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 WX0A2015092472884Engine · malfunctionedDURING CLIMB OUT IN CALM CLEAR AIR, FELT A HEAVY VIBRATION THROUGHOUT THE ENTIRE ACFT, IT ONLY LASTED A FEW SECONDS. R & R NR 2 ENG IAW TC 71-080-003. ACFT OK FOR SERVICE.SDR CA151006017Engine · making metal(CAN) AIRCRAFT EXPERIENCED AN ENGINE CHIP LIGHT ILLUMINATION. DURING INSPECTION, FOUND CHIPS ON BOTH ENGINE CHIP PLUGS, CONDUCTED THE CLEANING/FLUSHING STEPS IAW THE OPS & MM, AND DURING THE SUBSEQUENT 30-MINUTE GROUND RUN, THE ENGINE CHIP LIGHT ILLUMINATEDSDR CA151006008Engine · power loss(CAN) CUSTOMER REPORTED THAT DURING THE MISSED APPROACH, THE NR 2 ENGINE DID NOT GENERATE FULL POWER DURING THE GO-AROUND MANEUVER. THE PILOTS NOTED LARGE FLAMES COMING-OUT FROM THE EXHAUST AND A SPIKE IN THE ITT OF THENR 2 ENGINE. THE FLIGHT CREW SECURED THESDR CA150927005Engine · malfunctioned(CAN) THE PILOT REPORTED THAT THE N2 ON THE RT ENGINE STUCK AT 90 N2 DURING CLIMBOUT. MFG RECOMMENDED TO PERFORM SB 30409. TROUBLESHOOTING ONGOING.SDR CA150927004Engine · power loss(CAN) IT WAS REPORTED THAT THE ENGINE HAD AN IFSD DUE TO LOP. THE INCIDENT HAPPENED AT ALTITUDE OF ABOUT 20K , THE CREWS NOTICED AN ENGINE NR 1 OIL PRESSURE INDICATING 25 PSI. NO MASTER WARNING FOR OIL PRESSURE AND THE CREW ELECTED TO SHUT DOWN NR 1 ENGINE. AISDR CA151007013Bearing · failed(CAN) AN OIL ODOR IN CABIN UNDER UNKNOWN CIRCUMSTANCES WAS REPORTE. THE ENGINE ALSO HAD HIGH OIL CONSUMPTION AT THE TIME. TROUBLESHOOTING FOUND BEARING MATERIAL ON THE TURBOMACHINE CHIP DETECTOR. THE ENGINE WAS REPLACED AND FORWARDED FOR REPAIRS. ACFT WAS RETSDR CA151007006Engine · smoke(CAN) CUSTOMER REPORTED OIL ODOR AND SMOKE IN THE CABIN COMING FROM THE RT ENGINE. THE OIL PUMP WAS REPLACED AN ACFT RETURNED TO SERVICE.SDR 9EKA20150916024Engine · failedDURING CRUISE FLIGHT IN A SHALLOW RIGHT HAND TURN, NR 2 ENG EXPERIENCED HIGH SIDE FAILURE IMMEDIATELY, FOLLOWED BY UNCOMMANDED SHUTDOWN. ACFT RECOVERED 26 MILES BACK TO BASE IN SINGLE ENG CONFIGURATION.SDR JIKA2015091401Engine · power lossSHORTLY AFTER TAKEOFF, THE PILOT HEARD A LOUD BANG FROM THE RT ENG & LOST POWER. THE PILOT PERFORMED AN INFLIGHT SHUTDOWN OF THE RT ENG, RETURNED & LANDED WITHOUT INCIDENT. THE RT ENG IS BEING REPLACED. A FOLLOW UP TO THIS SDR WILL BE SUBMITTED WHEN A TEAR SDR A6WA201543061Engine · malfunctionedRECEIVED VIBRATION & HEARD LOUD BANG, THEN SAW N1 & N2 ON LT ENG DECREASING & ITT RISING UNTIL IT EXCEEDED 900 DEG C. PULLED LT ENG BACK TO IDLE UNTIL SHUTDOWN, CHECKLIST COULD BE COMPLETED. N1 & N2 CONTINUED TO