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 CA140804007Engine · leaking(CAN) DURING CRUISE FLIGHT, SMOKE IN THE CABIN WAS OBSERVED. THE AIRCRAFT DIVERTED, WHERE THE PROBLEM WAS ISOLATED TO ONE OF THE ENGINES DURING POST-FLIGHT INSPECTION. OIL WAS NOTED IN THE CABIN BLEED PORTS. ADDITIONAL TROUBLESHOOTING WILL CONTINUE TO DETERMINSDR CA140804006Engine · surges(CAN) WHILE IN CRUISE THE RT ENGINE WAS SURGING WITH TQ AND NP FLUCTUATING AND ACFT YAW. ITT STARTED TO RISE AND CREW SECURED THE ENGINE WHEN ITT REACHED 850 DEGREES. CUSTOMER REPORTED A CT DISK AND STATOR REPLACED 50 HOURS PRIOR THIS EVENT AND THAT GRINDING SDR ASOA20140724082Engine · bird ingestionPILOT REPORTED A STRONG ODOR OF SMOKE APPROACH AND SHUTOFF PACKS AND ODOR WENT AWAY. MX INSPECTED ACFT AND DETERMINED NR 1 ENGINE INGESTED A BIRD. MX PERFORMED A BIRD STRIKE INSPECTION, ENGINE COMPRESSOR SECTION BORESCOPE, AND FOD INSPECTION IAW MM 05-50-00. SDR CA140804005Engine · surges(CAN) IT WAS REPORTED THAT THE RT ENGINE HAD AN ENGINE SURGE. NO EEC AND PEC FAULT. BORESCOPE INSPECTION OF LP/HP IMPELLER OF BOTH ENGINES DID NOT SHOW ANY DAMAGE. GROUND-RUN PERFORMANCE CHECK, OK AS THE ENGINE SURGE HAS OCCURRED ON A REMOTE ISLAND, A TEAM HASDR CA140724010Engine · power loss(CAN) POWER LOSS DURING TAKEOFF RESULTING IN HARD LANDING. ENGINE WAS RUNNING AT THE TIME OF THE HARD LANDING.SDR CALA2014072300979Engine · leakingFLIGHT LVL 40 CONFIRMATION FLIGHT FOR SMOKE DETECTION IS UNSUCCESSFUL AT FL 400. TURNED OFF LT PACK & DESCENDED SMOKE CLEAR 5 TO 10 MIN NR 1 ENG HAS INTERNAL OIL LEAK AT COMPRESSOR SECTION IAW 21 51355 FOR NR 1 ENG CHANGE.SDR WRNA201407230015Engine · making metalON REACHING TOP OF CLIMB, A LEVEL 2 OIL PRESSURE LOW DISPLAYED. CREW FOLLOWED THE QRH PROCEDURES SIMULTANEOUSLY FOLLOWING THE QRH PROCEDURES "ENGINE SHUTDOWN IN FLIGHT" FOR ENG NR 2. THE CREW ACCOMPLISHED THE CHECKLIST THEN PROCEEDED TO DUMP APPROXIMATELY 50SDR CA140721018Engine · damaged(CAN) DURING THE TAKEOFF ROLL CREW EXPERIENCED A COMPRESSOR STALL ON THE NR 2 ENGINE AND CARRIED OUT A LOW SPEED RTO. ON ARRIVING AT THE GATE AND CREW WERE INFORMED BY GROUND MAINTENANCE THAT THERE WAS VISIBLE DAMAGE TO THE NR 2 ENGINE. NR 2 ENGINE REPLACED.SDR AALA20140719004Engine · failedAIRCRAFT SHOOK & RT ENG LOST OIL PRESS. RT ENG WAS SHUTDOWN, SINGLE ENG TIME 15 MINUTES. