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 CA120319002Engine · malfunctioned(CAN) ACFT DEPARTED ON LEG 3 OF A 3 LEG MISSION. PRE-FLIGHT AND PREVIOUS LEGS WERE UNEVENTFUL. ON DEPARTURE AND CLIMBING THROUGH 12,000 FT, FIRE WAS OBSERVED FROM THE NR 2 ENGINE STACKS. THE ENGINE WAS SHUTDOWN IAW THE CHECK LIST AND FIRE EXTINGUISHED. ACFSDR WX0A071135Engine · vibrationFLIGHT CREW REPORTED LOUD BANG AND SHUDDER FROM RIGHT ENGINE THROUGH FLIGHT LEVEL 270. FOLLOWED BY VIBRATION. PRECAUTIONARY ENGINE SHUTDOWN ACCOMPLISHED. MAINTENANCE PERSONNEL REMOVED AND REPLACED RIGHT ENGINE ASSY IAW TASK CARD R0807101 AND WORK ORDER 0161SDR SWAA2012030802014Engine · failedINFLIGHT SHUTDOWN/DIVERSION/DECLARED EMERGENCY - DURING CRUISE FL390 NR 2 ENG APPEARED TO COMPRESS OR STALL AND FAILED. N2 RPM WENT TO 0 WITH N-1 RPR AT APPROX 20 PERCENT DIVERTED AND ATTEMPTED RESTART AT 240. NO N2 RPM OBSERVED. REMOVED AND REPLACED NR 2 ESDR CA120312007Engine · making metal(CAN) (XIAN, MA60) FOLLOWING AN ENGINE SOUND ASSOCIATED WITH HIGH TEMPERATURE, THE PILOT ELECTED TO SHUT THE ENGINE DOWN BEFORE RETURNING TO THE POINT OF ORIGIN WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE. POST FLIGHT INSPECTION FOUND NO OIL VISIBLE OSDR AALA20120305006Engine · failedLIT - INFLIGHT DFW-MEM. CREW REPORTED LOSS OF RIGHT ENGINE OIL PRESSURE AND QUANTITY IN FLIGHT. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT DIVERTED LIT LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLSDR SWAA2012030802006Engine · failedDIVERSION/DECLARED EMERGENCY/ IN FLIGHT SHUTDOWN -- NR 1 ENGINE HAD INFLIGHT SHUTDOWN. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR UALA2012030201294Engine · surgesNR 1 ENGINE SURGED DURING HIGH POWER RUN. NOTE BLEED SHIFTED AT 79% N2, DUCT PRESSURE 35 PSI QUICKLY DROP TO 26 AND RETURNED BACK TO 36 AT N2 92.7% AT HIGH POWER. THEN ABOUT 20 SECONDS ENG SURGED. WINDS SPEED WAS 0. ACCOMPLISHED ENGINE SURGE INSPECTION ANDSDR CA120312005Engine · power loss(CAN) ON TAXIING OFF THE RUNWAY, CREW REPORTED DOUBLE ROLLBACK. THE LT ENGINE IMMEDIATELY REST BUT THE RIGHT ENGINE DID NOT RESPOND TO CONTROL INPUTS. CREW DECIDED TO SHUTDOWN ENGINES AND CALLED FOR A TOW BACK.SDR UALA2012030101293Unknown · malfunctionedABORTED TAKEOFF AT 100 KNOTS FOR LT ENG & SLOW TO RUN UP AT BRAKE RELEASE. LEFT ENGINE SPOOLED UP SLOW ON T/O ROLL. REJECTED T/O AT 100 KTS. ACCOMPLISHED VISUAL INSPECTION OF SVA ACTUATOR, LINKAGE, RODS AND RUNNER BLOCKS, FAN BLADES & TAIL PIPE ALL CHECK GOSDR ASAA12511181Engine · unknownCLIMBING THRU FL 260 NR 1 ENG EXPERIENCED LOTC. DIVERSION TIME: 28 MINUTES. MESSAGE 73 10331 RECORDED ON PREVIOUS LEG FOUND WHEN CHECKING EXCEEDANCES ON NR 1 