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 CA051116008Engine · failed(CAN) ON OCTOBER 31, 05, THE PILOTS WHEN APPROACHING, WERE TOLD TO RETURN TO DEPARTURE, BECAUSE THE AIRPORT WAS CLOSED. UPON LANDING AFTER SLOWING THE AIRCRAFT, THE PILOT TRIED TO BRING THE POWER LEVERS TO FLT IDLE, BUT THE NR 3 ENGINE WOULD NOT MOVE. MAINTENSDR ALG2005F00089Engine · making metalIN FLIGHT, ENGINE CHIP LIGHT ILLUMINATED. AFTER LANDING, NOTIFIED MAINTENANCE. THE ENGINE CHIP PLUG WAS FOUND TO HAVE METAL FLAKES. REMOVED AND REPLACED ENGINE WITH SERVICEABLE UNIT, IAW MM. (K)SDR SWAA053423Engine · power lossNR 2 ENGINE WOULD NOT SPOOL UP. REMOVED AND REPLACED NR 2 ENGINE HMU, FUEL PUMP, EEC, T25 SENSOR & FUEL NOZZLE FILTER, NO HELP. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR CA051129007Engine · flamed outDURING CLIMB, THE ENGINE FLAMED OUT. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. P&WC WILL MONITOR INVESTIGATION OF THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR XN0A1274Engine · failedNR 1 ENGINE FAULT ON T/O ROLL AT STEWART, LOUD BAND HEARD FOLLOWED BY EPR REDUCTIVE TOWARDS 0. ALL OTHER ENGINE INDICATIONS NORMAL DURING T/O ROLL.SDR AT0500040Engine · inoperativeRT ENG COMP STALL ON CLIMB-OUT, ENG SHUT DOWN, HIGH TGT. REMOVED AND REPLACED RT ENG ASSY. LEAK AND OPS CK NORMAL. OK FOR SVC.SDR HNAA0500096Engine · smokeIN FLIGHT SMOKE IN CABIN AND COCKPIT. USED COCKPIT 02 MASKS. TURNED 13 BLEED OFF AND OPENED OUTFLOW VALVE ON DESCENT TO CLEAR SMOKE AND FLY UNPRESSURIZED, THEN TURNED OFF NR 2 BLEED DIVERTED AND DECLARED EMERGENCY. REMOVED AND REPLACED NR 2 ENGINE.SDR CA051104013Engine · power loss(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED POWER ROLL-BACK ON TAKE-OFF. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE COMPRESSOR AND ENGINE INLET AREA. MFG WILL INVESTIGATE TSDR CA051104012Engine · shutdown(CAN) DURING CRUISE, THE ENGINE WAS REPORTED TO EMIT A LOUD (BANG) FOLLOWED BY SEVERE VIBRATION.THE ENGINE WAS SHUTDOWN IN FLIGHT AND A SINGLE ENGINE LANDING ACCOMPLISHED. MFG WILL INVESTIGATE THE INCIDENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR 2005FA0001475Engine · seizedENGINE INSTALLED ON AIRCRAFT AFTER RETURN FROM REPAIR FACILITY. DURING INITIAL GROUND RUN OF ENGINE THE POWER LEVER SEIZED AND VERY HARD TO MOVE. ENGINE TEMPERATURE AND PRESSURE WERE NORMAL. FEATHERED THE PROPELLER AND SHUTDOWN ENGINE. POST INSPECTION SHOWSDR UIA200509Engine · making metalAC LT ENGINE LOW OIL PRESS WARNING LIGHT ON, PILOT SHUT DOWN LT ENGINE IN-FLIGHT, THEN