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 MASA2011033102288Engine · malfunctionedLEFT ENG OIL PRESS WARNING & READING 0 ON DESCENT INTO ABQ. CREW PULLED THE NR 1 THROTTLE BACK TO IDLE AND CONTINUED THE DESCENT. MX REMOVED AND REPLACED LT ENGINE, ENG RUN C/W.SDR TRBA2011030Seal · failedDURING IDLE DESCENTS, BOTH HP VALVES ON, EXHAUST ODOR COMES THROUGH AIR SYS. R & I NEW PROBE DUMMY PLUG SEALS ON NR 2 ENGINE IAW MM 72-01-60. OPS CHECK GOOD NO EXHAUST ODORS AT THIS TIME. NO LEAKS NOTED AT PROBE.SDR KCSA11016Engine · flamed outAT 1307Z, FL350, STABLE CRUISE FLIGHT, DURING FUEL HEAT APPLICATION, NR 1 ENG FLAME OUT. PERFORMED INFLIGHT ENGINE FAILURE/SHUTDOWN. OIL PRESS 14 PSI. ENG WINDMILLED APPROX 9 MINUTES. NO PARAMETERS EXCEEDED. IN-FLIGHT START SUCCESSFUL. NO CAUTION/WARNINGSSDR UHLA2011032500131Engine · leakingCREW REPORTS SMELL OF SMOKE IN THE CABIN/COCKPIT AFTER TAKEOFF. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. RAN ENGINE, FOUND EVIDENCE OF LEAK AT NR 2 ENG A SUMP. CONSUMPTION MINIMAL, WITHIN LIMITS IAW GE MM 72-00-00. FERRIED TO IND. REMOVED AND REPLACEDSDR KCSA11014Engine · power lossAT 0600Z IN STABLE CRUISE, FL350- SMOOTH AIR, IGNITION ON, FUEL HEAT ON, NR 1 ENG ROLLED BACK - MIN OIL PRESS 35 PSI - NO PARAMETERS EXCEEDED - NO FIRE SWITCH PULLED - NO CAUTION / WARNINGS. 2 RAPID RESTARTS DURING APPROX 3 MINUTES. ENG STARTED BUT NO ACCL USDR KY7A20110203Engine · failedE2 INDICATIONS WERE NORMAL DURING TAXIING OUT. AFTER ACFT GOT TO ABOUT 30 PERCENT TORQUE, HEARD A POP FROM THE RT SIDE OF THE AIRPLANE AND NOTICED THE RT SRL OFF LIGHT ILLUMINATE, SAW ENGINE SPOOLING DOWN. PULLED STOP & FEATHER, REDUCED POWER ON LT ENGINESDR CA110331012Engine · shutdown(CAN) IFSD AFTER T/O, THE NR 2 ENGINE SUFFERED AN UNCOMMANDED SHUTDOWN. THE CREW PERFORMED AN AIR TURNBACK AND AN UNEVENTFUL SINGLE ENGINE LANDING FOLLOWED AT ORIGIN AIRPORT. TROUBLESHOOTING IS ON-GOING.SDR CA110323001Engine · failed(CAN) ENGINE SENT FOR OVERHAUL AFTER OPERATOR REPORTED FLAMES OUT OF EXHAUST DURING FLIGHT. BELIEVES THAT THE ENG INTERNAL FAILURE HAPPENED WHEN ONE OF THE COMPRESSOR TURBINE BLADES, PN 302340, FAILED AS A RESULT OF A POSSIBLE FATIGUE CRACK. THE SUBSEQUENT ISDR ASMF20110322001Bolt · looseCAPTAIN REPORTED DURING THE DESCENT, THE RT ENGINE VIBRATION REACHED 4.7 OF N2. ACFT WAS SENT TO THE HANGAR AND MX PERFORMED A TRIM BALANCE IAW MM 71-00-00 TASK 71-00-00-700-847-G01 DETECTING 6 RT ENGINE FAN WEIGHT BALANCE BOLTS WERE LOOSE AT THE 5, 11, 12, SDR C2XA11IA059Engine · vibrationIAH - FLIGHT 2482 IAH-GPT, THE CREW REPORTED ENGINE TWO VIBRATION IN AMBER FOR 2-3 SECONDS DURING CLIMB, AND AFTER POWERING BACK THE VIBE RETURNED TO GREEN