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 FDEA200811104881Engine · inoperativeENG NR 2 FAILURE DURING CLIMB-OUT. CLIMB POWER PASSING 1800 FT, FELT SHUDDER, HEARD A BANG, HAD YAW. COMPLETED SINGLE ENGINE LANDING. NO SMOKE OR FIRE PULLED NR 2 ENG FIRE HANDLE AND AGENT 1 DISCHARGED. EGT SPIKE TO 780. R AND I NR 2 ENGINE AND PERFORMED SDR ZZDA2008167Engine · shutdownIN CRUISE, NR 1 ENGINE AUTO-SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE IAW AIRTRAN TASK CARD 603.SDR Q2SA758003Engine · damagedDURING TAKEOFF AFTER V1 FROM HAAB, BIRD INGESTION INTO NR 3 ENGINE. AIR TURNBACK TO HAAB. FUEL DUMP OF 50,000 LBS. INSPECTION AFTER LANDING CONFIRMED DAMAGE TO NR 3 ENGINE FAN BLADES, AS WELL AS EVIDENCE OF BIRD STRIKE ON NR 2 ENGINE. NR 1, 3, 4, 6, 11, 13SDR CA081022009Engine · damaged(CAN) DURING CLIMB, THE PILOT HEARD AN UNUSUAL NOISE FROM THE ENGINE FOLLOWED BY A DECREASE IN COMPRESSOR TURBINE SPEED. THE PILOT RETURNED TO HIS POINT OF DEPARTURE WHERE AN UNEVENTFUL LANDING WAS MADE. THE ENGINE WAS NOT SHUT DOWN AND THE EMERGENCY POWER LEVSDR DLM88081300Engine · malfunctionedRT OIL PRESSURE DROPPED TO 0 AND RT OIL PRESSURE LOW MSG ON EOAP. SECURED RT ENG IN ACCORDANCE WITH THE QRH. OPENED LOWER COWL DOOR, REMOVED MAG CHIP DETECTOR. CLEANED INTO PAPER TOWEL. RE-INSTALLED MAG DETEDCTOR. PAPER TOWEL WITH ME LOCATED IN MCO PLACARDSDR ESPADJ2088-1Engine · lack of lubeDEPARTED CARTERSVILLE AIRPORT AND PASSING 2000FT MSL THE MASTER CAUTION AND OIL PRESSURE LIGHTS ILLUMINATED. THE CREW NOTED 0 OIL PRESSURE ON THE LEFT ENGINE AND RETURNED TO THE AIRPORT FOR AN UNEVENTFUL LANDING. GROUND CREW NOTED AN EXTENSIVE OIL LEAK AND CSDR BSY2008F00005Engine · failedACFT ENROUTE, WHEN THE ENGINE FAILED. PILOT WAS ABLE TO LAND ON A HIGHWAY WITH NO PROBLEMS. CAUSE UNKNOWN AT THIS TIME. (K)SDR CA081016015Engine · fire(CAN) DURING FLIGHT, THE PILOT SAW FLAMES COMING OUT OF THE ENGINE EXHAUST BEFORE LOSING POWER. HE DECLARED EMERGENCY AND DIVERTED THE FLIGHT TOWARDS A NEARBY AIRPORT. HE WAS NOT ABLE TO MAKE THE AIRPORT AND HE WAS FORCED TO LAND ON A ROAD. THE PILOT WAS NOSDR EIA2008055Engine · making metalDURING CRUISE ENCOUNTERED HEAVY SURGE NR 2 ENG ALONG WITH VIBRATION EPR DROPPED TO BOTTOM OF SCALE EGT REACHED YELLOW BAND, REDUCED POWER TO IDLE, VIBRATION PERSISTED, SHUT NR 2 ENGINE DOWN ENG WINDMILL OIL PRESS AT 28PSI. ANGLE GEARBOX AND MAIN GEARBOX CHIP SDR EIA2008F00010Engine · surgesDURING CRUISE, ENCOUNTERED HEAVY SURGE IN NR 2 ENGINE ALONG WITH VIBRATION, EPR DROPPED TO BOTTOM OF SCALE, EGT REACHED YELLOW BAND, REDUCED POWER TO IDLE, VIBRATION PERSISTED, SHUTDOWN NR 2 ENGINE, WINDMILLED OIL PRESSURE AT 28 PSI.SDR AALA200802452Engine · leakingEWR INFLT T1323/27SEP JFK TO ORD CREW REPORTED VIBRATION IN AIRFRAME FOLLOWED BY NR 1 ENGINE OIL QUANTITY LOSS AND OIL TEMPERATURE INCREASE. CREW SHUT DOWN NR 1 ENGINE. LANDED EWR WITHOUT INCIDENT. SINGLE ENGINE TIME 15 TO 20 MINUTES. REPLACED NR 1 ENGINESDR USA2008F00034Engine · vibrationFLIGHT 1615, CLT - MCI, PASSING 16,000FT THE NR 2 ENGINE TRIGGERED A HP VIB WARNING LIGHT (REGISTERING 5.0 VIBRATION). AFTER CONSULTING THE CHECKLIST THE CREW RESTORED POWER TO THE ENGINE, SIMILAR RESULTS OCCURRED. THE CREW DECIDED TO RETURN TO CLT. THE ENGSDR COMA0870026Engine · vibrationFLIGHT NR 6421 DURING CLIMBOUT FROM CVG NR 1 ENGINE N1 VIB INCREASED TO 1.8 YELLOW, IN CRUISE VIB WENT TO 2.4 YELLOW. SHUT DOWN ENGINE, RESTARTED ENGINE AND VIB WENT AWAY. EMERGENCY DECLARED. A/C CONTINUED TO MSP AND LANDED SAFELY. INSPECTED NR 1 ENGINE FASDR ABXA200810270254Engine · defectiveLEFT FAN ENGINE VIBRATION HIGH 4.7. OTHER VIBRATION INDICATIONS WERE: AIRPLANE VIBRATION, AUDIBLE NOISE, VIBRATION FOLLOWS THRUST CHANGE. REPLACED NR 1 ENGINE PER WORK CARD NR 7010. OPS CHECK NORMAL.SDR SIMA200827301Engine · smokeON FLIGHT 3540 DURING CLIMB OUT AT APPROX FL180 CREW DETECTED SMOKE IN THE COCKPIT FOLLOWED BY A LAV SMOKE INDICATION. CREW CONFIRMATION SMOKE IN THE CABIN. CREW THEN NOTICED A LOW OIL QUANTITY ON THE NR 1 ENG (3QTS) AND COMPLETED A PRECAUTIONARY ENGINE SHUTSDR DL76S081236Engine · making metalNR 2 ENGINE OIL PRESSURE WENT TO ZERO, HEARD AUDIBLE STALL. CREW SHUT OFF FUEL LEVER. MTC FOUND METAL IN THE TAIL PIPE. NR 2 ENG REPLACED PER TRANS 1T145.SDR CA080924013Engine · fluctuates(CAN) AT ABOUT 50 METERS FROM THE ARRIVAL GATE, THE ENG PARAMETERS STARTED FLUCTUATING. PILOT SHUTDOWN THE ENG. NO REPORTED DAMAGE. TROUBLESHOOTING IN PROGRESS. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR CA080924011Torque Shaft · cracked(CAN) DURING CRUISE TORQUE WAS LOST ON NR 1 ENGINE, SUBSEQUENTLY THE ENGINE WAS SHUTDOWN BY THE CREW. POST FLIGHT INSPECTION REVEALED A CRACKED TORQUE SHAFT AT THE WELD JOINT. ENGINE IS BEING REMOVED FOR INVESTIGATION. MFG WILL CONTINUE INVESTIGATING THE EVSDR CHQA200800186Engine · leakingFLIGHT 6142 CMH TO JFK. DURING TAKE OFF AT ABOUT 500 FT AGL THE FLIGHT CREW NOTICED AN OIL LIKE SMELL WITH NO EICAS MSGS. AT 1000 AGL LAV SMOKE APPEARED ON EICAS. THE FLIGHT ATTENDANT INSPECTED THE LAVATORY AND FOUND NO SIGNS OF SMOKE OR FIRE. THE LAV SMOKSDR FDEA200809213956Duct · leakingDURING CLIMB PASSING FL180, EICAS MESSAGE DISPLAYS L ENG OVHT ALL OTHER ENG INDICATIONS WERE NORMAL. RETARDED L THROTTLE AND TURNED OFF L BLEED AIR. AFTER APPROXIMATELY 2 MIN THE EICAS MESSAGE WENT AWAY. DECLARED EMERGENCY AND LANDED WITH L ENG AT IDLE. COSDR DL76P081209Engine · bird ingestionDURING T/O HAD BIRDSTRIKE ON LEFT SIDE OF AIRCRAFT. RETURNED MCO. MTC FOUND DENT IN FUSELAGE FWD OF LEFT PITOT PROBES. AOA VANE SHEARED OFF. PITOT PROBES IMPACTED. LEFT ENGINE HAS 2 FAN BLADES BENT OUT OF LIMITS AND SOME MINOR ACOUSTICAL LINER DAMAGED. VSDR AALA200802386Rotor · seizedORD INFLIGHT T779/20SEP. AT APPROX 2000 FEET NR 1 ENGINE LOST ALL POWER. