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 CALA050110Engine · failedON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE.SDR CA050420004Engine · failed(CAN) CLIMBING THROUGH APPROX 17,000' AT 320 KIAS, WITHOUT WARNING, A BANG WHICH CAUSED ACFT TO SHUDDER FOLLOWED BY VIBRATION & A HOWLING NOISE NR 2 ENG VIBRATION INDICATOR READING IN EXCESS OF 2 UNITS, EGT & OIL TEMP STARTED TO RISE, & ALSO A DROP IN EPR. ACSDR JBGA20050002Engine · flamed outENGINE FLAME OUT FOLLOWED BY AMBER ENGINE LIGHT. ENGINE RELIGHT NORMAL. ENGINE CONTINUED OPERATION NORMAL.SDR CA050429006Engine · shutdownDURING CRUISE, THE PILOT NOTICED OIL SMELL IN THE CABIN ACCOMPANIED BY DECREASING ENGINE OIL PRESSURE. THE PILOT DECLARED AN EMERGENCY AND COMPLETED AN UNSCHEDULED LANDING. FOLLOWING LANDING POWER COULD NOT BE MODULATED AND THE ENGINE WAS SHUT DOWN. SUBSEQUSDR SIMA200510805Engine · malfunctionedFLT 4014 - CREW NOTED, SEEING THE OIL PRESSURE STARTING TO DROP AND THEN THE E1 SHUTDOWN. DECLARED AN EMERGENCY AND LANDED SAFELY. REPLACED NR 1 ENGINE IAW WC 72-000-00. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CHQA200500082Engine · failedDURING LATE STAGES OF CLIMB, AT APPROX 24500 FT., NOTICED A SPIKE IN NR 2 ITT OF 911 C. FOR 1 SEC. REDUCED THRUST ON NR 2, ITT RETURNED TO GREEN RANGE. LEVELED OFF AT FL260 & SET TO CRUISE. SET POWER TO SAME N1 TO ALLOW CHK OF ENG PARAMS. BOTH N1 SETTINGS 80.5SDR 2005FA0000779Engine · leakingENGINE EXPERIENCED LOW OIL PRESSURE IN FLIGHT. PRECAUTIONARY SHUTDOWN PERFORMED. 23 PSI LOWEST READING ON OIL PRESSURE INDICATOR. OIL PRESSURE NEVER WENT TO -0- PSI. NO ABNORMAL VIBRATION EXPERIENCED. PRECAUTIONARY SHUTDOWN PERFORMED ON NR 2 ENGINE. EMERSDR CA050419006Engine · failed(CAN) DURING CRUISE, THE ENGINE EXHIBITED A LOUD NOISE ACCOMPANIED BY A LOSS OF POWER. THE AIRCRAFT DIVERTED AND A DEAD-STICK LANDING WAS ACCOMPLISHED. INITIAL INVESTIGATION REVEALED A FRACTURED REDUCTION GEARBOX HOUSING AND POWER TURBINE BLADES WITH LOSS OSDR UPS05844270Engine · flamed outNR 4 ENGINE FLAME OUT IN CRUISE FLT ENROUTE TO PHL. RESTART UNSUCCESSFUL. FUEL PRESSURE ON S/O PANEL DROPPED FROM 35 PSI TO 20 OIL TEMP & QTY NORMAL OIL PRESS DROPPED TO 18 PSI AFTER FLAMEOUT. R&R NR 4 ENGINE, MAIN ENGINE CONTROL (MEC) IAW MM 73-20-01-4. PERFSDR T48R20050007Turbine · separatedENGINE WAS REMOVED FROM N827NK NR 2 POSITION FOR IN FLIGHT SHUTDOWN. DISASSEMBLY AND INSPECTION REVEALED EVIDENCE OF A POSSIBLE INTERNAL OIL FIRE RESULTING IN THE HIGH PRESSURE TURBINE SHAFT FRACTURING. THE REAR TURBINE SECTION WAS SEVERELY DAMAGED WITH NO PSDR