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED RT ENG ON 07/21/2014. SYS GND CHECKED NORMAL OPERATION OPEN.SDR DALA2014072304179Engine · failedTHE NR 1 ENGINE FAILED DURING TAKEOFF. FLIGHT RETURNED TO DEPARTURE. PILOTS HEARD A THUD, NOTICED LT ENGINE ROLLED BACK AND SHUTDOWN, AND THE EGT INCREASED. THE QRH WAS COMPLIED WITH AND THE FUEL WAS SHUTOFF. MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINESDR CA140804004Engine · malfunctioned(CAN) DURING TAXI, THE PILOTS RECEIVED A CAUTION MESSAGE ASSOCIATED WITH FAULT CODE P3 SENSOR MIS-COMPARE ON NR 2 ENGINE. ACFT RETURNED TO HANGAR FOR TROUBLESHOOTING AND THE FAULT COULD NOT BE REPRODUCED. ON THE FOLLOWING FLIGHT, DURING CLIMB AT FL120 WHEN POSDR SIMA20140717001Unknown · malfunctionedLOUD BANG ON LT SIDE ENG INFLIGHT N1 & N2 FLUCTUATING 2%, ITT FLUCTUATING 15* ON LT ENG. LOUD BOOM SOUND FROM LT SIDE OF ACFT EVERY 15 SEC OR SO AUDIBLE IN THE COCKPIT. PERFORMED MANUAL TASK 72-00-00-700-801, NO DEFECTS NOTED.SDR CA140804002Engine · overtemp(CAN) THE ENGINE WAS INTENTIONALLY SHUTDOWN IN FLIGHT, THE CREW NOTICED THAT THE ITT WAS RISING AND EXCEEDED THE TRANSIENT LIMIT OF 865C FOR APPROXIMATELY 2 MINUTES, 1 OF WHICH WAS AT OR ABOVE THE STARTING LIMIT OF 1090C FOR APPROXIMATELY 1 MINUTE. ADDITIONASDR XV6A2014071500002Engine · warning lightDURING CRUISE FLIGHT AT 9500 FT, MASTER WARNING HORN & LIGHT SOUNDED. LT OIL PRESSURE ANNUNCIATOR ILLUMINATED & TORQUE DROPPED. RAN QRH ENG FAILURE CHECKLIST, DECLARED AN EMERGENCY & DIVERTED. REMOVED LT PROPELLER & ENGINE AS AN ASSEMBLY. INSTALLED SERVICESDR XV6A2015071500001Engine · failedLEFT ENGINE COMPRESSOR STALLED DURING CLIMB OUT AT APPROXIMATELY 23000 FEET. EGT EXCEEDENCE 627 DEGREES. ENGINE FAILED ON APPROACH. PERFORMED OVERTEMP INSPECTION, ENGINE FAILED BORESCOPE AND VISUAL INSPECTIONS. METAL FOUND IN TAILPIPE, ALONG WITH MOLTEN METSDR N6WA20140713001Engine · vibrationNUMBER 1 ENG N1 VIBE 1.9. INSPECTED NR 1 ENG BLADES FOR STIFFNESS CHECK & PERFORMED ENG RUN. FOUND TO HAVE 0.2 N1 VIBE AT THIS TIME IAW AMM 72-21-02. PLACED ON CARRYOVER 4239.SDR 2014FA0000427Coupling · crackedADS COUPLING FOUND TO HAVE A CRACK INDICATION ON ALL BOLT HOLES DURING FPI.SDR CA140721012Engine · malfunctioned(CAN) DURING A TRAINING FLIGHT, IN CRUISE CONDITION, THE CREW EXPERIENCED AN UNCOMMAND POWER INCREASE. THEY WERE UNABLE TO REDUCE THE ENGINE POWER. ENGINE WAS SHUTDOWN BY THE CREW. THEY LANDED UNEVENTFULLY TO THE DESTINATION AIRPORT. TROUBLESHOOTING IS IN PSDR AALA20140711016Engine · shutdownLEFT ENG HAD UNCOMMANDED SHUTDOWN DURING CRUISE, SINGLE ENG TIME 20 MINS. NO RE-START WAS ATTEMPTED. EMER DECLARED FLIGHT DIVERTED LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT ENG ON 07/15/2014. SYS GND CHECKED NORMAL OPERATION OPEN.SDR ASAA2014071108529Engine · vibratesNR 2 ENGINE TREND DATA SHOWS LOW PRESSURE ROTOR VIBRATION LEVELS TO BE TRENDING HIGHER THAN EXPECTED CURRENT LEVELS NEAR 1.5 UNITS. ACFT GROUNDED. ACCOMPLISHED ON BOARD FAN TRIM BALANCE ON NR 2 ENGINE IAW MM 71-00-00-750-808-F00. SWITCHED WEIGHT NR 2 FROM PSDR CA140721013Engine · malfunctioned(CAN) DURING CRUISE, THE PILOT HEARD A LOUD NOISE FROM THE 2 ENGINE FOLLOWED BY WARNING/CAUTION LIGHT FOR OIL INDICATION AND IN-FLIGHT SHUTDOWN. ACFT WAS DIVERTED.SDR CA150108008Bearing · failed(CAN) ENGINE CHIP LIGHT ILLUMINATED. FOUND NR 5 BEARING BRINELLED.SDR CA140721011Engine · surges(CAN) REVIEW OF THE GBS FILES INDICATES THAT THE ENGINE ENCOUNTERED A DROP IN P3, BY APPROXIMATELY 15 PSI, POSSIBLY DUE TO AN ENGINE SURGE. THE CAUSE OF SURGE IS NOT APPARENT AND INVESTIGATION IS CONTINUING.SDR CA140711004Engine · power loss(CAN) AFTER TAKE OFF, TORQUE INCREASED ON ENGINE NR 2 SLIGHTLY. AFTER ADJUSTING POWER LEVER, TORQUE ON NR 2 DECREASED TO ABOUT 30% AND AUTOFEATHER KICKED IN. CREW SHUT DOWN THE FEATHER ENGINE AND LAND SAFELY. FDR WAS PULL FOR DOWNLOAD AND FOUND OUT THAT THERE SDR JJBA201407080016Engine · power lossABORTED TAKEOFF, NR 1 ENG DID NOT ACHIEVE TAKEOFF POWER.SDR CA140721005Engine · power loss(CAN) PRIOR TO TAKEOFF, THE PILOT OBSERVED A LOW PROPELLER SPEED FOLLOWED BY A LOSS OF POWER. FIRE IN THE ENGINE COMPARTMENT WAS REPORTED WHICH HAD EXTINGUISHED BEFORE THE FIRE DEPT ARRIVED.SDR WX0A2014080572068Engine · malfunctionedAT 11,000 FT DURING CLIMB OUT, LT OIL PRESS LOW AOP WITH FALLING LT OIL PRESS ON GAUGE <30 PSI & FALLING FAST. IAW QRH 72/14 WITH OIL PRESS BELOW 35 PSI, SHUT DOWN ENG. COMPLIED WITH QRH PROCEDURE 72.3, ENG SHUTDOWN, LANDED SINGLE ENG. IAW WORK ORDER 228642SDR CALA2014071191456Engine · vibrationNUMBER 2 ENG VIBRATION. ENG NR 2 NEEDS A VIBRATION SURVEY TEST NR 8 ACCOMPLISHED IAW MM 71-00-00-725-008-N00. COMPLETED VIBRATION SURVEY, VIBRATION WELL WITHIN LIMITS IAW JRH. HIGHEST READING WAS 1.6 AT 82 PER CENT N1 FAN IAW MM 72-31-00 PG 507.SDR CA140721008Engine · malfunctioned(CAN) DURING FLIGHT AT 16000 FEET, THE CREW FELT A NOTICEABLE YAW THEY NOTICED THE ENGINE NR 2 DISTINCT TORQUE FLUCTUATIONS FOLLOWED BY TORQUE AND ITT PARAMETERS DROPPING RAPIDLY. THE CREW THEN ELECTED TO PERFORM THE CHECKLIST AND SHUTDOWN PROCEDURE, BY THE TSDR 2DYA20140708001Engine · power lossWE ENCOUNTERED AN AREA OF HI CLOUDS AS WE