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 YYFA20140313002Engine · power lossRIGHT ENG LOW N2 RPM INDICATION ON START, RETURNED TO GATE.SDR CA140326009Blade · damaged(CAN) CUSTOMER REPORTED NOISE FROM RT ENGINE IN TRANSIENT FROM CLIMB TO CRUISE, APPROXIMATELY 15 MINUTES INTO FLIGHT, AND WITH A LOSS OF POWER. PILOT INDUCED THE IFSD FOLLOWED BY ACFT RETURNING TO AIRPORT AND PERFORMED UNEVENTFUL SINGLE ENGINE LANDING. ON GROSDR YTRA20140313001Engine · making metalTHE PILOT MADE A PRECAUTIONARY LANDING DUE TO AN ENG CHIP LIGHT ILLUMINATION.SDR ASAA2014031207133Spinner · out of balanceNR 2 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAT NORMAL. ACFT GROUNDED. ENTERED WEIGHT SOLUTION ONTO REAR SPINNER IAW MM 71-00-75-808. ENTERED WT. LOCATION INTO AAVM. LOC. 29 & 34 REMOVED P12'S INSTSALLED P09'S AT SDR CA140326004Engine · malfunctioned(CAN) DURING LANDING, AFTER THRUST REVERSER DEPLOYMENT, ONE ENGINE DROPPED BELOW IDLE SPEED WITH INCREASING ITT INDICATION. THE PILOT ELECTED TO SHUTDOWN THE ENGINE AND TAXIED TO THE RAMP WITHOUT FURTHER INCIDENT. SUBSEQUENTLY THE ENGINE WOULD NOT START. TROUSDR CA140314006Engine · faultedDURING FLIGHT, THE PILOT REPORTED AN ELECTRONIC ENGINE CONTROL FAULT. THE ENGINE WAS FLOWN IN MANUAL MODE AND SUBSEQUENT INTERMITTENT FIRE ALARMS OCCURRED. THE ACFT LANDED SAFELY. POST FLIGHT INSPECTION FOUND EVIDENCE OF BURNING ON THE ENGINE.SDR CA140306001Engine · fire(CAN) REPORTED THAT WHEN BEGINNING DESCENT AN ORANGE GLOW WAS SEEN COMING FROM THE ENGINE. THE ENGINE FIRE LIGHT ILLUMINATED AND THE ENGINE WAS SHUTDOWN. THE FIRE LIGHT WENT OUT UPON SHUTDOWN AND THE FIRE BOTTLE WAS NOT DISCHARGED.SDR ASMF201403013Engine · failedCAPTAIN REPORTED THAT DURING LANDING, THE RT ENGINE PRESENTED LOW OIL QTY, SO FLIGHT CREW IMMEDIATELY PERFORMED THE RT ENGINE SHUTDOWN & ACCOMPLISHED THE QRH 7.21 PROCEDURE. REPLACED THE RT ENGINE IAW MM 71-00-02 & OPS TEST WAS PERFORMED IAW MM 71-00-00, TESTSDR CA140314009Engine · making metal(CAN) DURING FLIGHT, THE CHIP DETECTOR WARNING CAME ON ACCOMPANIED BY INCREASE IN OIL TEMPERATURE AND REDUCTION IN PRESSURE. THE PILOT ELECTED TO SHUT THE ENGINE DOWN BEFORE MAKING AN UNEVENTFUL SINGLE ENGINE LANDING. POST FLIGHT INSPECTION FOUND THE MAIN OILSDR CA140314008Engine · malfunctionedDURING FLIGHT, THE NR 1 ENGINE POWER COULD NOT BE REDUCED BELOW 98 PERCENT. THE PILOT WAS FORCED TO SHUT THE ENGINE DOWN BEFORE PERFORMING A SINGLE ENGINE LANDING. POST FLIGHT RESTART ATTEMPT OF THE ENGINE RESULTED IN