ENG. REPLACED NR 1 ENGINE PER T/C 78471000.SDR CA120229007Engine · making metal(CAN) UPON LANDING NR 2 ENGINE CHIP LIGHT ILLUMINATED, ACFT SHUTDOWN. ENGINEER INSPECTED THE NR 2 SCAVENGE FILTER CHIP DETECTOR FOUND CHIP CLASSIFIED AS MINOR CATEGORY. DEBRIS AND CHIP DETECTOR CLEARED ACFT GROUND RUN RELEASED BACK TO SERVICE. UPON LANDING BSDR HALA2012022900093Engine · hung startLEFT ENGINE HUNG START, FUEL FLOW AND DUCT PRESSURE WERE NORMAL. HUNG AT 56 PERCENT N2 AND EGT 710 DEGREES WHEN START ABORTED. SECOND START NORMAL. GROUND START 1 & 2, NO DEFECTS NOTED ON NR 1 ENGINE.SDR WI5R201203010001Bolt · improper partDURING ON-WING REPLACEMENT OF A DIFFUSER ON ENGINE 216014, THE INCORRECT CONFIGURATION BOLT WAS FOUND INSTALLED IN THE SERVICE ISLAND OF THE DIFFUSER BEING REMOVED. INSTEAD OF THE PN MS9558-04, PLUG BOLT, THAT IS REQUIRED FOR THE THIS ENGINE, A PN 45947, SPECSDR CA120228012Bearing · failed(CAN) EIR PT6A 2012-022, DURING CLIMBOUT THERE WAS A LOUD BANG AND THE ENGINE WAS SHUTDOWN. O/H CONFIRMED THAT THE ENGINE HAD SUFFERED A BEARING FAILURE. AFTER REMOVAL OF THE ACCESSORY GEARBOX ASSY IT WAS NOTICED THAT THE NR 1 BEARING WAS BROKEN CAUSING SECOSDR NOCA02612Unknown · fireEXPERIENCED A TAIL PIPE FIRE DURING THE STEPS IN REMOVING THE NR 2 ENGINE (S/N 31811). THE AIRCRAFT SUFFERED SIGNIFICANT DAMAGE TO THE RT ENGINE PYLON, SURROUNDING UNDER WING PANELS, RT INBOARD FLAP CANOE AND THE RT INBOARD FLAP. A PRELIMINARY INVESTIGATION SDR QMLA2012022712031Engine · making metalACFT HAD TWO MINOR, NR 2 ENGINE CHIP LIGHT EVENTS, EACH INVOLVING A FEW SMALL OR "LIGHT" CLASSIFIED PARTICLES ON THE FULL FLOW CHIP DETECTOR ONLY. EACH TIME THE DETECTOR WAS CLEANED AND A GROUND RUN PERFORMED WITH NO REPEAT OF THE CHIP LIGHT ILLUMINATED. AFTESDR BHKA201202270012Engine · overtempAFTER NORMAL START AND TAXI, THE ACFT BEGAN THE TAKEOFF ROLL. IMMEDIATELY AFTER THE "AIRSPEED'S ALIVE" CALL OUT (40 KNOTS) THE LT ITT READ 888 DEGREES C. THE TAKEOFF WAS IMMEDIATELY ABORTED WITH MINIMAL BRAKING (ACFT WEIGHT WAS 16,200). IN CHOCKS WITH BOTH SDR CA120312002Engine · fumes(CAN) DURING FLIGHT, UPON CLIMBOUT THROUGH 5000 FT, CABIN STARTED TO FILL UP WITH FUMES AND SMOKE. OXYGEN MASKS WERE DONNED AND BOTH ENGINES BLEED AIR TURNED OFF. EMERGENCY DECLARED, ACFT DIVERTED BACK TO DEPARTING AIRPORT. UNEVENTFUL LANDING. INVESTIGATION OSDR DXTA2012030804910Fuel Control · flamed outLEFT ENGINE FLAME OUT OR HUNG START, DURING EFC TEST. BOTH ENGINES STARTED NORMALLY ON GPU POWER. BOTH ENGINES FUNCTIONED NORMALLY OUT OF THE RAMP AREA. REPLACED THE LT ENGINE FUEL PUMP AND FUEL CONTROL IAW MM 73-20-00. LEAK AND OPS CHECKED GOOD.SDR DXTA2012022704888Engine · vibrationNR 1 ENGINE DISPLAYED