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 IPXA12B73984Engine · contaminatedIFSD - 'ENG 1 OIL FILT' EICAS FOLLOWED QRH PROCEDURES, NOTED OIL TEMP 121 & PRESS 87. MCD INSPECTION, FOUND LARGE AMOUNT OF DEBRIS. R & R NR 1 ENGINE IAW TC 71- 000-00-01 AND OPS CHECKED.SDR SIMA20120614003Unknown · smokeFLIGHT 4118, NR 1 ENGINE SMOKING 10 MINUTES AFTER SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. INSPECTED INTAKE AND EXHAUST OF ENGINE FOR OIL LEAK, GROUND RAN ENGINE IAW MM 72-00-00. COULD NOT DUPLICATE. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR NSVA20120613554Engine · vibrationDURING EN ROUTE CLIMB, THE CREW FELT SEVERE VIBRATION COMING FROM THE NR 2 ENGINE. THE CREW FOLLOWED UNUSUAL ENGINE VIBRATION PROCEDURES, SHUTDOWN ENGINE, DECLARED AN EMERGENCY. LANDED WITHOUT ADDITIONAL COMPLICATION . THE CREW REPORTED NO OTHER ABNORMAL ISDR 2012F00107Engine · making metalEICAS MESSAGE FOR RT OIL FILTER. DISPLAY REMAINED WHEN THRUST REDUCED. RT ENGINE SHUTDOWN. ENGINE VIBRATION DURING CLIMB. DURING INSPECTION FOUND DEBRI IN ALL MAGNETIC CHIP DETECTORS. ENGINE REPLACED.SDR KY7A2012061300001Engine · failedAFTER TAKEOFF, FIRST OFFICER CONFIGURED ACFT FOR CLIMB. SECOND OFFICER NOTICED SPLIT IN TORQUE INDICATION, SHORTLY FOLLOWED BY LOSS OF ENGINE POWER. SHUTDOWN ENGINE. DECLARED EMERGENCY AND RETURNED TO DEPARTURE AND MADE SAFE LANDING. MX R & R NR 1 ENGINESDR CA120619005Engine · flamed out(CAN) DURING A TRAINING FLIGHT WHILE SIMULATING AN ENGINE OUT & DURING FINAL APPROACH, THE OTHER ENGINE FLAMED OUT. AN UNEVENTFUL LANDING FOLLOWED. TROUBLESHOOTING IS ONGOING.SDR CA120619006Unknown · haze(CAN) DURING CLIMB, A SMOKE MIST ENTERED THE CABIN, ENG BLEEDS WERE SHUT OFF & THE ACFT WAS RETURNED TO THE DEPARTURE POINT, WHERE AN UNEVENTFUL LANDING WAS MADE. ENGINE REPLACED.SDR CA120619002Engine · fire warning(CAN) DURING REVENUE FLIGHT WHILE THE ACFT WAS IN CLIMB, THE ENG 2 FIRE ALERT ILLUMINATED. THE PILOT RELEASED BOTH FIRE AGENT BOTTLES WITHOUT STOPPING THE ALERT. THE ENG WAS SHUT DOWN & THE ACFT RETURNED TO THE AIRPORT OF DEPARTURE FOR AN UNEVENTFUL SINGLE ESDR UALA2012060803123Liner · crackedATTRITION LINER CRACKED 3 INCHES AND DELAMINATED AT 6:00 POSITION. NR 2 ENGINE ATTRITION LINER DAMAGE MEASURED FROM 5:30 TO 6:00 ABOUT 7.5 INCH BY 6 INCHES= 45 SQ INCHES FOR ABOUT 22 PERCENT DAMAGE. MORE DAMAGE FROM 6:00 TO 7:00 ABOUT 5.5 INCH BY 13 INCH, 5 SDR T8VA20120605001Engine · leakingON DESCENT FLIGHT CREW NOTICED THAT THE LEFT OIL PRESSURE GAUGE WAS GETTING INTO THE YELLOW ARCH AND A FEW MINUTES LATER THE OIL PRESSURE ANNUNCIATOR BEGAN TO FLICKER. PERFORMED