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 CA050221006Torque Tube · detached(CAN) DURING CLIMB THE ELECTRONIC PROPELLER CONTROL ANNUNCIATED ACCOMPANIED BY AN AIRCRAFT YAW AND SUBSEQUENT FADEC FAIL WARNING. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALEDTHE ENGINE'S TSDR CA050224011Engine · malfunctioned(CAN) THE ENGINE WAS SHUTDOWN IN FLIGHT DUE TO DECREASING ENGINE OIL PRESSURE ACCOMPANIED BY OIL ODOR IN CABIN AND INCREASING OIL AND TURBINE TEMPERATURES. MFG WILL MONITOR THE INVESTIGATION OF THE EVENT AND WILL SUPPLEMENT THIS REPORT TO PROVIDE ROOT CAUSE OSDR 2005F00054Engine · stoppedFLT 9133 - JAX - DURING TAKEOFF ROLL, WITH LEFT ENGINE AT APPROXIMATELY 1,000 LBS OF TORQUE, UNUSUAL NOISE HEARD. LEFT ENGINE CEASED. ABORTED TAKEOFF. DETERMINED LEFT POWER SECTION SEIZED. REMOVED AND REPLACED LEFT ENGINE ASSEMBLY AND ROUTED FAILED UNIT FOSDR CA050221009Engine · failed(CAN) DURING CLIMB THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY A DECAY IN ALL ENGINE PARAMETERS. THE CREW SHUT THE ENGINE DOWN IN FLIGHT, DECLARED AN EMERGENCY AND DIVERTED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE HIGH PRESSURE SDR CA050222007Engine · damaged(CAN) AS A RESULT OF PROP STRIKE ENG SUFFERED SOME TIP RUBS IN COMPRESSOR, PT & SCORING DAMAGE IN A PROPSHAFT BOLT HOLE. FULL O/H LEVEL INSP OF RGB COMPONENTS FOUND ONLY NORMAL OPS DAMAGE WITH NO ADDITIONAL DAMAGES. ENG FOUND TO HAVE 14 OF 47 1ST STAGE PT BLADSDR DXTA200500595Engine · failedRIGHT ENGINE FAILED ON CLIMBOUT ABOUT 3 MINS AFTER TAKEOFF. FOUND ENGINE HAD INTERNAL FAILURE. REMOVED AND REPLACED RT ENGINE, LEAK CHECKED AND OPS CHECKED GOOD PER G200 MM 71-00-00.SDR CA050323007Engine · failed(CAN) ON TAKE-OFF ROLL, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION ACCOMPANIED BY HIGH/INCREASING TURBINE TEMPERATURE. THE PILOT ABORTED TAKE-OFF AND SECURED THE ENGINE. SUBSEQUENT INSPECTION REVEALLED HOT SECTION DISTRESS.SDR ASMF200502010Engine · lack of lubeDURING ENGINES STARTING, RT ENGINE DID NOT STABILIZED AND WAS SHUTDOWN. OIL QTY CHECKED & REFILLED TO THE CORRECT LEVEL. RT ENGINE RESTARTED & ACFT DISPATCHED BUT IT RETURNED TO PLATFORM DUE TO DURING TAXING OIL TEMP INDICATION 177 DEGREES. ACFT SENT TO HASDR 0500196729Engine · overheatedSHORTLY AFTER TAKEOFF, THE NR 4 ENGINE NACELLE TEMPERATURE BEGAN TO INCREASE FOLLOWED BY THE FIRE WARNING ANNUNCIATION. THE CREW FOLLOWED COM PROCEDURES AND WHEN POWER WAS REDUCED THE FIRE WARNING CEASED AND THE NACELLE TEMPERATURE BEGAN TO DECREASE. THE NR SDR 05FDEA00287Engine · vibrationAT FL 340 EXPERIENCED NR 1 ENGINE VIBRATION, N1 