HIGH VIBRATION, IE LP 2.25, IN FLIGHT. PRECAUTIONARY SHUTDOWN AND LANDING WITHOUT FURTHER INCIDENT. INSPECTED AIRCRAFT, NO DEFECTS NOTED.SDR FDEA201202240680Engine · flamed outDURING CLIMB OUT, LOST ENG NR 2 AFTER SHUTTING OFF ENG ANTI ICE AT ABOUT 18,000; RAN QRH AND RETURNED TO AIRPORT. ALL ENG INDICATIONS SEEMED NORMAL. ROLL BACK OF EGT AND N1 ONLY. CREW REPORTED THEY DID NOT TRY A RESTART. PERFORMED RIG CHECK OF FUEL LEVER ASDR UALA2012022301091Engine · making metalMETALLIC DEBRIS FOUND ON ENG NR 2 NR 5 BEARING SCAVENGE CHIP DETECTOR. METALLIC DEBRIS FOUND ON ENG NR 2 NR 5 BEARING SCAVENGE CHIP DETECTOR. REPLACED NR 2 ENGINE PER AMM. ACP'D FINAL INSTALL INSPECTION OF RPL'D NR 2 ENGINE PER AMM.SDR HSYA2012022312412Engine · contaminatedPILOT REPORTED DURING TAXI, A STRONG CHEMICAL ODOR IN COCKPIT. TAXIED ACFT BACK TO THE BLOCKS. FREIGHT INSPECTED AND NO DISCREPANCIES FOUND. MX TROUBLESHOT AND FOUND THAT THE APPARENT CAUSE TO BE RESIDUAL RECOVERY WASH FLUID FROM A COMPLETED COMPRESSOR TURSDR USAA2012022400015Engine · malfunctionedPHL FLT 751 EN ROUTE BRU TO PHL. DIRTY SOCKS SMELL NOTED IN COCKPIT AND CABIN 5 MINUTES BEFORE TOUCHDOWN, WHICH LASTED APPROXIMATELY 2 MINUTES, THEN DISSIPATED. MAINTENANCE REPLACED THE RIGHT ENGINE ASSEMBLY. HPC STAGE 5 BORESCOPE - ORGANIC DEPOSIT FOUND, SDR UALA2012022201072Engine · making metalNR 1 ENGINE VIBRATION, RTFL. LEFT ENGINE, SHORTLY AFTER TAKEOFF ALL ENG PARAMETERS DECREASED AND ENGINE SHUTDOWN. RETURNED TO DEPARTURE. ON ARRIVAL AT GATE, NO EXTERNAL LEAKS, MAIN CHIP DETECTOR HAS METAL PARTICLES. REPLACED NR 1 ENGINE.SDR CA120228004Engine · flamed out(CAN) DURING APPROACH, DESCENDING THROUGH FL30, THE ENGINE FLAMED OUT. THE CREW DID TRY TO RESTART THE ENGINE WITHOUT SUCCESS. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED AT DESTINATION. FOLLOWING THE FLIGHT, THE ENGINE WAS STARTED AND BROUGHT TO FLIGHT SDR CALA2012022100112Annular Filler · failedNR 2 ENGINE HAS HIGH VIBRATION. NR 2 ENG OIL PRESSURE FLUCTUATED. VIBRATION DECREASED AT IDLE TO 2.5, FOUND ANNULUS FILLER SEVERED IN HALF CAUSING ENGINE DAMAGE. REMOVED AND REPLACED NR 2 ENGINE IAW WC 29-7100-1-4900.SDR REXA2012022000041Engine · contaminatedAFTER TAKEOFF, FLIGHT ATTENDANT SMELLED BURNING PLASTIC. PILOTS CONFIRMED AN ODOR. RETURN TO DEPARTURE. IDENTIFIED ODOR AS ENGINE WITH SOAP, RESIDUAL FROM ENGINE WASH ON RT ENGINE. RAN ENGINES TO 85 OIL TEMP WITH PACKS ON FULL HOT UNTIL ODOR DISSIPATED. SDR CA120228003Engine · power loss(CAN) SHORTLY AFTER INITIATING DESCENT AT FL390, THE PILOT RECEIVED AN ELECTRIC ENGINE CONTROL REVERSION TO MANUAL WARNING AS POWER WAS BEING REDUCED. ACFT VIBRATIONS WERE ALSO NOTICED. THE CREW RAN THE EMERGENCY