SINGLE ENGINE LANDING. GROUND INSPECTION RESULTS, FOUND ENGINE CONDITION PANEL TOTAL 7 FLAG, ONLY OIL TANK, RED FLAG SHOW ON, REMOVED OIL TANK CHIP DETECTOR FOUND MINOR METSDR DL76G050651Engine · smokeCREW REPORTS SMOKE OIL SMELL HAZE IN CRUISE. DONNED MASK AND MADE AN EMERGENCY LANDING. SMOKE DETECTORS IN CABIN WENT OFF. ENGINE USED 5 PINTS OF OIL. ENGINE CHANGED.SDR CA051104007Engine · flamed out(CAN) THE ENGINE FLAMED OUT DURING DESCENT. A SUCCESSFUL IN-FLIGHT RE-LIGHT WAS ACCOMPLISHED. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE DETERMINED.SDR CA051104006Engine · overheated(CAN) DURING CLIMB, ENGINE TEMPERATURE INCREASED ACCOMPANIED BY AN UNCOMMANDED DECREASE IN ENGINE TORQUE. THE ENGINE WAS SHUT DOWN IN FLIGHT. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR AALA20050698Engine · making metalBUF INFLIGHT T305/23OCT - RIGHT ENGINE WAS SHUT DOWN BY CREW DUE TO OIL FILTER CLOG LIGHT ILLUMINATING. FOUND METAL IN SCREEN AND FILTER AND OIL TANK. REPLACED ENGINE. FLIGHT DATA RECORDER DOWNLOAD REQUESTED BY ENGINEERING. SYSTEM GROUND CHECKED NORMAL OPSDR AWXA200501284Engine · malfunctionedSMF - AIR TURNBACK - FLT 544 - AFTER TAKEOFF, DURING CLIMB EN ROUTE TO PHX FROM SMF, CREW HEARD LOUD NOISE FROM THE NR 1 ENGINE AND NOTICED NR 2 ENGINE OIL QUANTITY GAUGE DROP BELOW ONE. AIRCRAFT RETURNED TO SMF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANSDR SF20051023Engine · surgesFLIGHT 7591 IAD-PIT ABORTED TAKEOFF AT 100 KNOTS DUE TO LT ENGINE SURGING. DEFERRED CTOT, CONT OPS PER MEL 76-10-1, CONTROL 3150, CAT C, DDD 11/02/05. RTO INSPECTION DUE FOR ABORTED T/O AT 100 KNOTS. C/W RTO INSPECTION IAW M/M 05-50-00-6 PROCEDURE NR 3, NO SDR CA051104011Engine · power loss(CAN) DURING A TRAINING TOUCH-AND-GO MANEUVER, THE ENGINE ROLLED BACK IN POWER AND THE LOW OIL PRESSURE WARNING ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT AND AN UNSCHEDULED LANDING CARRIED OUT. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSESDR 2005UALA01177Blade · wornENGINE 2 STALL DISPLAYED ON UPPER ECAM SCREEN DURING CLIMB OR CRUISE ACCELERATION. ENGINE NOT SHUTDOWN. STALL DISPLAYED ON UPPER ECAM SCREEN AFTER POWER REDUCTION FROM T/O POWER. ENGINE NOT SHUT DOWN. TROUBLESHOOTING BORESCOPE INSPECTION REVEALED OUT-OF-LISDR ABXA050338Air Duct · dentedNR 4 ENGINE L/S TRANSITION AIR DUCT HAD SEVERAL DENTS. 