ROLLED BACK TO 34%, N2 62% FF 690 LBS. EXECUTED ENG FIRE SEVERE DAMAGE CHECKLIST, FUEL DUMP ABOUT 3000 LBS, DECLARED EMERGENCY LANDING 18C. INSPECTED INTAKE AND EXHAUST. NO DEFECTS NOTED. BOROSCOPE INSPECTESDR HALA0500208Engine · stalledATB - LT ENGINE, AT ABOUT 300 FT STALLED ONCE, PRIOR TO POWER REDUCTION- (2) PRIOR TO POWER REDUCTION AT ABOUT 600 FT. RT ENGINE STALLED ONCE. AIRCRAFT DIVERTED, WHERE AN UNEVENTFUL LANDING WAS MADE. REPAIR IN WORK. (K)SDR AT0500009Engine · inoperativeON CLIMBOUT ENGINE LEFT SURGE ALERT CAME ON. ALL ENGINE PARAMETERS NORMAL. AT ABOUT 13,000 LEFT ENGINE FAILED, SEVERE DAMAGE SUSPECTED. REPLACED ENGINE.SDR GUU2005F00013Blade · failedDURING FLIGHT, DETECTED SMOKE IN THE COCKPIT AND CABIN. RT ENGINE LOW PRESSURE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED RT ENGINE. OPERATIONAL CHECK NORMAL. NOTE: VERIFIED TO BE 2ND STAGE PT BLADE FAILURE. (K)SDR BJNA05021Engine · failedNR 2 ENGINE FAILED ON THE BEGINNING OF TAKEOFF ROLL, 1.6 EPR HARD COMPRESSOR STALL AND ROLL DOWN. INSPECTION REVEALED EXTENSIVE DAMAGE TO THE T-1 THROUGH T-4 TURBINE BLADES, TURBINE FAILURE WAS CONTAINED. ENGINE TOTAL TIME 550207, TOTAL CYCLES 52176. SINCE SDR 2005F00045Engine · malfunctionedFLT - FLL/EYW - DURING FLIGHT, DETECTED SMOKE IN THE COCKPIT AND CABIN. RIGHT ENGINE LOW PRESSURE ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE. OPERATIONAL CHECK NORMAL. (M)SDR CA050214004Engine · smoke(CAN) DURING PUSH BACK, SMOKE WAS OBSERVED IN THE CABIN AREA WHILE ENGINES WERE BEING STARTED. THE AIRCRAFT RETURNED TO THE GATE. ENGINE STARTS WERE CARRIED OUT AT THE GATE AND THE SMOKE WAS NO LONGER OBSERVED IN THE CABIN. DE-ICING FLUID WAS SUSPECTED. NOSDR O3X02098711Engine · shutdownAIRCRAFT DEPARTED, ENROUTE, ON DESCENT, AT APPROX 1900 FT, THE RT ENGINE SHUT ITSELF DOWN. THE CREW PERFORMED EMERGENCY PROCEDURES, CLIMBED TO APPROX 6000 FT, AND SUCCESSFULLY RESTARTED THE ENGINE. CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. (K)SDR MALA050141Bearing · failedCREW REPORTED LOUD BANG, FOLLOWED BY CHIP LIGHT, OIL PRESSURE LOSS, AND OVERTEMP. IN FLIGHT SHUTDOWN. NR 2 BEARING FAILURE. NO FURTHER INFO AT THIS TIMESDR C2XA05IA024Bevel Gear · brokenBTR - FLIGHT 3334, THE CREW REPORTED THAT THE NR 2 ENGINE SHUTDOWN IN FLT. THE AIRCRAFT DIVERTED TO BTR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WAS APPRSDR DL73S050091Engine · malfunctionedFLT 7000 FT CLIMB EPR 250 - CLIMBING CLEAN HEARD LOUD BOOM WITH A/C SHUDDER ONCE. ALL ENG IND NORM AND STEADY. PNEU NORM. NO VISIBLE DAMAGE FROM CABIN F/A'S. ATB CVG UNEVENTFUL. DECLARED EMERGENCY