CHECK LIST TWICE TO RESTORE ENGINE CONTROL WITSDR USAA2012022100016Engine · leakingUPON DESCENT TO RSW, CREW REPORTED DIRTY SOCK FUMES PRESENT THROUGHOUT CABIN AND COCKPIT. CREW PLACED PACKS ON HIGH TO GET MAXIMUM VENTILATION. ODOR WASN'T AS BAD WITH PACKS ON. FLIGHT LANDED AT RSW WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAISDR CA120228002Sense Line · fractured(CAN) WHEN SETTING POWER JUST BEFORE TAKEOFF, DG GEN AND HYDRAULIC PUMP WARNINGS OCCURRED. THE ENGINE PARAMETERS, NH AND NP SPEEDS WERE LOW, AND TEMPERATURE HIGH. THE ENGINE DID NOT RESPOND TO POWER LEVER MOVEMENTS AND THE ENGINE WAS SHUTDOWN. AFTER ELECTRICASDR QMLA2012021712020Engine · making metalFOUND NR 2 ENGINE COMBUSTION DRAIN VALVE WAS NOT WORKING, REMOVED DRAIN FOR REPLACEMENT AND FOUND A PIECE OF METAL WEDGED INTO COMBUSTION DRAIN VALVE. METAL PIECE REMOVED FROM THE DRAIN VALVE IS APPROX. 0.278 L X 0.272 W X .028 THICK WITH 3 BROKEN EDGES AND SDR AALA2012021700001Engine · failedCREW REPORTED ON INITIAL DESCENT WHEN THROTTLES STARTED BACK THEY FELT A THUMP AND SAW THE LEFT ENGINE HAD FLAMED OUT. UNCOMMANDED ENGINE SHUTDOWN (SINGLE ENGINE TIME 20 MINS). NO ATTEMPT WAS MADE TO RESTART. CREW ALSO HAD A EICAS STATUS MESSAGE: "L ENG LP SDR UALA2012021700963Engine · vibrationDUE TO REPEAT VIB IND HIGHER THAN NORMAL TO PREVENT IRREG OPS, ACCOMPLISH FAN BLADE ROOT LUBE. `WILL REQUIRE VIBRATION SURVEY (HIGH POWER RUN), TEST NR 8 PER AMM. ACP'D TEST NR 8 VIBRATION SURVEY. TEST FAILED, (N1 VIB) INDICATES 4.2 AT 78% N1 AND (BB VIB) WSDR CA120312001Engine · shutdown(CAN) DURING APPROACH, THE ENGINE SHUTDOWN ITSELF UNDER UNKNOWN CIRCUMSTANCES. THE ACFT LANDED AT DESTINSTION WITHOUT FURTHER PROBLEMS. THE ENGINE WAS REMOVED AND FORWARDED TO EADS SECA WHERE AN INVESTIGATION WILL TAKE PLACE STARTING 27 FEB.SDR CA120220001Engine · malfunctioned(CAN) DURING CLIMB, ACFT HAD UNCOMMANDED AUTOFEATHER ON NR 2 ENGINE. CREW SHUTDOWN NR 2 ENGINE AND DECLARED AN EMERGENY WITH ATC. FLIGHT LANDED WITHOUT FURTHER INCIDENT. ENGINE NR 2 REPLACED AND ENGINE RUN CARRIED OUT FOUND SATISFACTORY.SDR REXA2012021500235Blades · vibrationABORTED TAKEOFF DUE TO RT ENGINE FAN VIBRATION . REMOVED & REPLACED 18 FAN BLADES ON RT ENGINE IAW AMM 72-20-00.SDR IPXA2M71696Engine · flamed outIN ICING CONDITIONS UNTIL 12,000 FT LEAVING FL 18.0 ENG 2 RPM LOW. ILLUMINATED FUEL FLOW NR 2 WENT TO 70 N2 RPM WAS 20 PERCENT, SELECTED ENGINE IGN OVRD ON AND ENGINE RECOVERED. ACCOMPLISHED NR 2 ENGINE BOROSCOPE AS A PRECAUTION. ACFT OK FOR SERVICE.SDR REXA2012021400225Plug · missingRT ENG TAIL CONE HAS EVIDANCE OF BURN DAMAGE. FOUND BOROSCOPE PLUG S50 MISSING. REPLACED BOROSCOPE PLUG IAW AMM 72-00-00. REMOVED AND