2 DENTS AT 9 AND 11 O'CLOCK POSITIONS OUT OF LIMITS IAW DC8 SRM 51-1-9A. CLEANED UP AREA OF DENTS AT 9 AND 11 O'CLOCK POSITIONS AND REPAIRED IAW DC8 SRM 51-1-9A. 2 MORE DENTS AT 11 O'CLOCK POSITION ARE WISDR UPS05545634Engine · malfunctionedAFTER T/O RT ENG EGT STARTED TO RISE RAPIDLY. ENG EXCEEDANCES RT EGT 879, N2 101, N3 99. RT ENG EEC AND LIMITER EICAS MSGS. APPROACHING FINAL TO LAND AT IDLE THRUST NI A RT TURN. RT ENG FLAMED OUT. EGT 879 FOR 21 SEC N2 101.4 21 SEC N3 99.7 FOR 21 SEC DM SDR CA051104004Engine · failed(CAN) THE ENGINE WAS REPORTED TO HAVE (FAILED) IN FLIGHT AND AN EMERGENCY LANDING WAS CARRIED OUT. THE AIRCRAFT CONTACTED POWER LINES AND SUBSEQUENTLY CRASHED INTO A HOUSE. PRELIMINARY EVALUATION OF THE ENGINE REVEALED NO ANOMALIES. MFG WILL INVESTIGATE THE SDR DL76G050632Engine · damagedDAMAGED BRACKETS, VSV LEVER ARMS, AND HEAT SHIELDS ON NR 1 ENGINE. REPLACED ENGINE.SDR DLM88050627Engine · failedNR 2 ENG FAILED DURING CLIMB-OUT AT 19,800 FT MSL, LOUD BANG, MODERATE VIBRATION FOLLOWED. REPLACED ENGINE.SDR HNAA0500091Engine · malfunctionedAPPROXIMATELY 200 FT AGL, NR 2 ENGINE TORQUE AND NH FLUCTUATED +/- 50 PERCENT SHUT DOWN ENGINE IN FLIGHT. REMOVED AND REPLACED NR 2 ENGINE.SDR QXEA200501349Warning Light · illuminatedSEA - FLIGHT 2060, ENGINE MANUAL CAUTION LIGHT. COMPLIED WITH RESET AND TEST PROCEDURES PER MCN 27631-01. TEST GOOD. NO PARTS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR CA051104002Engine · making metal(CAN) DURING TAKE-OFF AND CLIMB THE ENGINE WAS REPORTED TO SURGE AND LOSE POWER. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED METALIC DEBRIS ON THE TURBOMACHINE CHIP DETECTOR . MFG WILL INSDR AALA20050682Engine · making metalBOS - INFLIGHT JUST AFTER ROTATION A STRANGE RUBBING NOISE WAS HEARD FROM THE COCKPIT FOLLOWED BY A THUMP. A STRONG VIBRATION WAS FELT IN THE REAR OF THE AIRCRAFT. RETURNED TO BOS AND LANDED WITHOUT INCIDENT. FOUND METAL IN OIL FILTER. REPLACED RIGHT ENGISDR C2XA05TY055Bevel Gear · failedFLT 3251 - AT FL350 ENGINE NR 1 FAILED WITH NO INDICATIONS. MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE ASSY, COMPLIED WITH OPERATIONAL CHECKS AND ACFT WAS RELEASED TO SERVICE. *S/D* TEARDOWN REPORT: CAUSE OF THE UNCOMMANDED IN FLIGHT SHUTDOWN WAS A BSDR HALA0501023Bearing · failedON CLIMBOUT AT 16,00 FEET GOT (ENG R SURGE) LIGHT. FOLLOWED BY SOME SMOKE IN CABIN. FOLLOWED BY (ENG R SYS FAIL) LIGHT AND (R OIL FILTER) LIGHT. REDUCED POWER ON RT ENGINE RETURNED FOR LANDING. RT ENGINE INDICATIONS WERE NORMAL AFTER POWER REDUCTION. HOWSDR CA051013008Engine · power lossRT ENGINE WAS REMOVED FOR LOW TORQUE INDICATION AND SENT OUT FOR REPAIR AFTER TESTING PROVED AN INTERNAL PROBLEM. THE ENGINE WAS RE-INSTALLED FROM REPAIR