A RAPID INCREASE TO 60 PERCENT AND THE STSDR CA140314007Engine · malfunctionedWHEN BRINGING POWER UP FOR TAKEOFF, 2 LOUD NOISES WERE HEARD FROM THE LT ENGINE. THE TAKEOFF WAS ABORTED. THE PILOT ATTEMPTED POWERING UP THE ENGINES AGAIN WITH THE SAME 2 LOUD NOISES OCCURRING. THE ACFT WAS SHUTDOWN AND RESTARTED AND BOTH ENGINES WERE PUT INSDR 39LA2014030561Engine · fluctuatesEN ROUTE DURING CRUISE FLIGHT BETWEEN OAMS & OAIX AT 13,500 FEET, THE FLIGHT CREW NOTICED THE TORQUE FLUCTUATED ON THE NR 1 ENG FROM 89% TO 110% NON-COMMANDED. AS A PRECAUTION, THE NR 1 ENG WAS SHUT DOWN. FLIGHT CREW DECLARED AN EMERGENCY & LANDED WITHOUT INSDR OLJ2014F00000Bearing · making metalENROUTE, NR 2 ENGINE CHIP LIGHT INDICATED ON THE MASTER CAUTION PANEL. ACFT ABORTED FLIGHT. AFTER LANDING, THE ACFT WAS TAKEN OUT OF SERVICE. A CHIP WAS FOUND ON THE ELECTRICAL PLUG. IT WAS WITHIN LIMITS IAW THE MM ONLY ACTION TAKEN WAS AN ENGINE DRAIN ANDSDR SWIA201436677Engine · vibrationAT FL 380, ROUGHLY 30 SECONDS AFTER REDUCING TL TO CRUISE SETTING A SIGNIFICANT VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. REPLACED LT ENGINE ASSY IAW AMM.SDR CA140314005Engine · malfunctionedDURING TAXI BEFORE TAKEOFF, THE NR 2 ENGINE WARNING CAME ON AND THE PILOT SAW TEMPERATURE DECREASING FOLLOWED BY QUICK INCREASE. IMMEDIATELY PULLED THE RT THROTTLE TO CUTOFF NOT KNOWING IF THE ENGINE WAS RE-LIGHTING OR IF THE TEMPERATURE WAS RUNNING AWAY. THE SDR CA140314003Engine · fluctuatesAFTER CLIMBING TO THEIR ASSIGNED ALTITUDE AT FL400 AND INCREASING SPEED TO MAX CRUISE, THE CREW HEARD 2 LOUD NOISES. AT THE SAME TIME THEY SAW THAT ENGINE 2 PARAMETERS WERE FLUCTUATING INCLUDING DECREASING ROTOR SPEED AND RAPID TEMPERATURE INCREASE. A TEMP EXSDR CA140314001Engine · flamed outTHE PILOT REPORTED THE NR 2 ENGINE FLAMED OUT WHEN TRANSITIONING FROM IDLE TO FLIGHT. A TECH OUTSIDE OF HELICOPTER ADVISED OF WHITE SMOKE FROM ENGINE EXHAUST AT THE MOMENT OF ENGINE FLAMEOUT. SUBSEQUENT TROUBLESHOOTING COULD NOT REPRODUCE THE PROBLEM.SDR A6WA201441219Engine · contaminatedCABIN & COCKPIT FILLED WITH SMOKE & FUMES ONCE BLEEDS WERE TRANSFERRED TO ENGINES.
SWAPPED BLEEDS BACK TO APU & SMOKE & FUMES STOPPED. CONTACTED MX & CONFIRMED THIS