REPLACED RT EXHAUST FAIRING IAW AMM 78-11-01.SDR FDEA201202130567Engine · stalledON TAKEOFF ROLL AT APPROX 60 KTS LARGE COMPRESSOR STALL FROM 1 MOTOR WITH YAW AND LARGE VIBRATION. REJECTED TAKE-OFF. NR 1 SHOWED EGT EXCEEDANCE AND N1 WITH (X)- NO ROTATION. SHUTDOWN ENGINE, PULLED FIRE HANDLE. RETURNED TO RAMP. ENGINE REPLACED. DUE TSDR ASAA12511095Engine · vibrationAT 15 000 FT 71% N ENG VIB INDICATES .4 ON NR 1 .2 ON NR 2. TACTILE VIBRATION FELT IN RUDDER PEDALS PILOT SEATS FLOOR AND THROTTLES. ENG NR 1 THROTTLE VIBRATES THE MOST. VIBRATION FELT FROM 71.7 TO 69.3 NI. WITH ENG NR 1 SET AT 73 PERECENT AND ENG NR 1 THROTSDR HSYA201202121Engine · failedDURING CLIMB OUT FOR A STAGING FLIGHT, CREW PULLED THROTTLE BACK AT APPROX 4000 FT, NR 1 ENGINE MADE A POPPING NOISE, FOLLOWED BY TORQUE DECREASING TO 2100 FT LBS, FOLLOWED BY AN ADDITIONAL POPPING NOISE FROM THE NR 1 ENGINE. THE CREW PULLED THE POWER ON THESDR AALA20120210MIA02Engine · failedMIA - CREW REPORTED LEFT ENGINE OIL LOSS. LEFT ENGINE SHUTDOWN (SINGLE ENGINE TIME 20 MINS). EMERGENCY DECLARED FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE AT MIA ON 02/14/2012. SYSTEM GROUND CHECK NORMAL OPERATSDR AALA20120208JFK01Engine · failedJFK - CREW REPORTED A SOUND AS IF GEAR DOOR CLOSED, THEN NUMBER 2 FIRE WARNING. CAPTAIN DISCHARGED BOTH FIRE BOTTLES. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 12 MINS). EMERGENCY DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FSDR AALA20120208TUL02Engine · failedCREW REPORTED LEFT ENGINE SURGE AND FIRE INDICATION. EMERGENCY DECLARED FLIGHT RETURNED EZE LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT ENGINE ON 02/13/2012. SYSTEM GROUND CHECK NORMAL OPERATION.SDR SWIA201229555Bushing · corrodedRIGHT ENGINE THRUST SHAFT BUSHING HAS PITTING. (SERVICE) REPLACED RIGHT ENGINE THRUST SHAFT BUSHING.SDR SWIA201229540Engine · malfunctionedSMOKE IN REAR OF AIRCRAFT. RECEIVED A TRIPLE CHIME SMOKE ON MAP. (FLT 5621) REPLACED RIGHT ENGINE ASSEMBLY. PN: PW118B, SN OFF: AP0052.SDR UALA2012020600706Breather Tube · dentedFOUND NR 3 BREATHER TUBE PN 50U795-01 DENTED BEYOND LIMITS. REPLACED NR 3 BREATHER TUBE AND SAFETIED.SDR UALA2012020300670Engine · damagedBIRDSTRIKE, RTFL. ON CLIMB OUT AIRCRAFT EXPERIENCED A BIRD STRIKE, FOLLOWED BY ENGINE NR 2 VIBRATION. REFER TO MT72-021 FOR INSPECTION REQUIREMENTS. ENGINE REPLACEMENT REQUIRED DUE FOD INGESTION. REPLACED ENG PER MT71-017.SDR CA120213012Engine · surges(CAN) DURING MAINTENANCE FLIGHT, ON TAKEOFF THE CREW FELT 1 ENGINE SURGING. PILOT RETARDED POWER LEVER TO IDLE. ACFT RETURNED TO BASE FOLLOWED BY UNEVENTFUL LANDING. TROUBLESHOOTING ONGOING.
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