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE ON 20 SEP AT ORD DUE TO ROTOR SEIZED. SYSTEM GROUND CHECKED NORMAL OPS.SDR P5CA0801576Engine · surgesNR 3 ENGINE SURGED ON TAKE OFF ROLL. TAKE OFF ABORTED AT 100 KTS. HIGH ENERGY STOP INSPECTION COMPLETED PER AMM 05-51-10. NO TROUBLE FOUND. ALSO NR 3 ENGINE CIT SENSOR WAS REPLACED AND TESTED OK. ACFT DEPARTED WITH NO FURTHER ISSUES.SDR SIMA200826601Engine · malfunctionedON FLIGHT 4176 CREW REPORTED RECEIVING A LAV SMOKE INDICATION ON CLIMB ON EICAS FOLLOWED BY FA REPORT OF SMOKE IN CABIN. CREW RETURNED FOR AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. C/A DETERMINED OIL/SMOKE SMELL TO BE COMING FROM NR 2 ENGINE. SDR IXX2008F00097Engine · flamed outDURING CRUISE, AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RESTART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINT ISDR IXX2008F00096Engine · flamed outDURING CRUISE AT 36,000 FT WITH POWER REDUCTION NR 2 ENGINE FLAMED OUT, WITH 1-2 PSI OIL PRESSURE ATTEMPTED INFLIGHT RESTART, NO FUEL FLOW AND NO IGNITION. THE CREW PERFORMED INFLIGHT ENGINE SHUTDOWN PROCEDURE. THE CREW LANDED WITHOUT FURTHER INCIDENT. OPEN (SDR DXTA200809153275Bushing · deterioratedSTARTED BOTH ENGINES UNEVENTFULLY THEN LT ENGINE UNEXPECTEDLY STOPPED RUNNING. FOUND RUBBER BUSHING ON LT ENGINE BELLCRANK DETERIORATED. REPLACED BUSHING. C/W GROUND RUNS. PERFORMED ACCELERATION CHECK AND IDLE CUTOFF CHECK IAW MM CHP 71-01-03. ALL PARAMETESDR M7JA2009030200001Engine · malfunctionedIN CRUISE FLIGHT THE CAPTAIN NOTICE A DROP IN THE RT ENGINE OIL PRESSURE WITH INCREASE IN OIL TEMP. THERE WAS NOT VIBRATION OR VISIBLE OIL LEAKS ON THE MENTION ENGINE. THE PILOT FOLLOWED THE PROPER CHECKLIST EXECUTING A PRECAUTIONARY ENGINE SHUTDOWN. THE FLSDR 2008UALA05688Engine · malfunctionedUPON ARRIVAL AT GATE NR 1 ENGINE WAS SMOKING HEAVILY.SDR CA080917005Engine · vibration(CAN) IN CRUISE, THE FLIGHT EXPERIENCED A NR 1 ENGINE VIBRATION. THE ENGINE CONTINUED OPERATING NORMALLY BUT WITH VIBRATION. THE FLIGHT DIVERTED TO FAIRBANKS, ALASKA. AN ENGINE HAS BEEN SCHEDULED AND TOOLS, PARTS AND MANPOWER ARE CURRENTLY BEING SHIPPED TO SDR DJF2008F00014Engine · making metalREPORTED LOW OIL PRESSURE IN FLIGHT. THE AFFECTED ENGINE WAS SHUTDOWN, AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED. MAINTENANCE FOUND METAL IN THE OIL SYSTEM. THE ENGINE WAS REMOVED FOR OEM EVALUATION. AIRCRAFT RETURNED TO SERVICE. (K)SDR AC2A2008090878102Unknown · unknownDEPARTED AIRPORT AT 0951 WITH VFR CONDITIONS, CLEAR SKIES 12 MILES VISIBILITY. 