RANGE, RETURNED AIRCRAFT TO CLIMB POWER AND VIBRATION STABILIZED BETWEEN 2.0 AND 2.4 IPS. THE AIRCRAFT SDR MASA2011032202220Engine · overtempNR 1 ENGINE OVERTEMP ATO RTG. MX RAN ENGINE PER AMM COULD NOT DUPLICATE.SDR CA110321001Bearing · failed(CAN) THIS ENGINE WAS SENT FOR INVESTIGATION & REPAIR AFTER THE OPERATOR REPORTED METAL CONTAMINATION OF THE RGB OIL SYS. WAS ABLE TO CONFIRM THE OPERATORS REPORT OF METAL CONTAMINATION OF THE RGB OIL SYS. THE SOURCE OF THE METAL CONTAMINATION WAS DETERMINEDSDR COEA2011031801756Engine · contaminatedFLIGHT 8676 FORM ANC TO HOM: DURING THE TAKEOFF ROLL, PILOT OBSERVED SMOKE OR STEAM IN THE COCKPIT, ALONG WITH A HOT SMELL. PILOT ABORTED THE TAKEOFF, CLEARED THE RUNWAY AND DECLARED AN EMERGENCY. UPON INITIAL INSPECTION IT WAS DETERMINED THE ENGINE WAS SOASDR AALA20110317CUN01Engine · failedCUN - CREW REPORTED RIGHT ENGINE FIRE INDICATION ILLUMINATED IN FLIGHT WITH OVERHEAT AMBER EICAS MESSAGE. BOTH FIRE BOTTLES WERE DISCHARGED. RIGHT ENGINE SHUT DOWN (SINGLE ENGINE TIME 25 MINUTES). EMERGENCY DECLARED FLIGHT RETURNED CUN LANDED WITHOUT INCIDESDR NSVA2011053Engine · malfunctionedCRUISE, 15-20 MINS EAST OF PIT RECEIVED AN INDICATION OF NR 1 OIL PRESS LIGHT AND BEFORE THEY WERE ABLE TO RUN THE CHECKLIST RECEIVED THE NR 1 ENGINE FIRE LIGHT. RAN THE CHECKLIST AND SHUTDOWN THE ENGINE, F/O SMELLED SMOKE AFTER THEY USED THE FIRE BOTTLE. BRSDR REXA201100185Engine · malfunctionedON TAKEOFF ROLL FROM KMCI THE FLIGHT CREW HEARD A LOUD NOISE FROM THE RIGHT ENGINE FOLLOWED BY HIGH ITT INDICATION AND ENGINE SHUTDOWN. THE FLIGHT CREW ABORTED THE TAKEOFF. AFTER INSPECTION OF THE AIRCRAFT BY CFR THE AIRCRAFT RETURNED TO THE GATE. OUTSTATIOSDR CA110322001Engine · failed(CAN) MARCH 16TH, 2011, 11:20 PM, DIVERTED DUE TO RISE IN ITT, FOLLOWED WITH AN ENG SURGE. THE CREW SHUT THE ENG DOWN & LANDED SAFELY AT THE AIRPORT. AS OF NOW ALL WE KNOW IS THAT THERE WAS AN INTERNAL ENG FAILURE. THE ENG WAS REMOVED & SENT FOR A TEAR DOWNSDR FDEA201103161013Engine · damagedDURING GEAR RETRACTION AND AFTER GEAR RETRACTED, WE HEARD A GRINDING NOISE AND SMELLED A STRONG ODOR THAT IS SIMILIAR TO SOMETHING BURNING (NOT ELECTRICAL). DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE FOR AN UNEVENTFUL LANDING. TURNED OUT WE HIT A SKUNK OSDR UALA2011031801304Engine · making metalNR 2 ENGINE LARGE METAL DEBRIS FOUND IN INTERMEDIATE PRESSURE CHECK VALVE DURING C-CHECK MAINTENANCE. BORESCOPE INSPECTED PER MM. NO LIMITING DEFECTS NOTED. REQUIRES FOLLOW UP BOROSCOPE INSPECTION. DUE TO METAL FOUND IN INTERMEDIATE CHECK VALVE FOLLOW UP BSDR CA110331005Engine · power loss(CAN) IFSD (SINGLE ENGINE) DURING T/O ROLL, A LOSS OF POWER OCCURRED ACCOMPANIED