ENTERED THE AREA LIGHT TURBULENCE WAS ENCOUNTERED & A NOTED TEMP OF -51 SAT. LIGHT MOISTURE WAS OBSERVED & THE ENG ANTI-ICE WAS SELECTED ON. LIGHT ICING WAS OBSERVED INCREASING FROM MODERATE TO HEAVY & A TEMP OF -41 SDR SWAA2014070729654Engine · malfunctionedAIR TURN BACK & DECLARED EMER. NR 2 ENG EGT SPIKE 950 DEG C, VIBRATION 4.8. KEPT ENG AT IDLE FOR REMAINDER OF FLIGHT. R & R NR 2 ENG IAW MT.SDR CA140721006Engine · failed(CAN) DURING THE DECENT, THE CREW NOTICE OIL ODOR IN THE CABIN AND ENGINE NR 1 LOW OIL PRESSURE. THE PILOT SHUTDOWN THE ENGINE AND PERFORMED AN UNEVENTFUL SINGLE ENGINE LANDING. THE ON GROUND TROUBLESHOOTING REVEALED NOISY POWER TURBINE SECTION DURING PROPELSDR CA140704001Warning Message · activated(CAN) REPORTED A CHIP DETECTOR LIGHT INDICATION FOLLOWED BY AN OIL PRESSURE AND OIL TEMPERATURE FLUCTUATION AND ENGINE TORQUE DROPPING TO ZERO.SDR SWAA2014070729655Engine · overheatedDIVERSION ON TAKEOFF NR 1 ENG OVERHEATED 973 DEGREES FOR 8-10 SECONDS. R & R NR 1 ENG IAW MT.SDR HALA2014070300095Warning Message · illuminatedDURING NR 1 ENGINE START, ECAM MESSAGE, NR 1 ENGINE CTL SYS FAULT. ACCOMPLISHED ECAM ACTIONS. NEXT START NORMAL, NR 1 ENGINE SLOW RESPONSE. PERFORMED TSM 73-21-72-810-899-A. ENGINE RUN NORM. NO FAULTS NOTED. OK FOR SERVICE.SDR SWIA201438521Engine · malfunctionedNR 2 ENGINE INDICATION FLUCTUATION AND UNCOMMANDED ACCELERATION ON CLIMBOUT.SDR CA140721002Turbine · damaged(CAN) DURING FLIGHT, THE ENGINE NR 2 SHOWED ITT FLUCTUATIONS. THE ENGINE OIL PRESSURE LIGHT WAS INTERMITTENT DURING FINAL APPROACH. AFTER LANDING, THE ENGINE NR 2 FIRE WARNING TURNED ON. BOTH FIRE EXTINGUISHER BOTTLES WERE ACTIVATED AND THE FIRE WARNING TURSDR ASAA2014062908392Engine · faultedWHILE ACCOMPLISHING T/C 78273000, NR 1, ENGINE SHOWED LONG TIME FAULT CODE 76-31361, STARTER LEVER SIGNAL DISAGREE. ACFT GROUNDED. ACCOMPLISHED T/C 78273000. NO FAULTS FOUND.SDR CA140701012Engine · overtemp(CAN) ON TAKEOFF, PILOT REPORTED AN OVER TEMPERATURE INDICATION. THE CREW ELECTED TO SECURE THE ENGINE AND PROCEEDED TO DESTINATION. PRIOR TO LANDING, CREW RESTARTED THE ENGINE AND PERFORMED UNEVENTFUL LANDING.SDR CA140701010Engine · inoperative(CAN) DURING AN ENGINE SHUTDOWN TRAINING EXERCISE, THE PILOT WAS NOT ABLE TO RESTART THE ENGINE. THE CUSTOMER CONTACTED MFG TO SEND THE ENGINE FOR INVESTIGATION.SDR DEMA2014063000002Engine · failedDURING CRUISE, THE PILOT NOTICED A FLUCTUATION OF THE ENGINE TORQUE INDICATOR. THE FLUCTUATION WAS BETWEEN 50-100 FT/LBS. IMMEDIATELY