DL76L050212Engine · making metalNR 2 ENGINE REPLACED DUE METAL FOUND IN NR 3 MCD.SDR AU510001965Engine · bird ingestionNR 1 ENGINE BIRDSTRIKE. INVESTIGATION FOUND THE REMAINS OF THREE FLYING FOXES. THOROUGH INSPECTION OF THE ENGINE FOUND NO OBVIOUS DEFECTS. A WATER WASH WAS CARRIED OUT AND THE AIRCRAFT RELEASED TO SERVICE.SDR AU510001958Engine · shutdown(AUS) RT ENGINE PARAMETERS DECREASED AND ENGINE SHUTDOWN. EXTENSIVE INVESTIGATION COULD FIND NO CAUSE FOR THE SHUTDOWN. THE AIRCRAFT WAS RETURNED TO SERVICE AND HAS OPERATED WITHOUT FURTHER INCIDENT. (OTHER CAUSE: UNKNOWN ) (CASA NR 510001958)SDR 2005F00080Engine · failedWHILE TAXIING, THE RIGHT ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED. ALSO, SMOKE CAME OUT OF THE ENGINE. AIRCRAFT RETURNED TO BLOCKS. REPLACED RIGHT ENGINE ASSY. ENGINE SENT FOR INSPECTION AND EVALUATION. (M)SDR CA050422001Engine · failed(CAN) AFTER TAKEOFF ON CLIMB OUT THE CREW HEARD A LOUD BANG AND THE RT TGT ROSE QUICKLY. THE TOWER REPORTED FIRE FROM THE TAIL OF THE AIRCRAFT. THE CREW EXECUTED THE ENGINE FIRE CHECKLIST AND RETURNED TO THE AIRPORT AND PERFORMED A SINGLE ENGINE LANDING. ENGSDR 2005UALA00322Engine · shutdownRETURNED TO FIELD DUE TO NR 2 ENGINE SHUTDOWN. THE ENGINE EXPERIENCED A SURGE IN THE HPC AND WAS SHUTDOWN. THE ENGINE SURGE WAS CAUSED BY A DISRUPTION IN AIRFLOW THROUGH THE HPC THAT WAS CAUSED BY DAMAGE TO THE COMPRESSOR AIRFOILS. THE AIRFOIL DAMAGE WAS CAUSSDR DJFA2005077Engine · failedKMIA TRIP ID NR 812480, CREW REPORTED THAT THE RIGHT ENGINE FAILED WITH A VERY LOUD BANG SHORTLY AFTER THE GEAR WAS RETRACTED. A SEVERE SHUTTER WAS FELT THROUGHOUT THE AIRCRAFT AFTER THE ENGINE FAILURE. THE RIGHT FIRE HANDLE WAS PULLED AND THE NR 1 EXTINGUISSDR MWEA050031Engine · failedCREW HEARD A LOUD NOISE FROM THE LEFT SIDE AND NOTED POWER LOSS AND OIL PRESSURE ON THE NUMBER ONE ENGINE. REMOVED AND REPLACED LEFT ENGINE.SDR C2XA05IA053Engine · failedOKC - FLIGHT 3453, THE CREW REPORTED AN ENGINE NR 1 INFLIGHT FAILURE, LOUD BANG FOLLOWED BY UNCOMMANDED SHUTDOWN. THE AIRCRAFT RETURNED TO OKC WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER ONE ENGINE, OPERATIONALLY CHECKED WITSDR CA050527011Engine · failedDURING TAKEOFF ROLL, THE ENGINE CHIP DETECTOR ANNUNCIATED. THE TAKEOFF WAS ABORTED AND THE ENGINE WAS SHUT DOWN. SUBSEQUENT INSPECTION REVEALED HOT SECTION DAMAGE INCLUDING DISTRESSED COMPRESSOR TURBINE AND POWER TURBINE BLADESSDR 20054Engine · malfunctionedDURING FLIGHT AT CRUISE ALT 14,000 FT, A SHARP JOLT/POP WAS FELT WITH AN ASSOCIATED YAW TO THE RT. ALL ENGINE INDICATORS APPEARED