BY OIL SPLATTERING THE WINDSHIELD. THE T/O WAS ABORTED.SDR CA110331001Engine · shutdown(CAN) IFSD AFTER LANDING, THE CREW REPORTED AN UNCOMMANDED ENGINE SHUTDOWN WHILE TAXING. TROUBLESHOOTING IS ON-GOING.SDR CA110315011Engine · failed(CAN) AFTER TAKEOFF THERE WAS AN ENGINE STALL WITH FLAMES ON THE NR 1 ENGINE. THERE WAS SMOKE COMING INTO THE CABIN. THE FLIGHT DIVERTED WHERE HE DECLARED AN EMERGENCY AND LANDED APPROX. 7000K OVERWEIGHT. THE AIRCRAFT WAS INSPECTED BY CFR SERVICES BEFORE TAXIISDR GUUA94531031511AEngine · malfunctionedPILOT REPORTED NR 1 ENG N1 AND TORQUE DECREASED CONTINUOUSLY IN FLIGHT WHEN TORQUE REACHED 0 ENGINE SECURED. DIVERTED, LANDED WITHOUT INCIDENT. (OPEN)SDR UALA2011031501234Engine · faultyODOR IN CABIN, RTFL. STRONG ODOR FILLED CABIN CLIMBING THROUGH 10K CAUSING MID CABIN LAV SMOKE ALARM TO GO OFF. SAMC TEXT: FLT CREW DEBRIEFING - NOT ELECTRICAL SMELL. BURNING EYES ACCOMPANIED WITH OIL-GLYCOL TYPE OF ODOR. APU PNEUM NOT USED THROUGHOUT EVESDR IPXA1165411Engine · noneEMERGENCY DECLARED. IMMEDIATELY AFTER ROTATION HEARD LOUD BANG & SMELLED SMOKE IN COCKPIT. ALL COCKPIT ENGINE INDICATIONS WERE NORMAL. OCCURRED DURING GEAR RETRACTION. EVIDENCE OF BIRDSTRIKE IN NR 1 ENG. ACCOMPLISHED ENG BIRD STRIKE INSP IAW AMM 05-51-19-00SDR CA110331006Engine · power loss(CAN) POWER ROLL BACK DURING CLIMB, THE ENGINE POWER ROLLED BACK. THE CREW PULLED THE THRUST LEVER TO IDLE AND CONTINUED CLIMB WITH THE SECOND ENGINE. THE THRUST LEVER WAS READVANCED AT FL130, THE ENGINE RESPONDED WELL AND THE FLIGHT CONTINUED TO DESTINATION SDR CA110331003Engine · power loss(CAN) POWER ROLL BACK/IFSD DURING DECENT, THE CREW REPORTED ENGINE TORQUE ROLLED BACK AND THEN INCREASED BEFORE ROLLING BACK AGAIN. THE ENGINE WAS SHUTDOWN AND SECURED AND AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED. TROUBLESHOOTING IS ON-GOING.SDR CA110321005Engine · faulty(CAN) TAIL 833 CREW REJECTED THE TAKEOFF WHEN THE TORQUE INDICATION ON THE NR 2 ENG WENT TO ZERO BOTH ANALOG & DIGITAL. AFTER TALKING TO MX, THE CREW TRIED AGAIN & THEY DID ANOTHER REJECTED TAKEOFF. BOTH REJECTED TAKEOFFS WERE BELOW 80 KTS. ACFT REMOVED FORSDR RU3A1110Engine · power lossAPPROX 20 MIN INTO 2ND FLT, RT ENGINE ROLLED BACK TO IDLE DURING CLIMBOUT / LEVEL OFF AT 8900 MSL FOLLOWING LOW APPROACH. ROLLBACK WAS ACCOMPANIED BY SIGNIFICANT VIBRATION BUT NO ANNUNCIATORS. CREW BROUGHT RT THRUST LEVER TO IDLE, DECLARED AN EMERGENCY AND CSDR UALA2011031401216Engine · smokeREPORTED SMOKE FROM RIGHT ENGINE ON TAKEOFF. CREW DID A VISUAL CHECK FROM CABIN - SAW NOTHING. NOTHING ON DOWNLINKS FROM THE ACFT. ALL INDICATORS IN COCKPIT NORMAL. ALL IN AGREEMENT AT THIS TIME TO MONITOR AND CONTINUE