PRECAUTIONARY ENGINE SHUTDOWN CHECKLIST TO AVOID DAMAGING THE ENGINE AND LANDED SDR MASA2012060534859Engine · contaminatedLAVATORY SMOKE WARNING AND ODOR IN FWD CABIN. FOUND TO BE DUE TO A PREVIOUS COMP WASH. CLEARED ACM'S.SDR HALA2012060500158Engine · making metalLT ENGINE HIGH VIBRATION, 6. METAL FOUND IN TAILPIPE. OPENSDR CA120619003Engine · making metal(CAN) WHILE POWERING UP FOR TAKEOFF, THE NR 1 ENG OIL PRESSURE & FADEC WARNINGS CAME ON WITH OIL PRESSURE INDICATING 0. THE TAKEOFF WAS ABORTED. POST EVENT INSPECTION FOUND HEAVY CONTAMINATION OF THE CHIP DETECTOR & OIL FILTER WITH METAL CHIPS. ENG IS BEINGSDR ASOA20120604051Engine · leakingCREW REPORTED SMOKE IN THE LAVATORY. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. ENGINE LEAKING, MX REPLACED THE NR 2 ENGINE. OPS CHECKED GOOD.SDR CA120626014Engine · malfunctioned(CAN) DURING T/O ROLL AROUND 50 TO 60 KT, THE CREW HEARD A NOISE, REFERRED TO AS A "BANG" FROM THE LT OF THE ACFT WITH CORRESPONDING MOMENTARY INCREASE IN ENGINE NR 1 TQ FROM 90 TO 93 THEN BACK TO 90 PERCENT IN ABOUT 1 SEC. NO ANOMALY IN ENGINE PARAMETERS NORSDR MHIA20120605001Engine · malfunctionedTHE AIRCRAFT WAS SCHEDULED FOR A CHARTER. WHILE TAXIING TO THE TAKEOFF SPOT BOTH PILOTS HEARD A LOUD NOISE COMING FROM THE NR 1 ENGINE FOLLOWED BY A CHIP LIGHT. THEY THEN SHUT THE ENGINES DOWN. THE ENGINE IS BEING FORWARDED TO THE ENGINE MANUFACTURER TO DETSDR PCSA2012060501Engine · power lossDURING CLIMBOUT THE NR 2 ENGINE LOSS POWER.SDR CA120618001Engine · making metal(CAN) ABORTED TAKEOFF DUE TO A LOW OIL PRESSURE WARNING. INSPECTION FOUND THAT THE OIL FILLER CAP HAD COME OFF. FURTHER INSPECTION FOUND DEBRIS ON BOTH MAGNETIC CHIP DETECTORS BEFORE & AFTER A PENALTY RUN. THE ACFT IS NOW GROUNDED. MFG WILL INVESTIGATE TO SDR ASAA2012062092391Warning Light · false activationRIGHT BLUE ENGINE VALVE CLOSED, LIGHT ILLUMINATED AFTER APPROX 1 HOUR AT CRUISE. ALL OTHER PARAMETERS APPEAR NORMAL. ACFT GROUNDED. PERFORMED EEC BITE TEST IAW MM TASK 73-00-00-810-801. NO DEFECTS NOTED. ACCOMPLISHED ENGINE RUN CHECK FOR 5 MINS IAW TASK 71SDR UALA2012060103043Vane · crackedNR 1 ENG FAILED BOROSCOPE. NR 1 ENG SN 727703 2ND STG VANE HAS A CRACK MORE THAN 50 % OF BLADE WIDTH ON CONVEX SIDE ON LOWER THIRD OF VANE. CRACK IS IN MIDDLE OF VANE AS VIEWED THRU AP11. RPL'D ESN 727703 WITH ESN 727888 IN POS 01 PER TOD AMM 71-00-02 CONFIG SDR UALA2012060103045Engine · vibrationVIBRATION FROM NR 1 ENG, FELT IN FLIGHT DECK. NEED TO ACP TAP TEST INSPECTION OF THE NR 1 ENGINE FAN BLADES. ACCOMPLISHED TAP TEST PER AMM. ALL BLADES HAVE AN ACCEPTABLE VALUE. ACP'D