WITH A NEW TORSION SHAFT SN 05P15649 AND TORQUE SENSOR P/N 3101726 AND NTS TEST FLIGHT WAS CARRIED OUT ANSDR PCSA10120501Engine · overheatedAFTER DEPARTURE ENGINE NR 3 OIL TEMPERTURE INCREASED TO 160, PERFORMED ALTERNATE PROCEDURE, NO HELP. SHUT DOWN ENGINE, DUMPED FUEL TO LAND. MX INSPECTED INLET & EXHAUST OF NR 3 ENGINE; INLET OK, EXHAUST SHOWS EVIDENCE OF OIL LEAK, SUSPECT NR 6 BEARING SEAL. SDR MWEA050115Engine · malfunctionedNUMBER TWO ENGINE PRESSURE RATIO DECREASED AT 0.2 AND ENGINE PRESSURE RATIO AND 10 PERCENT N1 BOTH PACKS ALSO SHUTDOWN. SERVICED FUEL CONTROL BELLOWS. INSPECTED PT2 MOISTURE TRAP AND PT7 MOISTURE TRAP, PS4 STRAINER, CHECKED PT2 AND PT7 LINE AND FITTING AND BSDR AMTA200500854Line · looseEICAS MSG LT ENG OVHT DISPLAYED WITH ENG OVHT ILLUMINATED. LGT EXTIN AFTER THRUST REDUCTION. FOUND NR 1 ENG TEMP SENSOR SENSE LINE LOOSE ON FAN AIR MODULATING VALVE, SECURED IN PLACE, RAN ENGINE, OPS CHECK NORMAL. (K)SDR MWEA050114Engine · out of limitsRIGHT ENGINE AT/NEAR ALL PARAMETER LIMITS. PERFORMED RIGHT ENGINE PT7 LEAK CHECK, NO LEAKS. PERFORMED PT7 AND PT2 LEAK DOWN CHECKS TEST PASSED. RAN BOTH ENGINES AND FOUND NO ABNORMAL GAUGE READINGS AT TAKEOFF POWER SETTINGS. STICK SPILT WAS WITHIN LIMITS, SDR SB05129Engine · failedPIT - FLT 391 - ON CLIMBOUT FROM PIT, AT FL140, CREW REPORTED A LOUD BANG FROM THE NR 1 ENGINE. SIMULTANEOUSLY, SMOKE FILLED THE COCKPIT, THE NR 1 ENGINE OVERTEMP LIGHT ILLUMINATED AND THE AIRCRAFT YAWED. ENGINE CAME TO AN ABRUPT STOP. CREW SECURED THE ENGISDR AU510001986Engine · failed(AUS) RT ENGINE FAILED DURING LANDING ROLL WHEN REVERSE THRUST WAS DE-SELECTED. THOROUGH INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. SUSPECT THE FUEL FLOW MAY HAVE DROPPED TOO FAR WHILE REDUCING NEGATIVE THRUST TO A POINT THAT THE ENGINE FLAMED OUT. THESDR HNAA0500093Engine · malfunctionedNR 2 TORQUE DROPPED FOM 90 PERCENT TO 61 PERCENT WHEN ECU SELECTED TO NORMAL AFTER TAKEOFF WITH NO ILLUMINATION OF NR 2 MANUAL LIGHT. CYCLED BETA LOCKOUT CIRCUIT BREAKER.SDR DL764050618Engine · failedLEFT ENGINE EGT STAYING AROUND 687 DEG CELSIUS AND N2 IS AT 75.5 ENG WILL NOT ACCEL. METAL SIZE OF BB-S CAN BE SEEN IN THE AFT TURBINE SECTION. BOROSCOPE REVEALED HPC DAMAGED. THE T/E OF THE HPT SHOWED EVIDENCE OF FOD DAMAGE. REPLACED ENGINE.SDR 2005FA0001433Engine · flamed outWHILE IN CRUISE, WE WERE VMC ON TOP OF A CLOUD DECK, EXPERIENCED A NR 2 ENGINE CHIP LIGHT. IMMEDIATELY, NR 2 ENGINE SHUTDOWN. NR 1 AUTOPILOT ALSO DROPPED OFF LINE. EMERGENCY WAS DECLARED AND SINGLE ENGINE