ON TO ORD.SDR C2XA11TY027Engine · malfunctionedSMOKE IN CABIN. REMOVED AND REPLACED NR 2 ENGINE. OPS AND LEAK CHECK GOOD. AIRCRAFT RELEASED AND RETURNED TO SERVICE.SDR UIEA2011031100149Check Valve · failedBLOCK TURN BACK DUE NR 4 ENGINE FAILED TO ACCELERATE PAST 40 PERCENT N1, WITH HIGH EGT AND 4 COMPRESSOR STALLS WERE EXPERIENCED. (REPLACED 8TH STAGE CHECK VALVE AND PERFORMED ENGINE RUNUP. ALL OPERATES NORMAL. DUE TO COMPRESSOR STALL, BOROSCOPE INSPECTION ACCSDR CA110315009Engine · flamed out(CAN) FLAMEOUT AFTER T/O, THE ENGINE FLAMED OUT AFTER THE LANDING GEAR WAS RETRACTED. THE A/C RETURNED TO THE POINT OF DEPARTURE WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS MADE, TROUBLESHOOTING IS ON-GOING. +++++ (TC# 20110315009)SDR CA110315007Engine · malfunctioned(CAN) UNCOMMANDED ACCELERATION AFTER T/O, THE CREW REPORTED THAT BOTH ENGINES ACCELERATED BEYOND THE SET TAKE-OFF CLIMB POWER SETTING WITH NO PILOT INPUT. POWER WAS REDUCED MANUALLY, AND THE FLIGHT RETURNED TO THE POINT OF ORIGIN WHERE AND UNEVENTFUL LANDING WSDR FDEA201103090924Engine · overtempRT WINDSHEAR WARNING ON APPROACH TO RWY 14, MISSED APPROACH WITH FIREWALL POWER AT 640MSL & WENT TO CLIMB AT 1100MSL. NO ENGINE PAREMETERS OBSERVED. ANALYSIS CONFIRMED THE NR 1 & NR 3 ENG EGT, N1 & N2 WERE WITHIN LIMITS. NR 2 ENG EXPERIENCED & EGT OVERTEMP SDR ZP7A20110311001Engine · flamed outMX PERFORMED AN ADJUSTMENT ON THE FUEL DENSITY AND IDLE RPM ON THE LT ENGINE, WHICH REQUIRES A MAX ALTITUDE ACCELERATION CHECK IAW THE MM CHAP 72-00. FLIGHT CREW LT RDU FOR THE PURPOSE OF PERFORMING THIS CHECK. FLIGHT CREW CLIMBED AND STARTED THE CHECK AT FLSDR 2011FA0000163Engine · making metalDURING TAKEOFF THE PILOT EXPERIENCED AN ENGINE CHIP LIGHT AND RETURNED FOR LANDING. MX FOUND SMALL CHIPS ON THE LOWER ENGINE PLUG AND A SLIVER ON THE UPPER PLUG. THE ENGINE WAS REMOVED FROM THE ACFT AND SENT TO SERVICE FOR MX.SDR A6WA201140170Engine · flamed outAFTER 10,000 FT AND INCREASING TO CLIMB POWER, LEFT ENG ITT 854C, 62 DEGREE HIGHER THAN RT ENG ACARS`D MX, THEY REQUESTED CHECK WITH SPEED SWITCHES OFF, COMPLIED, NO DIFFERENCE NOTED REDUCED POWER, TURNED RT SPEED ON, NO DIFFERENCE. TURNED LT SPEED ON, ENGINESDR UALA2011030701111Union · leakingNR 2 ENG HAS HEAVY COKING ON VSV UNISON RINGS AT TOP OF ENGINE FROM FLUID LEAK AT PYLON. REMOVED & REPLACED NR 2 ENGINE.SDR 2DYA20110305001Engine · stalledACFT DEPARTED, FL 3-5-11 ON FLIGHT 5812 - DEPARTING AT 11,000' 280 KNOTS, EXPERIENCED A SERIES OF COMPRESSOR STALLLS ON NR 2 ENGINE. REDUCED THRUST ON ENGINE, RETURNED TO DEPARTURE. SUBSEQUENT VISUAL INSP OF NR 2 ENGINE INDENTIFIED METAL DEBRIS IN TAILPIPE. SDR SIMA201106701Engine · malfunctionedON FLIGHT 4521 THE CREW REPORTED A HEAVY OIL ODOR THROUGHOUT THE AIRCRAFT. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED NUMBER 1 ENGINE PER AE WORKCARD 71-000-00. THE LEAK AND OPERATIONAL CHECKS WERE GOOSDR C2XA11IA041Engine · leakingDFW - FLIGHT 2463 THE CREW REPORTED A STRONG BURNING OIL SMELL FROM THE NUMBER ONE ENGINE BLEED AT HIGH POWER SETTINGS. THE AIRCRAFT LANDED AT DFW WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND IT WAS FERRIED TO IAH WHERE MAINTENANCE REMOVED AND RESDR CWQA03032011Engine · failedNR 1 ENGINE FAILURE ON CLIMBOUT, CREW FELT THE ENGINE POP AND VIBRATE CLIMBING THROUGH 10,000FT WITH OIL PRESSURE LIGHT MASTER CAUTION AND ENGINE ITT SPIKE THROUGH LIMITS AS THE ENGINE SHUTDOWN, CHECK LIST FOLLOWED AND UNSCHEDULED LANDING PERFORMED WITHOUT FURSDR 2011FA0000146Clutch · failedCLUTCH DISC LINING FAILURE, CAUSE UNKNOWN. DAMAGE TO THE CLUTCH PRESSURE PLATE AND ENGINE FLYWHEEL OCCURED. ENGINE AUTOMATICALLY SHUTDOWN DUE TO OVERSPEED SIGNAL AS COMMANDED BY THE FADEC CONTROL. UNSCHEDULED ON AIRPORT LANDING SUCCESSFUL.SDR QXEA2011030700207Engine · surgesDUAL PEC CAUTION MESSAGE ON CLIMB. NR 2 ENG STARTED SURGING ON FINAL APPROACH. NP VARIED 1030-1060. NR 1 AND NR 2 A/C GEN'S DROPPED OFF LINE TURNING OFF RUNWAY. POWER LEVERS WERE NOT MOVED BEHIND FLIGHT IDLE GATE. PEC CAUTION CAUSED BY INADVERTANT CONDITISDR PCSA20110301Engine · flamed outCREW LOG ITEM "ENGINE NR 3 SURGED 3 TIMES (EPR N1 & N2). ON THIRD SURGE ENGINE 3 FLAMED OUT (EPR DROP FOLLOWED BY N1 AND EGT). RESTARTED ENGINE AND INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. ENGINE WINDMILLED FOR 10 MINS." MAINTENANCE INSPECTED THE ENGINESDR CA110315005Engine · shutdown(CAN) IFSD ON 3 SEPARATE OCCASIONS BETWEEN FEB. 28TH AND MAR. 4TH, DURING FINAL APPROACH, AS POWER WAS REDUCED, THE ENGINE SHUT ITSELF DOWN. EACH TIME, AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. TROUBLESHOOTING FOR THESE EVENTS FOCUSED ON THE FUEL SSDR HALA2011022700118Engine · failedNR 1 ENGINE FAILED. SHUT DOWN ENGINE. ENGINE CHANGE IN WORK. OPENSDR MASA2011022502026Engine · shutdownRT ENG AUTO S/D AFTER LIFT OFF. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD WITH ONE ENGINE. ONCE ON THE GROUND ARFF INDICATED THAT THERE WAS NO VISIBLE EXTERNAL DAMAGE, THE ACFT TAXIED BACK TO GATE AND DEPLANED. REPLACED NR 2 ENGINE.SDR CA110228020Engine · overtorqued(CAN) OVERTORQUE/IFSD THE CREW ELECTED TO SHUTDOWN THE ENGINE FOLLOWING AN OVERTORQUE WHILE CLIMBING THROUGH 1000`. AN UNEVENTFUL SINGLE ENGINE LANDING WAS PERFORMED AT THE POINT OF DEPARTURE. TROUBLESHOOTING IS ON-GOING. ENGINE MFG WILL INVESTIGATE TO ESTA
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