WAS 1ST FLIGHT AFTER COMPRESSOR CLEANING. SUSPECT RESIDUAL CHEMICALS FROM COMPRESSOR WASH. RSDR DJFA20140302001Engine · failedDURING FLIGHT, AT 7000 FT MSL, LT ENGINE MADE AN AUDIBLE THUMP & ITT INCREASED TO APPROXIMATELY 800 DEGREES, N1 ROLLED BACK TO IDLE. POWER WAS REDUCED TO IDLE & ITT REDUCED TO APPROXIMATELY 500 DEGREES. AN EMERGENCY WAS DECLARED & ACFT RETURNED TO BASE. LSDR SIMA20140302001Engine · malfunctionedAFTER TAKEOFF AT 1500 FEET LAVATORY SMOKE WARNING ON EICAS. RETURNED TO KCMH. FLIGHT ATTENDANT REPORTED SMOKE IN LAST 3 ROWS. ACCOMPLISHED FIM ASK 21-20-00, FOUND SMALL AMOUNT OF DEICING FLUID AT NR 2 ENG AIR INLET. CLEANED AS REQUIRED, RUN ENG IAW ETN-EM-SDR DALA14014295810Engine · failedEXECUTED AN AIR RETURN AFTER A LT ENGINE STALL AND DECREASING PARAMETERS. MAINTENANCE FOUND METAL IN TAIL PIPE DURNING INSPECTION. ENGINE CHANGED.SDR ZP7A20140301001Engine · shutdownDURING DESCENT, AT 13,900 FT, EXPERIENCED A BRIEF LT ENGINE ROLLBACK. ALL IGNITERS AND PUMPS WERE ON AT THE TIME. RELIT ON ITS OWN, LEAVING THE LT BLEED AIR FAIL AND LT GEN FAIL WITH THE ASSOCIATED MASTER WARNING ANNUNCIATORS FLASHING. TURNED LT GENERATOR BSDR CA140302001Engine · flamed out(CAN) DURING TAXI MANEUVERS THE LT ENGINE FLAMED OUT. CONFIRMED COLD WEATHER, -31 CELSIUS, FLAMEOUT BEHAVIOR EXPERIENCED PREVIOUSLY.SDR CA140313006Engine · smokeACFT WAS ON TAXI PREPARING FOR TAKEOFF WHEN CONTROL TOWER CONTACTED THE PILOT TO ADVISE OF SIGNIFICANT SMOKE FROM LT ENGINE EXHAUST. PILOT SECURED ENGINE AND RETURNED TO FBO.SDR CA140314004Engine · malfunctionedTHE ACFT HAD A RUNWAY EXCURSION FOLLOWING WHAT THE PILOT DESCRIBED AS AN ENGINE RUNAWAY DURING LANDING AS HE WAS GOING IN REVERSE.SDR CA140326008Engine · warning light(CAN) THE HELICOPTER WAS PERFORMING A TRAINING FLIGHT WHEN FOLLOWING THE ILLUMINATION OF A CAUTION RELATED TO CHIP TRANSMISSION, PLANNED TO LAND, DURING THE FINAL PHASE A ROTOR RPM DROOP WAS REPORTED. THE HELICOPTER TOUCH THE GROUND AND CAME TO REST ONTO IT`S SDR ASOA20140226023Engine · contaminatedCREW REPORTED SMOKE IN COCKPIT IMMEDIATELY AFTER TAKEOFF AND PERFORMED AIR TURN BACK. MAINTENANCE INSPECTED ACFT AND DETERMINED THE ACFT WAS DE-ICED PRIOR TO TAKEOFF AND FOUND DE-ICE FLUID IN BOTH ENGINE INLETS. MAINTENANCE REMOVED FLUID AND RAN ENGINES AND PSDR CALA2014022790498Engine · surgesENG 222027 HAD A SILENT SURGE IN CRUISE.SDR CA140312002Engine · malfunctionedDURING CLIMB, A LOUD NOISE WAS HEARD AND POSSIBLY THE NR 1 ENGINE SHUTDOWN. ACFT RETURNED TO POINT OF ORIGIN AND MADE A SINGLE ENGINE LANDING WITHOUT INCIDENT. NO OTHER INFORMATION IS KNOWN AT THIS TIME.SDR 7GMB1153022420141Bearing · failedDURING THE ROUTINE INSPECTION, FOUND NR 1 ENGINE OIL DEBRIS MESSAGE ON CMC, CENTRAL MAINTENANCE COMPUTER. INSPECTED FOR PARTICLES ON THE