIN REPORTED THAT DURING DESCENT AT 18500 FEET, THE LEFT ENGINE OIL FILTER LIGHT CAME ON. THE ABNORMAL PROCEDURE 05-14 WAS PERFORMED AND THE A/T ARMED SWITCH WAS SHUT OFF AND THE ACCELERATOR WAS HELD BUT LIGHT CONTINUED. ENGINE WAS SHUT DOWN. AT PLATFORSDR CA050527029Engine · shutdownON DESCENT, THE ENGINE EXPERIENCED AN UNCOMMANDED SHUT-DOWN. AN IN-FLIGHT RELIGHT WAS SUBSEQUENTLY ACCOMPLISHED. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE, ONCE DETERMINED.SDR CA050621003Engine · failed(CAN) DURING CRUISE SMOKE BECAME EVIDENT IN THE CABIN ACCOMPANIED BY HIGH ENGINE OIL TEMPERATURE AND LOW OIL PRESSURE INDICATIONS. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION FOUND OIL LEAKING FROM THE ENGINE INLET AREA. MFG WILL MONITOR THE ISDR AALA20050349Engine · leakingNR 1 ENGINE WAS SHUT DOWN IN FLIGHT DUE TO LOSS OF OIL QUANTITY AND OIL PRESSURE AT FLIGHT LEVEL 360. SINGLE ENGINE OPERATION FOR 90 MINUTES. AIRCRAFT DIVERTED TO MIA. REPLACED NR 1 ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR DL738050287Cover · looseNR 1 ENG OIL QTY TOP ZERO. ENG OIL PRESS TO REDLINE. FLT CREW COMPLETED ENG FAILURE SHUTDOWN PER QRH CHECK LIST. UNEVENTFUL SINGLE ENG LANDING AT SLC. NR 1 ENG WINDMILL WITH POS PRESS AT ALL TIMES. FOUND NR 1 ENG TURNING PAD COVER LOOSE. REPLACED O-RINGSSDR WRNA200500013Engine · damagedNR1 ENGINE COMPRESSOR STALLED AT FL 11.5, AIRCRAFT RETURNED. LANDING NORMAL. ENGINE BOROSCOPE COMPLIED WITH, NO DISCREPANCIES NOTED. NR 1 ENGINE FAN CASING ACOUSTIC LINERS FROM 1O`CLOCK TO 8 O'CLOCK POSITION DAMAGED. REMOVED AND REPLACED PANELS IAW 72-31-08,
Back to JASC 7200