NORMAL. DURING DESCENT TO LANDING, AS POWER LEVERS PULLED BACK AN ABNORMAL FAINT "WHINING" WAS HEARD. DURING TAXI TO GATE IN FLSDR A6WA200540147Check Valve · stickingLOW OIL ENGINE PRESSURE WARNING IN FLIGHT (RED). INDICATED LOW ON GAUGE LOW PRESSURE, COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. REMOVED AND REPLACED ENGINE NR 2 GEARBOX BB CARBON SEAL AND MATING RING. ALSO, REMOVED AND REPLACED ENGINE NR 2 REPLENISHMENTSDR MALA050313Engine · fluctuatesAC DID AN AIR RETURN DUE TO LT ENGINE TORQUE FLUX.SDR ANCF200400046Blade · damagedDURING OVERNIGHT SERVICE WAS ACCOMPLISHED EO 83-72-007 BORESCOPE INSPECTION FIRST AND SECOND STAGE TURBINE BLADES AND FOUND ON RT ENGINE TWO BLADES WITH CRACKS ON TRAILING EDGE CONCAVE SIDE OF FIRST STAGE TURBINE. THE ENGINE HAS BEEN REMOVED IAW AMM 72-00-00,SDR COMA0560230Engine · out of toleranceFLIGHT 5267 DURING CLIMBOUT OF CVG THE RIGHT ENGINE WOULD NOT ACHIEVE CHARTED RATED THRUST. AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. REPLACED THE RIGHT ENGINE ASSEMBLY.SDR CA050419007Engine · malfunctioned(CAN) DURING A MAINTENANCE FLIGHT, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. THE PILOT WAS UNABLE TO MODULATE POWER AND SUBSEQUENTLY SUCCESSFULLY EJECTED FROM THE AIRCRAFT. MFG WILL MONITOR THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF RSDR 2005FA0000587Engine · destroyedAFTER TAKE-OFF THE LT ENGINE SUFFERED A CATASTROPHIC FAILURE. TWO CONNECTING RODS (NR 5, 6) FAILED AND KNOCKED A HOLE IN THE CRANKCASE. THE RESULTING HOLE IN THE CRANKCASE WAS THE LOCATION OF A FIRE WHICH BURNED THROUGH THE COWLING AND CONTINUED BURNING. THE SDR MALA050311Engine · malfunctionedLT ENGINE OIL PRESSURE LIGHT ILLUMINATED AND GAUGE WAS READING LOW (ABOUT 25-30 PSI) ON TAKEOFF. CREW FOLLOWED QRH BUT DID NOT SHUT DOWN ENGINE. AIR RETURNED. REMOVED AND REPLACED LT ENGINE.SDR ZN3R425038Bearing · fracturedENGINE RETURNED TO SERVICE CENTER FOLLOWING COMMANDED SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE. DURING INSPECTION A FRACTURED CAGE AND OUTER RACE WAS FOUND ON A FORWARD PLANETARY ROLLER BEARING.SDR 2005FA0000599Bearing Race · fracturedENGINE RETURNED TO SERVICE CENTER FOLLOWING COMMANDED SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE. DURING INSPECTION A FRACTURED CAGE AND OUTER RACE WAS FOUND ON A FORWARD PLANETARY ROLLER BEARING.SDR 20053Engine · malfunctionedAFTER T/O APPROX 500FT AGL, NR 2 ENGINE TQ DROPPED TO 11 PERCENT, ALL OTHER INSTRUMENTS INDICATING NORMAL. ENGINE BEGAN TO SURGING AND UNABLE TO CONTROL WITH THRUST LEVERS. COMMENCED WITH ENGINE SHUTDOWN