WITH CVG DEPT CONTROL. BORO BOTH ENGINES, OK. FOUND LEFTSDR AU510001555Engine · bird ingestionRT ENGINE BIRDSTRIKE. THREE FAN BLADES DAMAGED BEYOND LIMITS LAID DOWN IN MAINTENANCE MANUAL.SDR CA050621006Engine · failedDURING FLIGHT, ENGINE OIL PRESSURE AND TURBINE TEMPERATURES WERE REPORTED TO RISE, FOLLOWED BY AN OIL PRESSURE REDUCTION AND FLAMES EMANATING FROM THE EXHAUST. THE PILOT SHUT THE ENGINE DOWN IN FLIGHT AND COMPLETED A DEAD-STICK LANDING. MFG WILL MONITOR THE ISDR CA050213006Engine · failed(CAN) DURING FLIGHT ENGINE OIL PRESSURE AND TURBINE TEMPERATURE INCREASED. OIL PRESSURE SUBSEQUENTLY REDUCED, ACCOMPANIED BY FLAMES FROM THE ENGINE EXHAUST. THE PILOT SHUT THE ENGINE DOWN IN FLIGHT AND CARRIED OUT AN EMERGENCY LANDING. MFG WILL MONITOR INVESDR IXXA0500015OEngine · failedDURING CLIMBOUT FROM KBWI, NR 4 ENGINE OIL PRESSURE LIGHT CAME ON. OIL PRESSURE/QUANTITY NORMAL. OIL TEMP WAS SLIGHTLY HIGHER THEN OTHERS AT 105C. COMPLETED CHECKLIST AND LIGHT WOULD NOT GO OUT. CREW SHUT DOWN ENGINE INFLIGHT THEN DIVERTED AIRCRAFT TO KWRISDR DHL2005760005Engine · flamed outENGINE NR 1 FLAMED OUT AFTER 30 SEC OF IDLE. ATTEMPTED 2ND START PER MX CONTROL, NO LIGHT OFF, NO FUEL FLOW. PERFORMED ABNORMAL PROCEDURE PER AOM. ATTEMPTED ANOTHER START WITHOUT ANY PROBLEM. ENGINE IDLES NORMALLY. RESET FIRE HANDLE AND ATTEMPTED RESTART.SDR RAIA00502002Engine · vibrationBWI - LT OIL CONTAM LIGHT IN-FLIGHT ENGINE STATS GOOD BUT FELT VIBRATION IN LEFT ENGINE. MAINTENANCE PERFORMED MAG-CHIP ADJUSTMENT/TEST. OPS CHECK AND NO ENGINE VIBRATION'S NOTED AT THIS TIME.SDR CA050329004Engine · malfunctioned(CAN) DURING CRUISE, ENGINE TORQUE INCREASED UNCOMMANDED, ACCOMPANIED BY A LOW OIL PRESSURE WARNING ANNUNCIATION WITH OIL PRESSURE DECREASING TO ZERO. THE ENGINE WAS SHUTDOWN IN FLIGHT AND SUBSEQUENTLY REMOVED FOR INVESTIGATION. MFG WILL INVESTIGATE THE INCISDR CA050213003Engine · making metal(CAN) A CHIP DETECTOR WARNING ANNUNCIATED IN FLIGHT, REPORTED AS ACCOMPANIED BY PROPELLER SPEED FLUCTUATIONS. SUBSEQUENT INSPECTION REVEALED METAL PARTICLES AT THE CHIP DETECTOR AND OIL FILTER LOCATIONS. PWC WILL INVESTIGATE THE EVENT AND WILLSUPPLEMENT THISSDR SIMA200503403Engine · damagedDURING CLIMB AND CRUISE, NR 2 ENGINE HIGH ITT. FOUND CUSTOMER SERVICE MANIFOLD HAD COME OFF ENGINE. REPLACE NR 2 ENGINE ASSY. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE.SDR P5CAO501312Engine · stalledDURING CRUISE AT FL 310, NR 3 ENGINE COMPRESSOR STALLED, EGT WENT TO 500 DEGREES, N1 50 PERCENT, N2 40 PERCENT. PERFORMED RESTART THE ENGINE WOULD NOT START PAST 30 PERCENT N1, 40 PERCENT N2, WITH EGT AT 625 DEGREES & F/F AT 400 PPH. THROTTLE MOVEMENT HAD NOSDR C2XA05IA017Engine · damagedIAH - FLIGHT 2720, THE CREW REPORTED THAT DURING FLIGHT THEY SMELLED A BURNED PACK SMELL WITH NO INDICATION OF SMOKE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, ANSDR CA050213002Engine · failed(CAN) DURING CRUISE THE ENGINE LOW OIL PRESSURE INDICATOR ANNUNCIATED. THE ENGINE WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION EVIDENSED NOISE FROM THE REDUCTION G EAG THE PROP. MFG WILL INVESTIGATE THE EVENT AND WILL SUPPLIMENT THIS REPORT TO PROVIDE ROOSDR CA050208001Engine · failed(CAN) ENG SUFFERED ONLY MINOR DAMAGE FROM PROP STRIKE WHICH WERE TIP RUBS IN COMPRESSOR, PWR TURBINE COMPONENTS. TIP RUBS FOUND ON PT BLADE PATHS ARE CONSIDERED TO BE MINOR AND NOT UNCOMMON TO FIND AT ANY DISASSEMBLY EVEN AFTER ONLY 77 HOURS OPERATION SINCE THSDR 2005FA0000122Engine · making metalPILOT REPORTED HEARING A GRINDING NOISE FROM THE ENGINE WHICH WAS FOLLOWED BY AN ENGINE CHIP LIGHT INDICATION. A POWER ON PRECAUTIONARY LANDING WAS MADE. THE ENGINE WAS REMOVED AND REPLACD WITH A LOANER ENGINE. THE DISCREPANT ENGINE AS AN ASSEMBLY WAS SENT SDR COMA0560117Engine · malfunctionedFLIGHT 5852 RT ENGINE OIL PRESSURE WARNING. REPLACED THE RT ENGINE.SDR AALA20050111Engine · malfunctionedMAN - CLIMBING AT FL280 LEFT ENGINE EXPERIENCED TWO COMPRESSOR STALLS. INDICATION ACCOMPANIED WITH HIGH VIBRATION. N2 VIBRATIONS WERE FIVE UNITS. ENGINE POWER WAS REDUCED TO IDLE FOR DESCENT AND LANDING. EVENT RECORD SWITCH PRESSED AT IDLE POWER. LATER ONSDR MALA050231Engine · failedNR 1 ENGINE FAILED IN FLIGHT, HEARD A LOUD BANG, ENGINE SHUT DOWN. THE AIRCRAFT WAS INSPECTED IAW THE MESABA REQUIREMENT AS LISTED ON THE 3 ENGINE FERRY 02 TASK CARD AND WAS FOUND TO BE SAFE FOR THE INTENDED FERRY FLIGHT FROM DTW TO MSP. APU MUST BE RUNNING SDR 2005F00035Engine · malfunctionedLGA - FLT 706 - AT 4,000 FEET, ON CLIMB-OUT, AFT CABIN FILLED WITH SMOKE, LAV SMOKE DETECTOR WENT OFF, TURNED RIGHT ACM OFF AND EMERGENCY RETURN TO LGA, SMOKE DISIPATED AFTER LANDING. REMOVED AND REPLACED NR 2 ENGINE. PERFORMED BURN OUT OF HIGH PRESSURE PNEUSDR 2005F00018Engine · fireON CLIMB, RIGHT ENGINE CAUGHT ON FIRE. ENGINE WAS SHUT DOWN AND RETURNED TO THE AIRPORT. REPLACED ENGINE FOR EVALUATION. (M)SDR CA050128001Engine · malfunctioned(CAN) DURING TAKE-OFF, THE CREW OBSERVED NR 2 ENGINE EPR GAUGE NOT WORKING. TAKE-OFF WAS REJECTED AND AIRCRAFT RETURNED TO THE GATE. NR 2 ENGINE EPR DEFERRED IAW MEL 77-1 AND DMI NR 10956 RAISED. ALL OTHER ENGINES PARAMETERS NORMAL. AIRCRAFT RELEASED AND NSDR CA050213001Engine · failed(CAN) DURING CLIMB THE ENGINE LOST POWER ACCOMPANIED BY A LOUD NOISE AND VIBRATIONS. THE ENGINE WAS SHUT DOWN IN FLIGHT AND THE AIRCRAFT RETURNED TO POINT OF DEPARTURE. SUBSEQUENT INSPECTION REVEALED DAMAGE TO THE TURBOMACHINE MODULE. MFG WILL MONITOR THE ISDR MALA050212Processor · malfunctionedAFTER ENGINE START NR 1 LOW OIL PRESSURE LIGHT CAME ON. OIL PSI SHOWED BETWEEN 40 AND 50 PSI (GREEN ARC). OIL PRESSURE GOOD 80 PSI WHEN ENGINE NR 1 AT 80 PERCENT. NR 2 OIL PRESSURE LIGHT NEVER WENT OUT, RETURNED TO GATE. AIRCRAFT TO BE FERRIED TO MSP FOR RSDR DL73S050060Engine · malfunctionedAFTER TAKEOFF WHEN THROTTLES RETARDED NR 2 ENGINE REMAINED AT 1.6 EPR. REPLACED FUEL CONTROL.SDR 2005FA0000421Engine · failedWHILE AT FL300, EXPERIENCED AN INFLIGHT FAILURE OF THE RT ENGINE AS FOLLOWS, RT ENGINE INSTRUMENTS, ITT, N1, N2 AND FUEL FLOW ALL BEGAN INCREASING. RT FUEL COMPUTER WAS TURNED OFF, POWER WAS REDUCED TO IDLE. THE ENGINE INSTRUMENTS CONTINUED TO INCREASE AND JSDR ARWA20050106Engine · malfunctionedNR 1 ENGINE OIL PRESSURE LIGHT ILLUMINATED; OIL PRESS GAUGE INDICATED 25 PSI, FOLLOWED BY A LOSS OF OIL QUANTITY, WENT TO ZERO. PERFORMED OIL PRESSURE LIGHT ILLUMINATED CHECKLIST; THEN, PERFORMED IN-FLIGHT ENGINE SHUTDOWN ABNORMAL CHECKLIST. ENGINE SHUTDOWN SDR AALA20050055Engine · shutdownDFW - ON CLIMB-OUT AT 8500 FEET, HEARD LOUD BOOM FROM RIGHT ENGINE. ENGINE SPOOLED DOWN TO WINDMILL. WINDMILLED FOR 16 MINUTES. DOWNLOADED FLIGHT DATA RECORDER PER ENGINEERING. REPLACED NUMBER TWO ENGINE. SYSTEM GROUND CHECKED NORMAL OPERATION.SDR AALA20050054Engine · inoperativeDFW - FIFTEEN MINUTES BEFORE LANDING THE RIGHT ENGINE OIL QUANTITY WENT TO ZERO. AFTER A COUPLE OF MINUTES THE AMBER LOW OIL QUANTITY LIGHT CAME ON QUICKLY FOLLOWED BY THE RED LIGHT. THE RIGHT ENGINE WAS SHUTDOWN PER CHECKLIST. THE SHUTDOWN WAS NORMAL. THENSDR DHL2005760004Engine · shutdownNR 1 ENGINE AUTO-SHUTDOWN WHEN NR 2 ENGINE WAS STARTED. RESTARTED NR 1 ENGINE, NO DEFECTS NOTED.SDR CA050214002Engine · inoperative(CAN) FOLLOWING FIRST START OF THE DAY THE ENGINE EXPERIENCED AN UNCOMMANDED N2 ACCELERATION. THE PILOT SHUT THE ENGINE DOWN. MFG WILL INVESTIGATE THE EVENT AND WILL SUPPLEMENT THIS REPORT TO PROVIDE ROOT CAUSE, ONCE DETERMINED.SDR CA050126009Engine · leaking(CAN) IN CRUISE, THE ENGINE OIL PRESSURE REDUCED ACCOMPANIED BY A LOW OIL PRESSURE INDICATION. THE PILOT SHUT THE ENGINE DOWN, DECLARED AN EMERGENCY AND DIVERTED THE FLIGHT. SUBSEQUENT INSPECTION REVEALED EXTERNAL OIL LEAKAGE. MFG WILL INVESTIGATE THE EVENT
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