MAGNETIC INDICATOR PLUGS AND FOUND SWARF IAW MM. SENT OIL SAMPLE AND THE PARTICLES FOR ANALYSIS. THE ANALYSIS REPORT INDSDR 2014FA0000098Engine · vibrationDURING DESCENT AND TAXI, NR 1 ENGINE HAD VIBRATION AT 40 PERCENT N1.SDR CA140225003Engine · vibration(CAN) IMMEDIATELY AFTER DEPARTURE DURING CLIMB, THE ACFT EXPERIENCED ENGINE VIBRATIONS FROM THE NR 1 ENGINE. THE FLIGHT LEVELED OFF AT 13,000 FT AND THE VIBRATIONS SUBSIDED. THE CREW RECOMMENCED THE CLIMB TO 17,000 FT WITH THE VIBRATION RETURNING. THE CREW ESDR CA140312004Engine · unknownTHE PILOT REPORTED NP STAYED AT 100.5 PERCENT DURING INITIAL CLIMB, JUST AFTER TAKEOFF. THE PILOT ELECTED TO SHUTDOWN ENGINE NR 2 AND LANDED SAFELY. NO EEC NOR PEC FAULTS WERE DETECTED. PROPELLER INTERFACE UNIT (PIU) WERE SWAPPED FROM ENGINE NR 1 AND NR 2 FOSDR CALA2014022400226Engine · vibrationNR 1 ENG ROLL BACK INFLIGHT AT FL 400 DROPPED TO 67% N!, THEN RECOVERED, AS WE CONTINUED VIBRATION GOT GRADUALLY WORSE & VIOLENT ON FINAL, LANDED WITH NR 2 ENG POWER & NR 1 ENG AT IDLE VIBRATING. R & R NR 1 ENG IAW WORK CARD 29-7100-1-0900 & 29-7100-1-4900. SDR CA140303001Line · damaged(CAN) AFTER TAKING OFF, THE ACFT SUFFERED ENGINE PROBLEMS. THE PILOT DROPPED THE LOADED WATER AND LANDED IN A MARSH. THE CAUSE FOR THIS ACCIDENT WAS ATTRIBUTED TO DAMAGE ON A FLEXIBLE PY LINE. IAW RECORDS, A LARGE NUMBER OF MFG POWERED AIR TRACTORS INCORPSDR CA140225006Engine · stalled(CAN) ON DEPARTURE PASSING 13,000 FT CREW HEARD A LOUD BANG FOLLOWED BY AN ENG 1 STALL ECAM. MOMENTARY FLAMES OBSERVED FROM AFT OF LT ENGINE ACCOMPANIED BY ACRID ODOR. ODOR DISSIPATED AFTER APPROXIMATELY 5 MINUTES. NR 1 ENG TROUBLESHOT IAW TV 142067, ALL PRSDR FDEA201402200375Engine · failedAFTER TAKEOFF NR 1 ENGINE FAILED & OVER TEMPED. MAX POWER TAKEOFF COMPLETED CHECKLIST. CREW FIRED ONE EACH FIRE BOTTLE. R & R NR 1 ENGINE. OPS & LEAK CHECKED GOOD, OK FOR SERVICE.SDR FDEA201402200374Engine · failedDURING CLIMB, HAD A LIGHTNING STRIKE ON RADOME & RECEIVED A NR 2 ENGINE N1 EXCEEDANCE WITH AUTO THROTTLES ON OF 118.1. QRH PROCEDURES FOLLOWED & ALL ENGINE INDICATIONS NORMAL. DURING CLIMB TO ALT RECEIVED A NR 2 ENGINE OIL FILTER BYPASS. QRH PROCEDURES FOSDR CA140224013Engine · vibration(CAN) DURING TAKEOFF, CREW REPORTED VIBRATION ON NR 2 ENGINE. THEY REDUCED THE POWER ON THIS ENGINE AND REQUESTED FOR DESCENT AND DIVERSION. ONCE POWER WAS REDUCED, THE VIBRATION STOPPED. INVESTIGATION IS ON-GOING.SDR CA140224012Engine · power loss(CAN) THE CUSTOMER REPORTED A TORQUE