PROCEDURES. DECLARED EMERGENCY WITH APPROACH. LEVELESDR CA050401005Engine · making metal(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED REDUCTION IN POWER FOLLOWING TAKE-OFF. THE FLIGHT DIVERTED TO POINT OF ORIGIN. DURING SUBSEQUENT TROUBLESHOOTING, THE CHIP DETECTOR WARNING ANNUNCIATED AND METAL PARTICLES WERE FOUND ON THE DETECTOR. MFG WILL MONISDR ASOA05270Engine · malfunctionedDURING CRUISE, THE CREW NOTICED LT ENGINE ITT RISE IN EXCESS OF 800 DEGREES ITT AND REDUCED THE POWER ON THE ENGINE TO BRING IT WITHIN ITT LIMITS AT WHICH TIME THE ENGINE BEGAN TO SURGE. AN EMERGENCY WAS DECLARED AND JUST PRIOR TO THE CREW SHUTTING DOWN THE LSDR CHQA200500065Engine · failedCLIMBING, BOOM HEARD FROM RT SIDE OF A/C. LOOKED AT INSTRU ON NR 2, ITT TO RED. THRUST LEVER TO IDLE. ENG 2 OUT ON EICAS & DECLARED EMERGENCY. PROCEEDED W/E-2 OUT ABNORM CHKLST. ENG SHUTDOWN CHKLST. DISPATCH CONTACTED & DIVERT TO KBDL. CHKD ENG INSTS, & SDR SIMA200509114Carbon Seal · leakingCREW REPORTED SMOKE AND FUMES IN CABIN. FOUND OIL LEAKING FROM NR 2 ENGINE CARBON SEAL. REPLACED NR 2 ENGINE IAW WC. OPS CHECK GOOD, AC RETURNED TO SERVICE. (SW21200504808) (K)SDR 20052Engine · fodRIGHT ENGINE MADE POPPING NOISE DURING CRUISE AND INDICATED TORQUE FLUCTUATION AND SLIGHT VIBRATION. NO OTHER LIGHTS OR INDICATIONS WERE OBSERVED. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW AIA FORM M-105. OPS AND LEAK CHECK GOOD.SDR CA050329015Safety Valve · broken(CAN) AERONAUTICAL ACCESSORIES PC SAFETY VALVE KIT, STC SE327AT, STA SE93-4. UPON REMOVAL FOR OVERHAUL THE ACTUATING KNOB WAS FOUND SHEARED AND HELD IN PLACE BY THE RETAINING CLIP. THE KNOB WOULD NOT HAVE FALLEN HOWEVER THE VALVE ITSELF WAS NO LONGER HELD IN SDR IXXA0500025OEngine · flamed outON CLIMB NR 3 ENG FLAMED OUT 32,000 FT, NO AUDIBLE/VISUAL ENG STALL OR VIBRATION. WEATHER VMC THROUGHOUT CLIMB. ENG FLAMED OUT N1 30%, N2 15% & OIL PRESSURE 3 PSI. GEN WENT OFF LINE, IGNITION NOT ON. FUEL CONFIG NORMAL, FUEL TEMP TANK -5C & FUEL PRESSURE ASDR DXTA200500640Engine · malfunctionedAFTER APPLYING TAKEOFF POWER, RIGHT EEC REVERTED TO MANUAL MODE, ABORTED TAKEOFF. ITEM IS UNDER INVESTIGATION.SDR MALA050287Engine · leakingIN CRUISE MEM - JAX 24,000 FT THICK HEAVY SMOKE (PETROLEUM BASE ODOR) IN THE FLIGHT DECK/CABIN. NO WARNINGS IN THE FLIGHT DECK LEADING UP TO THE EVENT. EMERGENCY DECLARED AND FLIGHT 3632 DIVERTED TO ASN. LANDED WITHOUT FURTHER INCIDENT. POST FLIGHT CREW NOSDR AALA20050207Engine · overtempPHL - INFLIGHT LEFT ENGINE FAILURE ON TAKEOFF. ENGINE HAD LARGE VIBRATION FOLLOWED BY WHAT FELT LIKE