1.5 MILES SOUTHWEST AT AN ALTITUDE OF 500 FT AND CLIMBING, HEARD A LOUD REPORT ASSOCIATED WITH A HARD RT YAW AND NR DECREASING THROUGH 92 PERCENT. HAD JUST PASSED OVER A CLEAR AREASDR CA081105002Engine · overtemp(CAN) WHILE DEPARTING AREA WITH AN AIRSPEED OF 30 TO 40 KNOTS AND A 500 FT PER MINUTE RATE OF DESCENT, NR 2 ENG N1 LOW RPM AUDIO HORN SOUNDED ALONG WITH ILLUMINATION OF NR 2 ENG LOW OIL PRESSURE LIGHT. A SCAN OF ENG GAUGES REVEALED NR 2 ENG HAD LOW N1 RPM WITSDR CA080925006Engine · malfunctioned(CAN) WHILE DEPARTING AREA WITH AN AIRSPEED OF 30 TO 40 KNOTS AND A 500 FT PER MINUTE RATE OF DESCENT, NR 2 ENGINE N1 LOW RPM AUDIO HORN SOUNDED ALONG WITH ILLUMINATION OF NR 2 ENGINE LOW OIL PRESSURE LIGHT. A SCAN OF THE ENGINE GAUGES REVEALED THE NR 2 ENGINSDR CA080917016Engine · malfunctioned(CAN) DURING A RE-POSITIONING FLIGHT, THE PILOT NOTED LOW AND FLUCTUATING OIL PRESSURE. THE ENGINE WAS SHUT DOWN AND SECURED AND A SINGLE ENGINE LANDING WAS PERFORMED. GROUND INSPECTION FOUND CONTAMINATION IN THE OIL FILTER AND FILTER BOWL. THE ENGINE WILL SDR CA080917013Engine · malfunctioned(CAN) A YAW OF THE ACFT CAUGHT THE ATTENTION OF THE PILOT AND A QUICK REVIEW OF THE COCKPIT GAGES REVEALED THAT THE RT ENGINE TORQUE WAS FLUCTUATING BETWEEN APPROXIMATELY 20% TO 40% WITH THE TEMPERATURE INDICATION RISING TO APPROXIMATELY 820 DEGREES. THE PILOSDR UIE2008F00044Isolation Valve · failedAIR TURN BACK. DURING CLIMB BOTH LT AND RT MANIFOLD PRESSURE WAS FLUCTUATING. DURING TROUBLESHOOTING AFTER CRUISE POWER SET 103.4, THE NR 1,3, AND 4 PYLONS VALVES WOULD NOT CLOSE. WITH LT AND RT ISOLATION VALVES CLOSED, IT WAS DETERMINED THAT THE NR 1 PYLON VASDR 2008FA0000610Bearing · failedSPOOL BEARING ASSY FAILED INTERNALLY. BEARING ASSY NO LONGER ROTATES AND CAUSED DRIVE SHAFT GUIDE POST AND FORK IN GOVERNOR LEVER ASSY TO BEND. THE UPPER BEARING LOWER SHIELD AND RETAINER HAS COME OFF. THE LOWER BEARING IS INTACT BUT NO LONGER ROTATES. (K)SDR CA080917012Engine · malfunctioned(CAN) DURING A 5 MIN. RE-POSITIONING FLIGHT, THE ENGINE LOST POWER AND AN EMERGENCY LANDING WAS ATTEMPTED. THE ENGINE WILL BE RETURNED TO P&WC FOR INVESTIGATION. P&WC WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR IXX2008F00093Line · looseDURING TAKEOFF ROLL, NR (1) ENGINE WOULD NOT ACCELERATE PAST 78 PERCENT. NR 2 WITH CORRESPONDING LOW N1, FUEL FLOW AND EGT. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINT INSPECTED AND FOUND LOOSE PT2 LINE ON PRBC VALVE. MAINT RECONNECTED LINE. OPERSDR CA081007002Engine · malfunctioned(CAN) POST LANDING AND TAXI. ACFT WAS STATIONARY WITH BOTH ENGINES IN THE GROUND IDLE POSITION WITH ROTORS TURNING. PILOT OBSERVED ROTOR SPEED WAS NEARING A KNOWN "AVOID RANGE" AND ELECTED TO NUDGE THE NR 1 ENGINE CONTROL LEVER FORWARD TO INCREASE ROTOR SPEESDR DL76G081157Engine · making metalFOUND DURING SERVICE CHECK, FOUND METAL ON MCD. SHOP ANALYST REPORTS BEARING MATERIAL. MUST REPLACE ENGINE, E/C IN WORK ATL.SDR 2008FA0000737Engine · fodAFTER TAKEOFF, OVERSPEED WARNING LIGHT ILLUMINATED. RPM REDUCTION USING PROP GOVERNOR CONTROL NOT SUCCESSFUL, USED THROTTLE CONTROL TO REDUCE ENGINE RPM. LANDED WITHOUT INCIDENT. REPAIR STATION INSPECTED AND DUPLICATED PROBLEM ON ENGINE GROUND RUN. ALL VISUAL SDR CA080917009Engine · shutdown(CAN) PILOT REPORTED THAT DURING TAXI THE ENGINE EXPERIENCED UNCOMMANDED ROLL BACK AND SHUTDOWN. TROUBLESHOOTING INDICATED THAT THE ENGINE MAY HAVE ALSO EXPERIENCED AN OVERTEMP CONDITION AND WAS REMOVED FROM SERVICE FOR INSPECTION. P&WC WILL CONTINUE INVESTISDR CA080911006Engine · failed(CAN) AFTER T/O AND CLIMB OUT, NR2 ENGINE LOST OIL QTY AND OIL TEMP ROSE RAPIDLY INTO RED INDICATION. INFLIGHT SHUTDOWN COMPLIED WITH AND ACFT RETURNED TO DEPARTURE. NR2 ENGINE REPLACED IAW AMM AND KFL TASK CARDS, ACFT RETURNED TO SERVICE. ENGINE TO BE EVALUATSDR COMA0880016Engine · vibrationENROUTE, CREW REPORTS FAN VIBRATION ON RT ENGINE. AC DIVERTED AND LANDED SAFELY. INSPECTED RT ENGINE FAN BLADES NO DEFECTS NOTED. PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED. (K)SDR EIA2008F00003Engine · stalledDURING TAKEOFF EGT`S WERE PEAK 934,908,908,913 ON ENG`S ONE THRU FOUR. AUTO THROTTLES WERE ON. AFTER REDUCTION TO CLIMB POWER, PASSING THRU 1800`, IN LEFT TURN WE HEARD A LOUD BANG ACCOMPANIED WITH AN AIRCRAFT SHUDDER. NOTICED NR 3 N1 ROLLING BACK WITH N2 ROLSDR 2008FA0000608Bearing · failedSPOOL BEARING ASSY (PN 2544198) FAILED INTERNALLY. BEARING ASSY NO LONGER ROTATES AND CAUSED DRIVE SHAFT (PN 2539033) GUIDE POST AND FORK ON GOVERNOR LEVER ASSY. (PN 2523293) TO BEND. ONE FLYWEIGHT (PN 2544200) WAS DAMAGED FROM THE SPOOL BEARING CHAFING. (K)SDR CNM2008F00001Engine · overheatedDURING CLIMB THRU 15000 FT N2 103.4 TAT +20 NACELLE TEMP WAS 240 DEGREE C PREV SUPPLY SELECTED OFF AXCELL TEMP DECREASED 10 DEGREES C STILL 40 DEGREE C ABOVE QRH CHARTED VALVE (NR 1 ENG). (K)SDR HEF2008F00000Bearing · failedUPPER BEARING, (PN 2525465) INSIDE OF SPOOL BEARING ASSY FAILED (CAME APART). LOWER SPOOL BEARING, (PN 2525468) IS STILL INTACT, BUT NO LONGER ROTATES FREELY. (K)
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