LP COMPRESSOR (FAN) ONE SHOT METHOD TRIM BALANCE PER MM. OPERATIONAL TESSDR FDEA201205312025Tube · crackedDURING CLIMB, PERFORMANCE WAS SUBSTANDARD. RETURNED TO DEPARTURE. INSPECTION FOUND TUBE FROM P1 PROBE TO COWLING BROKEN OFF. ADEL CLAMP THAT SECURES LINE TO THE INSIDE OF THE NOSE COWL WAS BROKEN ALSO.SDR SAJF201206141017Engine · failed(B-18721) DURING CLIMB, EICAS MESSAGE "ENG 4 OIL PRESS" WITH OIL PRESSURE INDICATING 4 PSI, FOLLOWED QRH, ENGINE 4 SET TO IDLE, SHORTLY NOISE AND VIBRATION, THEN N1,N2 DROP, EICAS MESSAGE "ENG 4 FAIL", FOLLOW QRH ENG SHUTDOWN. GROUND CHECK FOUND METAL CHIPS SDR UALA2012052903023Engine · hung startNUMBER 2 ENGINE HUNG START ON TWO ATTEMPTS. ATTEMPTED SECOND START WITH BOTH IGNITIONS ENGINE START PARAMETERS NORMAL, STARTS OKAY.SDR SIMA20120528004Engine · smokeFLIGHT 3282, DURING POST FLIGHT, FOUND SMOKE COMING FRONT NR 1 ENGINE (FRONT AND BACK). AIRCRAFT REMOVED FROM SERVICE. PERFORMED VISUAL INSPECTION ON NR 1 ENGINE AND DID NOT FIND ANY OIL INLET, EXHAUST AREA FLIGHT CREW PERFORMED ENGINE RUNS NO SMOKE AT SHUTSDR 29GA95571052712AEngine · malfunctionedFLIGHT: RIGHT ENGINE OIL PRESSURE ILLUMINATED IN FLIGHT ON APPROACH ASSOCIATED SMELL OF SMOKE IN CABIN AND COCKPIT. ENGINE SECURED AND EMERGENCY DECLARED. REPLACED RIGHT ENGINE ASSEMBLY.SDR AALA20120527007Engine · failedMCO - INFLIGHT JFK-MIA. CREW REPORTED RIGHT "OIL FILTER" EICAS MESSAGE WHICH DID NOT EXTINGUISH WITH POWER REDUCTION. CREW SHUT DOWN RIGHT ENGINE (SINGLE ENGINE TIME 25 MINS). EMERGENCY DECLARED FLIGHT DIVERTED MCO LANDED WITHOUT INCIDENT. AIRCRAFT REMOVEDSDR SIMA20120527009Engine · smokeFLIGHT 3422, CREW REPORTED NR 1 PACK CREATED SMOKE, HAZE AND AN ODOR WHEN TURNED ON. AIRCRAFT REMOVED FROM SERVICE. RAN BOTH ENGINES IAW AMM 71-00-01. DID NOT DETECT SMOKE ODOR AND SAW NO HAZE USING EITHER PACK UNIT. NO PARTS REMOVED OR REPLACED. OPS CHECKSDR QMLA2012052712088Engine · making metalDURING LANDING, THE NR 1 ENGINE CHIP LIGHT ILLUMINATED AS THE COLLECTIVE WAS PLACED FULL DOWN AFTER LANDING. EXCESS CHIPS WERE FOUND ON CHIP DETECTOR AND MX DETERMINED ENGINE MUST BE REPLACED.SDR CA120606001Engine · shutdown(CAN) DURING APPROACH ON THE DOWNWIND LEG AT 500 FT AGL, THE ENGINE SHUT ITSELF DOWN WITH NO PRIOR WARNING. THE PILOT MADE A FORCED LANDING IN A FIELD. THE ACFT SUFFERED SIGNIFICANT DAMAGE TO THE PROPELLER AND NOSE GEAR.SDR DALA1234050967Engine · failedCREW DIVERTED TO IAD FOLLOWING THE FAILURE OF THE RIGHT ENGINE DURING CLIMB TO FL30. THE FLIGHT CREW REPORTED HEARING A LOUD BANG AND THEN EXPERIENCED FEELING A JOLT & SHUDDER CULMINATING WITH THE LOSS OF POWER