SEIZURE. ENGINE GENERATOR TEMPERATURE 975C. REPORTS OF FIRE AND SMOKE BY AIR TRAFFIC CONTROL, OTHER AIRCRAFT AND PASSENGERS. NO FIRE WARNING. ENGINE SHUTDSDR DLM88050174Engine · leakingON CLIMB JUST AFTER TAKEOFF BOTH AFT LAV SMOKE DETECTORS SOUNDED FOLLOWED BY VISIBLE SMOKE IN THE CABIN. REPLACED RT ENGINE FOR INTERNAL OIL LEAKAGE.SDR ANCF200400043Engine · bird ingestionDURING ROTATION THE RT ENGINE WAS IMPACTED WITH A BIRD. ALL ENGINE PARAMETERS WENT DOWN TO IDLE AND RETURNED SLOWLY TO NORMAL PARAMETERS IAW AMM 05-51-08 PAGE 601 BIRD STRIKE CONDITION. CHECK WAS ACCOMPLISHED AND NOT FOUND DAMAGE IN THE ENGINE AREAS.SDR GTIA050074Engine · vibrationNR 1 ENGINE HAS VIBRATION AT IDLE ON GROUND AND IN FLIGHT, AIRCRAFT TAIL SWAP WITH 819NK. PERFORMED ENGINE VIBRATION TEST ON NR 1 ENGINE AND NO DEFECTS NOTED, WITHIN LIMITS. INSPECTED INLET AND EXHAUST AREAS, INSPECTED CSD, GEAR BOX MAG PLUGS AND OIL FILTER,SDR WRNA200500006Engine · unserviceableDURING CLIMBOUT NR 2 ENGINE EXCEEDED EGT LIMITS. WHEN LIMITS WERE IN NORM OPERATING RANGE NO RESPONSE WAS SEEN WHEN THROTTLES WERE ADVANCED. FUEL DUMP PROCEDURES FOLLOWED, AIRCRAFT RETURNED TO AIRPORT, LANDING NORMAL. REMOVED AND REPLACED NR 2 ENGINE IAW A3SDR CA050329008Engine · malfunctioned(CAN) THE ENGINE WAS REPORTED TO HAVE LOST POWER IN CRUISE. DURING TAKE-OFF ROLL ON A PREVIOUS FLIGHT, THE ENGINE DID NOT REPOND TO THROTTLE INPUT. MFG WILL MONITOR THE INVESTIGATION OF THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR CA050323002Engine · out of limits(CAN) THE ENGINE HAS BEEN INSTALLED AFTER OVERHAUL, AND ON GROUND RUN HIGH VIBRATION ON THE FORWARD POINT WITHIN LIMIT BUT ABNORMALLY HIGH. AFTER CONTACTING THE OVERHAUL FACILITIES, WE DID SOME TESTS FOR RESULT. THE VIBRATION WENT UP CLOSER TO THE LIMIT. AFTESDR CA050527010Engine · failedTHE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED GRINDING NOISES FROM THE POWER SECTION. THE ENGINE WAS REMOVED FOR REPAIR.SDR CA050329009Engine · malfunctioned(CAN) DURING CRUISE THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN. THE FUEL CONTROL (MFC) AND FUEL PUMP WERE REMOVED FOR INVESTIGATION. MFG WILL MONITOR THE INVESTIGATION OF THIS EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR C1HA200593002Engine · overtempON TAKEOFF AFTER V1 THE NUMBER 1 ENGINE HAD SEVERE FLUCTUATIONS IN ALL INSTRUMENTS WITH VIBRATIONS ON NUMBER ONE SIDE. HEARD THREE LOUD POPS NR 1 EGT WENT TO 700 DEGREES C, THREE DIFFERENT TIMES IN RAPID SUCCESSION. DUMPED FUEL RETURNED FOR LANDING. FOLLOWE
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