INSTRUMENT ILS APPROACH WAS ACCOMPLISHED. WEATHER ATSDR AALA20050659Engine · damagedMCI - INFLIGHT CLIMBING THROUGH FL20, FLIGHT CREW HEARD A BANG AND SAW NR 2 ENGINE EXHAUST GAS TEMPERATURE DOUBLED AND LOSS OF N1 AND N2. AIR RETURNED TO MCI AND LANDED WITHOUT INCIDENT. FOUND SEVERAL MISSING FAN BLADES. REPLACED RIGHT HAND ENGINE. SYSTEM SDR CA051104005Engine · making metal(CAN) IN FLIGHT, COMPRESSOR SPEED DECREASED UNCOMMANDED ACCOMPANIED BY AN INCREASE IN TURBINE TEMPERATURE. THE ENGINE WAS SHUTDOWN IN FLIGHT AND THE AIRCRAFT DIVERTED FOR AN UNSCHEDULED LANDING. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS IN THE ENGINE OIL ASDR DL76G050617Engine · failedNR 1 ENGINE, S/N 704883 FAILED OPN 5155 BOROSCOPE INSP DUE TO 1 EA 1ST STAGE NGV HAVING BURN THRU AREA BEYOND M/M LIMITS. ENGINE REMOVAL REQUIRED. ENGINE S/N 704883, REMOVED AND REPLACED PER TRANS 1T160.SDR 2006FA0000113Line · leakingPILOT SAW TORQUE PRESS FLUCTUATE. TORQUE PRESS LINE TO GAUGE LEAKED AND ENGINE WAS STARVED OF OIL. THE AIRCRAFT HAD MADE A NORMAL LANDING AND SHUTOFF ENGINE SEIZED UP ON COASTDOWN, REPLACED ENGINE. (K)SDR CALA0500331Engine · making metalTHE NR 2 ENGINE GAVE OFF A LOUD BOOM AND THE AIRCRAFT SHUDDERED AND YAWED DURING CLIMBOUT OF ORD AT 8,000 FEET. THE NR 2 ENGINE INDICATIONS WERE FROZEN. QRH WAS FOLLOWED AND THE CREW SHUTDOWN THE ENGINE. THE AIRCRAFT WAS RETURNED TO ORD WHERE IT LANDED WITHSDR CED2006F00021Engine · shutdownTHE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED WITHOUT INCEDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOU REQUEST AFTER MAINTENASDR AWXA200501180Engine · failedAFTER TAKEOFF CREW HEARD LOUD BANG AND FELT VIBRATION COMING FROM THE NR 1 ENGINE. AIRCRAFT RETURNED TO PHX, DECLARED EMERGENCY AND LANDED WITHOUT FURTHER EVENT. MAINTENANCE BORESCOPED THE NR 1 ENGINE LPC AND HPC, FINDING DAMAGE TO THE HPC STAGES 7, 8 AND 9.SDR SWAA053018Engine · overtempAIR TURNBACK, NR 2 ENGINE OVERTEMP AT 990 DEGREES FOR 15 SECONDS. RED OVERTEMP LIGHT ILLUMINATED FOR MORE THAN 1 MINUTE. MX FERRY TO PHX. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR 2006FA0000112Engine · making metalDURING FLIGHT, THE CHIP LIGHT ILLUMINATED, CHIPS WERE FOUND AND BEFORE 30 MINUTE GROUND RUN WAS COMPLETED ANOTHER LIGHT OCCURRED. CHIPS WERE OF SUFFICIENT SIZE THAT REQUIRED REMOVING THE ENGINE. (K)SDR MASA200500764Engine · overtempASH 6110 PHX. RED FLASHING ITT ON LT ENGINE DURING TAKE OFF ROLL. TEMPERATURE EXCEEDED 900 DEGREES. MX R2 ENGINE.
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