ROTATION, ITT WENT TO ALMOST ZERO. VIBRATION SDR R61A201509140635Engine · power lossCREW REPORTED A LOUD BANG FOLLOWED BY LOSS OF ALL POWER FROM THE NR 1 ENGINE. CREW DECLARED AN EMERGENCY, RAN QRH AND RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT.SDR CA150925008Engine · fluctuates(CAN) CREW REPORTED THAT DURING CLIMB THE LT ENGINE TEMPERATURE WAS FLUCTUATING AND INDICATING HIGH. THE POWER WAS REDUCED AND THE TEMPERATURE STABILIZED. THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE. TROUBLESHOOTING IS ON-GSDR 3D9A2015091200006Engine · making metalNR 1 ENGINE CHIP LIGHT ILLUMINATED IN FLIGHT. MADE PRECAUTIONARY LANDING. DISCOVERED SMALL SLIVER ON REAR BEARING SUPPORT HOUSING CHIP DETECTOR. CATEGORIZED AND TYPED AS MINOR FUZZ IAW LTS101-750B-1, MM 72-00-00 PARA 20 C & D. RETURNED TO SERVICE IAW MFG, LSDR CA150925009Engine · power loss(CAN) SOON AFTER TAKEOFF, DURING CLIMB, ENGINE POWER ROLLED BACK CLOSE TO IDLE SPEED. ENGINE WAS NOT RESPONDING TO PLA INPUT. CREW ACTIVATED PLA AND MADE EMERGENCY LANDING WITHOUT INCIDENT. POST LANDING INSPECTION DID NOT REVEAL ANY EXTERNAL FINDINGS ON ENGINSDR CA150925002Engine · malfunctioned(CAN) THE OPERATOR REPORTED AN AIR TURN BACK DUE TO HIGH ITT, LT ENGINE ON TAKEOFF, ITT ROSE TO JUST SHORT OF RED LINE, LATER DECREASED WITH REDUCED POWER.SDR CA150927002Engine · making metal(CAN) DURING THE LAST WEEK, THERE WERE SOME REPORTS OF OIL ODOR IN COCKPIT WHEN PL ARE RETARDED TO FI FOR DESCENT IN THE SUBJECT ACFT. A BORESCOPE INSPECTION WAS PERFORMED AS THE LAST STEP IN THE TROUBLESHOOTING IN THE GAS GENERATOR CASE AREA, P2.5 AND P3 LOCSDR SIMA20150908003Engine · smokeSMOKE COMING OUT OF ENG 2, AFTER SHUTDOWN WITH A STRONG SMELL OF BURNED OIL. COMPLIED WITH ETN-EM-79-015 STEPS 1 - 9. RETURNED ENG TO SERVICE. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR CALA2015091094283Engine · malfunctionedNUMBER 3 ENG SURGED ABOUT 25 MINUTES AFTER TAKEOFF, FOLLOWED BY EEC MODE & EGT SPIKE. ENG WAS SHUT DOWN & ACFT RETURNED. REPLACED ENG IAW TOD 71-00-02 CONFIG 3 PAGE 401. OPERATIONS & LEAK CHECKED NORMAL.SDR CA150915001Engine · unknown(CAN) THE HELICOPTER CRASHED ON A ROCK SLOPE ADJACENT TO THE SEA. PICTURES TAKEN DURING THE ACCIDENT SEQUENCE SHOW SMOKE COMING FROM 1 OF THE ENGINES AND A DAMAGED WINCH LINE. THE HELICOPTER CAME TO REST AGAINST LARGE ROCKS WITH THE TAIL BOOM SEPARATED AND SDR CA150911004Engine · power loss(CAN) DURING A FLIGHT TEST, AFTER ANNUAL CHECK, THE NR 1 ENGINE EXPERIENCED A LOSS OF TORQUE. NO OTHER DETAILS ARE AVAILABLE ON THE CIRCUMSTANCES. THE OPERATOR IS CURRENTLY