POWER ROLLBACK RT AFTER TAKEOFF. AFTER EVALUATION, CREW ELECTED TO CONTINUE THEIR MISSION AND ONCE LEVELED, THE TORQUE STABILIZED. AN UNEVENTFUL LANDING WAS PERFORMED. THE CREW DID NOT HAVE TO USE ANY EMERGENCY PROCEDURESDR DALA14010860964Engine · failedREJECTED TAKEOFF AT APPROX 120KTS DUE TO SUSPECTED COMPRESSOR STALL WITH EGT RISING TO 677 ON RT ENGINE. MAINTENANCE FOUND METAL DEBRIS IN TAIL PIPE OF RT ENGINE. THE RT ENGINE REPLACED IAW AMDS CARD 7100-4682RT. LEAK & OPS CHECKED GOOD.SDR SIMA20140218003Carbon Seal · failedFIFTEEN MINUTES AFTER TAKEOFF OF ABOUT FP 270 E2 OIL QTY 5 QT AFTER CHECKED SHUT DOWN MODE SINGLE ENGINE LANDING. ENGINE REPLACED DUE TO NR 7 CARBON SEAL REPLACEMENT.SDR ASAA2014021706887Engine · unknownFOUND LONG TERM FAULT 711181 N2 SIGNAL IS OUT OF RANGE ON NR 1 ENGINE. ACFT GROUNDED.SDR USAA2014021800002Engine · leakingAT CRUISE ALTITUDE FL390, CREW NOTICED NR 2 ENG OIL QTY AT 7.0 QUARTS. LEFT TPA GATE ABOUT AN HOUR PRIOR WITH 18.5 QUARTS ON BOTH ENGS. SOON AFTER, OIL QTY NR 2 CONTINUED TO DECREASE. CREW DECLARED AN EMERGENCY & DIVERTED TO CLT. SHUTDOWN NR 2 ENG AS PRECASDR CA140224009Engine · power loss(CAN) WHILE TAXIING FOR A REGULAR FLIGHT THE NR 2 ENGINE POWER ROLLED BACK AND IT FLAMED OUT. TROUBLESHOOTING IS ONGOING.SDR CA140224008Engine · making metal(CAN) DURING FLIGHT, AT APPROXIMATELY 6500 FT, THE PILOT REPORTED A LOUD RUMBLING SOUND FROM NR 2 ENGINE. THE CREW REPORTED FIRE COMING OUT FROM NR 2 ENGINE EXHAUST. THE ENGINE WAS SHUTDOWN AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED AT THE AIRPORT OSDR CA140217009Ecu · malfunctioned(CAN) DURING CLIMB, THE NR 1 ENGINE REVERTED TO MANUAL AND THE CREW LOST TORQUE INDICATION ON THE LT ENGINE. THE CREW ELECTED TO RETURNED TO THE AIRPORT. UPON TROUBLESHOOTING MAINTENANCE CHECKED THE NR 1 ECU- ENGINE CONTROL UNIT, FOR FAULT CODES. NONE WERE SDR CA140217005Engine · failed(CAN) LEFT ENGINE FAILURE, ENROUTE, LT ENGINE WENT FROM CRUISE POWER TO IDLE AND WAS UNRESPONSIVE TO THROTTLE LEVER MOVEMENT. AFTER A COUPLE OF MINUTES THE ENGINE SHUTDOWN AND WOULD NOT RESTART. ACFT DIVERTED.SDR 27MA20140217001Engine · shutdownRIGHT ENGINE NO COMMANDED SHUTDOWN ON TAXI TO RUNWAY.SDR CA140224006Engine · malfunctioned(CAN) DURING REVENUE FLIGHT, THE ACFT WAS AT FL 430 WENT THE AUTO THROTTLES RETARDED. THEN NR 2 ENGINE HAD IGNITION AND THE ITT ROSE TO 860 DEGREES C. THE CREW ELECTED TO SHUTDOWN NR 2 ENGINE AND THE ACFT LANDED SAFELY.
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