IN THE RIGHT ENGINE. MAINTENANCE FOUND METAL INSDR AALA20120526002Engine · malfunctionedTUL - INFLIGHT DFW-STL. CREW REPORTED LEFT ENGINE OIL PRESSURE LOSS IN FLIGHT. EMERGENCY DECLARED FLIGHT DIVERTED TUL LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT TUL ON 05/26/2012. SYSTEM GROUND CHECK NORMAL OPERATION.SDR SIMA20120525001Oil System · overservicedFLIGHT 3969, CREW REPORTED A FAINT ODOR OF UNBURNED OIL IN COCKPIT AND CABIN, DURING CLIMB AND DESCENT FOR SHORT PERIODS OF TIME. AIRCAFT REMOVED FROM SERVICE. FUNCTIONAL CHECK FLIGHT FOUND TO BE SATISFACTORY. PERFORMED OPERATIONAL CHECK OF LEFT AND RIGHT SDR CA120525005Switch · failed(CAN) IT WAS REPORTED THAT WHILE IN LEVEL CRUISE FLIGHT AT 41,000 FT, THE LT ENGINE BEGAN SPOOLING DOWN JUST AS THE LT FADEC FAIL MESSAGE APPEARED, AND THE ENGINE SUBSEQUENTLY SHUTDOWN. THE CREW DIVERTED THE ACFT AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PESDR UALA2012052402919Engine · stalledNR 2 ENGINE STALL. REPLACED PRECOOLER Y DUCT ON NR 2 ENG. NR 2 FEC, REPAIR OR REPLACED THE AFT PYLON, PYLON TO REVERSER 'L' SEAL ON THE LT SIDE ACCT DAMAGED. REPLACED NR 2 ENG PYLON TO REVERSER "L" SEAL ON LEFT SIDE. REPLACED NR 2 ENGINE.SDR HALA2012052300146Engine · warning lightLT ENGINE SYS FAIL MESSAGE. REMOVED AND REPLACED NR 1 ENGINE IAW M144-717. ENGINE RUN OK. OK FOR SERVICE.SDR CA120605002Engine · overheated(CAN) FOLLOWING TROUBLESHOOTING, OF UNKNOWN NATURE, FOR A CHIP DETECTOR WARNING PERFORMED BY A LOCAL FBO, THE ACFT WAS RELEASED TO SERVICE. ON THE 1ST FLIGHT FOLLOWING, THE CREW RECEIVED AN ENGINE TEMPERATURE EXCEEDANCE WARNING ACCOMPANIED BY HIGH VIBRATIONS.SDR HYIA2012052200001Engine · power lossRT ENGINE LOST POWER, VIBRATED SUDDENLY. INSPECTED ENGINE, CHECKED PARAMETERS, PERFORMED COMPRESSION CHECK, ADJUSTED IDLE FUEL MIXTURE, CHECKED RT WING TANK SUMP FOR WATER, PERFORMED RUN UP, COULD NOT DUPLICATE, FCF CHECKS GOOD.SDR AALA20120522024Engine · bird ingestionVVI - CREW REPORTED LEFT ENGINE INGESTED MEDIUM SIZE BIRD. EMERGENCY DECLARED, FLIGHT RETURNED VVI LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT MIA ON 05/26/2012. SYSTEM GROUND CHECK NORMAL OPERATION.SDR ASMF201205009Engine · making metalCAPTAIN REPORTED THAT DURING APPROACH, THE RT ENGINE OIL FILTER BY PASS LIGHT TURNED ON, SO FLIGHT CREW ACCOMPLISHED THE QRH 7.22 PROCEDURE, CONFIRMING THE FAILURE AND ACFT CONTINUES TO LANDING. DURING MX REVISION, THERE WERE DETECTED METAL CHIPS IN THE MAIN SDR AALA20120520006Engine · failedRDU - CREW REPORTED DURING CLIMBOUT LEFT ENGINE OIL PRESSURE INDICATION WENT TO ZERO. PERFORMED IN-FLIGHT SHUTDOWN