DOWNLOADING ENGINE AND AIRFRAME DATA, TROUBLESHOOTING IS ON-GOING.SDR A6WA201543039Engine · surgesLEFT ENG ITT AT IDLE IS 590 DEGREES C & RT ENG ITT AT IDLE IS 480 DEGREES C. AT TAKEOFF POWER 91%, LT ENG WAS SLOW TO SPOOL UP, ITT IMMEDIATELY WENT TO 900 DEGREES C & AN AUDIBLE SURGE WAS HEARD FROM LT ENG. PERFORMED ENG POWER ASSURANCE CHECK IAW AMM 71-00-SDR HALA2015090500189Engine · fodFOD DAMAGE NR 2 ENGINE INLET COWL AT 12 O'CLOCK POSITION, 1" ROUND. THE COWL WAS REPAIRED IAW CMM TASK 71-60-00-300-813-A01, AND REPLACED IAW CMM TASK 71-60-00-300-813-A01.SDR CA150925003Engine · power loss(CAN) THE PILOT REPORTED THAT AFTER NOTICING AN INCREASING IN RAT INDICATION AND A DECREASING IN THE RATE OF CLIMB,BOTH ENGINES ROLLED BACK. "NORMALLY THE ENGINE ROLL BACK IS PREDATED BY A T2 HEATER FAIL L/R. BUT WAS NOT THE CASE. SINCE THE RATE OF CLIMB WAS VSDR CA150911006Engine · power loss(CAN) THE LT ENGINE HAD A UNCOMMANDED POWER ROLL BACK. NO T2 HTR CAS MESSAGE APPEARED. IT OCCURRED DURING CLIMB IN IMC, SUPER MOIST, LIGHT ICE, AROUND FL270.SDR CA150911005Engine · power loss(CAN) WHILE ON APPROACH THE ACFT LOST POWER FROM NR 2ENGINE. CREW MADE A EMERGENCY CALL OUT AND TOOK APPROPRIATE EMERGENCY ACTION TO STABILIZE THE FLIGHT FOR SINGLE ENGINE OPERATIONS AND DIVERTED. WHILE ENROUTE, THE CREW SUCCESSFULLY RESTARTED NR 2 ENGINE UTISDR ASAA2015083112984Shim · wornALL 24 FAN BLADE SHIMS REQUIRE REPLACEMENT, REF TASK CARD 78472002. ACFT GROUNDED. R & R ALL 24 FAN BLADE SHIMS, REF TASK CARD 78472002.SDR CA150911003Engine · overtemp(CAN) AFTER TAKEOFF, THE RT ENGINE TEMPERATURE WARNING TURNED AMBER. THE ENGINE TEMPERATURE CONTINUED TO RISE UNTIL POWER WAS REDUCED. THE CREW ELECTED TO RETURN TO THE ORIGIN AIRPORT WHERE AN UNEVENTFUL LANDING WAS MADE. HIGHEST INDICATED TEMPERATURE WAS 9SDR CA150911002Engine · overtemp(CAN) ON TAKEOFF ROLL, JUST AFTER THE BRAKES WERE RELEASED, THE LT ENGINE TEMPERATURE READ 722 C WITH 89.6 PERCENT N1 AND A OAT OF 26 DEGREES CELSIUS. TAKEOFF WAS ABORTED WITHIN 2 SECONDS DUE TO THE TEMPERATURE EXCURSION. TROUBLESHOOTING IS ON-GOING.SDR CA150910003Engine · power loss(CAN) IT WAS REPORTED THAT THE ACFT HAD JUST DEPARTED AIRPORT AND WAS CLIMBING THROUGH 300 FT, WHEN A LOUD NOISE WAS HEARD FROM 1 OF THE ENGINES. THE PROPELLER AUTO-FEATHERED, AND THE ENGINE SHUTDOWN IMMEDIATELY. THE ACFT LANDED SINGLE ENGINE WITHOUT INCIDENTSDR CA150901008Engine · malfunctioned(CAN) AFTER STOWING THRUST REVERSERS, FLIGHT CREW ATTEMPTED LT TURN TO EXIT RUNWAY. USED BRAKING AND ENGINE THRUST IAW QRH, DUE TO STEERING INOPERATIVE