FOLLOWING THE TORQUE FLUCTUATION, THE OIL PRESSURE DROPPED AND THE OIL TEMPERATURE ROSE. AN EMERGENCY WAS DECLARED AND THE SDR MASA2014062702193Engine · unknownNR 1 ENGINE PRODUCED A LOUD BANG DURING CLIMB AT 12000 FEET. OPENSDR CA140701014Engine · malfunctioned(CAN) WHEN APPROACHING AIRPORT, THE PILOT HEARD A LOUD BANG ON LT ENGINE, ASSOCIATED WITH ACFT TENDENCY TO THE LT. LEFT ENGINE LOST POWER AND ITT INCREASED. THE PILOT ELECTED TO SHUTDOWN ENGINE AND PERFORM A SINGLE ENGINE LANDING. TROUBLESHOOTING ONGOING.SDR CA140701008Engine · unknown(CAN) CUSTOMER REPORTED AN IFSD OF THE LT ENGINE DURING CLIMB THROUGH 3500FT, INITIAL REPORT IS THAT THE ENGINE MADE A LOUD NOISE, FOLLOWED BY A VERY SHORT SPIKE IN FUEL FLOW, WF, AND SUDDEN DROP IN TORQUE, TQ, AND COMPRESSOR SPED, NG. THE ITT INCREASED TO A MSDR I5PA201406010002Engine · leakingNUMBER 3 ENG SHUT DOWN IN FLIGHT DUE TO POSSIBLE COMPRESSOR STALL, FOLLOWED BY OIL LOSS. THE INLET & EXHAUST LOOKED OK, BUT EVIDENCE OF OIL LOSS FROM THE EXHAUST. NR 3 ENG HAS BEEN R & R. INSTALLED IAW AMM. PERFORMED OPERATIONS CHECK & HIGH POWER ASSURANCESDR CA140721003Engine · vibration(CAN) AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION HAD COME BACK AFTER THE ENGINE WAS REINSTALLED. THE PILOT MENTIONED THAT THIS VIBRATION HAD NOT BEEN FELT WHEN THE RENTAL ENGINE WAS INSTALLED.SDR CA140701006Engine · overtemp(CAN) THE PILOT ABORTED THE TAKEOFF DUE TO THE LT ENGINE ITT INDICATOR BAND MOVE TO RED ENGINE TEMPERATURE LIMIT AND THE WHITE INDICATOR BAND TURNED TO RED. ALL OTHER ENGINE INSTRUMENTS DISPLAYED NORMAL INDICATIONS PRIOR TO TAKING THE RUNWAY. TROUBLESHOOTISDR FDEA201406251547Engine · failedON DEPARTURE ROLL TPE 23R APPROACHING 100 KTS EXPERIENCED NR 1 ENG FAILURE. REJECT PERFORMED, ACFT TOWED BACK TO GATE TIME 1349. ENG FIRE AGENT DISCHARGED IAW QRH PROCEDURE. NR 1 ENG REMOVAL & REPLACEMENT ACCOMPLISHED.SDR CA140805001Engine · vibration(CAN) DURING CRUISE, THE PILOT FELT ENGINE VIBRATIONS AND ELECTED TO DIVERT THE FLIGHT FROM ITS INTENDED DESTINATION. A SAFE LANDING WAS MADE WHERE POST FLIGHT INSPECTION FOUND METALLIC FUZZ ON THE CHIP DETECTOR. THE ENGINE IS BEING REPLACED.SDR CA140626006Engine · vibration(CAN) WHILE ENROUTE THE CREW NOTED A CHANGE IN ENGINE SOUND ACCOMPANIED BY A FAINT VIBRATION WHICH THEY DESCRIBED AS SIMILAR TO BLADE ICING AND ELECTED TO LAND AS A PRECAUTION. ALL ENGINE INDICATIONS WERE NORMAL THROUGHOUT THE FLIGHT. ON THE GROUND THE NR 1 E
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