OF LEFT ENGINE (SINGLE ENGINE TIME 24 MINS). EMERGENCY DECLARED FLIGHT RETURNED RDU LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. RSDR CA120523016Engine · malfunctioned(CAN) ACFT WAS INVOLVED IN LONGLINE OPERATIONS. DURING A MOVE WITH LOAD ON HEADING FOR THE LANDING ZONE UNDER LOW POWER AS THE PILOT BEGAN TO SLOWLY PULL IN POWER TO SLOW THE DECENT A POPPING NOISE WAS HEARD AND A RISE IN THE ITT WAS NOTED ON THE NR 1 ENGINE SDR WX0A071207Engine · malfunctionedFLIGHT CREW PERSONNEL REPORTED THAT DURING CLIMBOUT AT APPROX FL270, LEFT ENGINE COMPRESSOR STALL/ ENGINE PARAMETERS ROLLED BACK ENGINE SHUTDOWN PER CHECKLIST. MAINTENANCE PERSONNEL REPLACED THE LEFT ENGINE IAW TASK CARD R0807101, OPS AND LEAK GOOD. AIRCRAFTSDR CA120524007Engine · failed(CAN) AFTER DEPARTING, SMOKE IN THE CABIN OCCURRED AND THE CREW ELECTED TO RETURN TO THE DEPARTURE AIRPORT. ON SHORT FINAL, THE NR 2 ENGINE LOST POWER FOLLOWING A LOUD MECHANICAL SOUND. DURING THE SUBSEQUENT SINGLE ENGINE LANDING, CONTROL WAS LOST AND THE ACSDR ASMF201205008Skin · damagedDURING TRANSIT CHECK WAS DETECTED A LIGHTNING STRIKE IN RT ENGINE. MX PERSONNEL PERFORMED A LIGHTNING STRIKE CONDITIONAL INSPECTION IAW MM 05-51-19, FOUND DAMAGES WITHIN LIMITS.SDR CA120517003Engine · overtemp(CAN) NR 2 ENGINE ITT SHOW UP IN RED 798 DEGREE , FOLLOWED BY A SHUDDERED WITH A LOUD BANG. ENGINE WOULD NOT RESPONSIVE TO THROTTLE ADVANCE IAW QRH, RETURN TO IDLE AND SHUTDOWN.SDR UALA2012051602781Engine · stalledSTALL DISPLAYED ON UPPER ECAM SCREEN DURING POWER DECELERATION. REMOVED PLUGS "B" AND "C" AND DRIVE PAD COVER, COMPLETED BORO OF HPC STG 3 AND 6 NO DAMAGE NOTED. REPLACED 7B SOLENOID VALVE, AND HPC 7TH STAGE BLEED VALVE DUE TO FAILED FUNCTIONAL TEST.SDR REXA2012051500744Engine · malfunctionedFLT 4147 CVG-PHL HAD ITT ON NR 2 ENGINE RISE CREW HEARD LOUD BANG AND A/C STARTED SHAKING. CREW FOLLOWED QRH PROCEDURES SHUT DOWN NR 2 ENG AND RETURNED TO CVG. CREW DID DECLARE EMERGENCY. MX ONSITE INSPECTED OUTSIDE OF ENGINE NO DEFECTS FOUND. PERFORMED DFSDR SIMA20120515006Frame · corrodedDURING MAINTENANCE INSPECTION FOUND THE RIGHT ENGINE FRONT FRAME FORWARD FLANGE HAS MULTIPLE ENLARGED FLANGE HOLES DUE TO EXCESIVE CORROSION. ENGINE REQUIRES CHANGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT ENGINE IAW W/C 71-000SDR CA120606002Engine · fire(CAN) DURING CRUISE AT FL270, WHILE SIMULATING AN "ENGINE OUT" TO THE F/O, THE PILOT PULLED THE CONDITION LEVER BACK TO IDLE AND MOVED THE PROPELLER LEVER BACK TO THE DETENT TO SIMULATE ZERO THRUST. ALTER THE SIMULATION, UPON PUSHING THE PROPELLER LEVER FORWA
Back to JASC 7200