CAUTION MESSAGE POSTED SHORTLY AFTER TAKEOFF, WHEN LT AND RT ENGINES SUDDENLY SHUTDOWN.SDR ASAA2015082712955Warning Message · illuminatedNR 1 ENGINE SHOWS FAULT HISTORY ECONOMIC FAULT MESSAGE 73-31371, UPPER EGT SECTORS READING HIGH ON FLT LEG 9. ACFT GROUNDED, OPEN.SDR AALA201508289018Engine · leakingFLIGHT 9200 EN-ROUTE, DURING CRUISE, ENG 2 OIL PRESS WENT TO ZERO. ENG 2 WAS SHUT DOWN. THE FLIGHT DECLARED AN EMER & DIVERTED WHERE IT LANDED WITHOUT FURTHER INCIDENT. R & R NR 2 ENG ASSEMBLY IAW JC 33L40071001.SDR CA151130013Engine · malfunctioned(CAN) WHEN DESCENDING FROM CRUISE TO FL 150, THE PILOT NOTED WARNING LIGHT ON "ENG MAIN". PILOT REDUCE THE POWER TO IDLE (VIA POWER LEVER). WHEN THE PILOT TRIED TO ACCELERATE THE ENGINE ALL ENGINES PARAMETERS CONTINUED IN IDLE. NO COMMAND VIA POWER LEVER. POWESDR CA150910002Engine · overtemp(CAN) LEVEL OFF AT FL380 THROTTLES, AS ACFT ACCELERATED DURING LEVEL OFF, THE LEFT ITT MOVED INTO THE RED INDICATION AND REQUIRED THROTTLE REDUCTION OUT OF MCT TO CHANGE THE READING INTO THE GREEN. ITT INDICATED IN THE RED FOR APPROXIMATELY 2 SECONDS.SDR CA150908014Engine · power loss(CAN) DURING THE TAKEOFF ROLL, FLIGHT CREW IDENTIFIED THAT THE NR 1 ENGINE N1 WAS NOT ACHIEVED FOLLOWING APPLICATION OF THRUST. THE TAKE-OFF WAS ABORTED AND THE THRUST LEVERS WERE BROUGHT TO IDLE. THE FLIGHT CREW NOTED AT IDLE THRUST THAT THE NR 1 ENGINE N1 WASDR CA150901007Engine · power loss(CAN) LOSS OF NR 2 ENGINE POWER OCCURRED DURING APPROACH AND THE TORQUE INDICATION SHOWS 3 %. THE AIRCRAFT PERFORMED AND UNEVENTFUL LANDING. IT WAS FOUND THAT A TUBE WAS BROKEN AT CONNECTION TO HMU. THE TUBE WILL BE REPLACED.SDR CA150901005Engine · smoke(CAN) ENGINE WAS INSTALLED AFTER REPAIR AND SINCE THEN THE CREW HAS REPORTED SMOKE AND OIL ODOR IN THE CABIN AND ALSO THE FIRE DETECTOR AT THE LAVATORY WERE INDICATING THE SAME. WHEN THE ENGINE WAS RUN ON THE GROUND THERE WAS NO SMOKE. DURING TAKEOFF AND LEVSDR HALA2015082500168Engine · flamed outNR 1 ENGINE FLAMED OUT AT 40 KNOTS, DURING TAKEOFF ROLL. ENGINE CHANGE IN PROCESS.SDR CA150901004Engine · fluctuates(CAN) CUSTOMER REPORTED THAT ON DESCENT BOTH ENGINES TORQUE FLUCTUATING BETWEEN 20 PERCENT -7 PERCENT WHILE OTHER ENGINE PARAMETERS WERE SAID TO BE STABLE. EVENT LASTED APPROXIMATELY 3 MINUTES AND THE ACFT WAS REPORTED TO BE, FISH TAILING, DURING THAT EVENT. SDR 8MHR2015FA0000422Nozzle · fracturedENGINE WAS REPORTED TO HAVE N1 LOCKUP. ON DISASSEMBLY OF THE TURBINE, FOUND 6 OF THE 8 LOCATING TANGS SEPARATED FROM THE SECOND STAGE NOZZLE.SDR P5CA2015082700104Adapter · wornWORN, NR 1 ENGINE LT AND RT CORE COWL HOLD OPEN ROD BEARING AND ADAPTER WORN IAW AMM 70-50-00-912-001 -001, REV 112, REPLACED NR 1 ENGINE LT AND RT CORE COWL HOLD OPEN ROD END AND ADAPTER. CONDITION CHECK NORMAL.SDR AALA201508259006Engine · bird ingestionFLIGHT 894 EN-ROUTE, ON DESCENT SMELL OF ELEC BURNING NEAR ROWS 18 - 22 ACFT LT. THE FLIGHT DECLARED AN EMER, DIVERTED & LANDED WITHOUT FURTHER INCIDENT. FOUND BIRD STRIKE ON NR 2 ENG. PERFORMED WORK ON CARDS 26L00005006, 26L00072005, 26L00072007 & 26L0002SDR CA150901003Engine · power loss(CAN) DURING FLIGHT AT 40,000 FT THE NR 2 ENGINE POWER ROLLED BACK TO 40 PERCENT N1, 50 - 60 PERCENT N2. THE ENGINE DID NOT RESPOND TO THROTTLE MOVEMENTS. THE ACFT DESCENDED TO 34,000` WHERE IT WAS OBSERVED THAT RT ENGINE RECOVERED GRADUALLY BACK UP TO NORMAL SDR ASAA2015082112970Engine · faultedWHILE ACCOMP T/C 78273000, FOUND NR 1 ENGINE W/ ECONOMIC FAULT 73-31371, UPPER EGT SECTORS READ HIGH. ACFT GROUNDED. ON DEFERRAL.SDR JLTA20150824001Engine · malfunctionedON FRIDAY, AUGUST 21ST AT APPROX 1900Z, ACFT DEPARTED EMPTY & ENTERED CRUISE, EVERYTHING WAS NORMAL. ON THE INITIAL DESCENT CREW HEARD A STRANGE NOISE & OBSERVED AN ENG COMPUTER LIGHT FOR THE NR 2 ENG. ALL OF THE INSTRUMENTS FOR THE NR 2 ENG THEN FLUCTUATED SDR DALA2015082105124Engine · making metalDIVERTED DUE TO A RT ENGINE OIL FILTER CAUTION EICAS MESSAGE. FOLLOWED THE QRH AND THE ENGINE WAS SHUTDOWN. EMERGENCY WAS DECLARED. TROUBLESHOT IAW FIM 79-21-00-815-803-P00. FOUND MAGNETIC CHIP DETECTOR CONTAMINATED IN EXCESS OF INSPECTION LIMITS AMM 79-21SDR CA150901001Engine · power loss(CAN) DURING TAKE-OFF THE EEC WARNING LIGHT CAME ON FOR A SHORT TIME AND ENGINE NR 1 DID NOT ACCELERATE. AFTER ANOTHER TAKE-OFF ATTEMPT THE ENGINE SPOOLED DOWN AND WENT OFF. THE PILOT TRIED TO RESET THE EEC BUT WITH NO SUCCESS. FIELD SERVICE REP. WILL GO ON SISDR CA150820010Engine · shutdown(CAN) ENGINE WAS RECEIVED FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED AN IN-FLIGHT SHUT-DOWN DUE TO LOSS OF TORQUE. DUE TO THE TIME ACCUMULATED BY THE ENGINE SINCE THE PREVIOUS OVERHAUL, THE OPERATOR ALSO ELECTED TO OVERHAUL THE ENGINE AT THIS SHOSDR A6WA201542997Engine · bird ingestionBIRD STRIKE RT ENG AFTER TAKEOFF, ROTATION VIB FELT IN ACFT, N1 FAN BLADES. ENG VIB WENT FROM .3 TO 2.1, LANDED UNDERWEIGHT. VIBE FELT IN FEET & YOKE.SDR ASAA2015082012971Engine · faultedWHILE PERFORMED T/C 78273000, FOUND NR 1 ENGINE FAULT 79-31121, OIL FILTER SIGNALS DISAGREE, LONG TIME FAULT. ACFT GROUNDED. ON DEFERRAL.
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