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 2006UALA00932Engine · vibrationAT FL320, NR 3 ENG HIGH EGT, HIGH VIBES AND HIGH OIL PRESS PER CREW. EGT REACHED 670C. AFTER SHUTDOWN, ENG WINDMILLING, VIBES FELT IN AIRFRAME AND OIL PRESS INDICATES ZERO. SHOP TEARDOWN SHOWED THE ROOT CAUSE TO BE FAILURE OF A STAGE-2 HIGH PRESSURE TURBINESDR DXTA200601388Engine · failedDURING TAXI, RIGHT ENGINE SHUT DOWN, HAD JUST ADVANCED TLA TO CROSS A RUNWAY AND RIGHT ENGINE FAILED. CHECKED THE RIGHT ENGINE FADECS FOR FAULTS, NO FAULTS INDICATED. RAN THE RIGHT ENGINE NUMEROUS TIMES WITH NORMAL STARTS AND ACCELERATION EACH TIME. INSPECTSDR SWAA061592Engine · making metalDURING SCHEDULED MV2 CHECK, FOUND METAL PARTICLES AT NR 1 ENGINE FWD MAGNETIC CHIP DETECTOR. REMOVED AND REPLACED NR 1 ENGINE PER SAW MT.SDR IXXA060180OEngine · fluctuatesIN FLIGHT NOTICED SLIGHT RUMBLE, NR 3 ENG N1 BEGAN TO FLUCUATE. ENG BEGAN TO ROLL BACK, ENG OIL PRESSURE LIGHT CAME ON. ENG SHUTDOWN, OIL PRESSURE WENT TO NEAR ZERO PSI. INSPECTED ENG INLET & EXHAUST, SPECIFIC GRAVITY, CHECKED MAGNETIC CHIP DETECTORS, FUEL SDR CA060531009Engine · malfunctioned(CAN) DURING TAKE-OFF ROLL THE ENGINE WAS REPORTED TO EMIT A LOUD NOISE ACCOMPANIED BY SEIZURE OF THE POWER SECTION. SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TCSDR AALA20060288Engine · shutdownGRU - AT 8000 FEET LEFT ENGINE HAD AN UNCOMMANDED SHUTDOWN AFTER A STRONG BANG. RETURNED TO GRU AND LANDED WITHOUT INCIDENT. INSPECTED LEFT ENGINE INLET AND EXHAUST AND NO DAMAGE FOUND. DURING INSPECITONS FOUND SEVERAL METALIC DEBRIS ON EXHAUST. REPLACED NSDR DHL2006748003Engine · failedNR 2 ENG FAILED AT APPROX 20000 LOUD BANG SHOOK AIRPLANE. REMOVED AND REPLACED NR 2 ENGINE ASSY IAW B727 MTM 71.2.SDR A6WA200640176Case · crackedLT ENGINE LOW PRESSURE TURBINE CASE IS CRACKED 1.5 INCHES LONG AT 9 O`CLOCK POSTION .75 INCH AFT OF FORWARD FLANGE. CLEANED SUSPECT AREA AND PERFORMED LPI IAW CRJ NDTM 51-20-08. FOUND 1 CRACK LIKE INDICATION APPROXIMATELY 1.5 INCH LONG AT 9 O`CLOCK POSITION.SDR 2006UALA00894Engine · bird ingestionBIRD STRIKE TO NR 1 ENGINE AND ASSOCIATED VIBRATIONS RESULTED IN A RETURN TO FIELD. BIRD STRIKE DAMAGE 3 FAN BLADES. REPLACED FAN BLADES.SDR 06FDEA1728Engine · seizedAFTER T/O AT 1,000' WITH STD POWER, NR 3 ENGINE SEIZED AT QUIET OIL QUANTITY DROPPED TO ZERO. CONDUCTED EPR REDUCTION. QRH ENGINE FIRE/SEVERE DAMAGE CHECKLIST. RETURNED TO FIELD. CRASH CREW REPORTED OIL LEAKING FROM ENGINE. PERFORMED ENGINE SEIZURE INSP PSDR DAT2006F00004Engine · leakingDURING THE FLIGHT, THE FLIGHT CREW SAW A LOW OIL PRESSURE LIGHT. THE FLIGHT CREW CHECKED THE ENGINE GAUGES AND CONFIRMED IT BY THE LOW OIL PRESSURE GAUGE. THE FLIGHT CREW WENT THROUGH THE ENGINE SHUTDOWN CHECKLIST AND SHUTDOWN THE RT ENGINE. THE FLIGHT CREWSDR SIMA200612803Engine · malfunctionedCREW HEARD A LOUD BANG AT START OF TAKEOFF ROLL, ALL ENGINE PARAMETERS WERE FINE GOT EITHER AN E2 OUT OR E2 FAIL. CREW WAS UNSURE RETURNED TO GATE IN JFK. REPLACED ENGINE NR 2. ENGINE NR 2 P/N OFF/ON AE3007A1/3, ENGINE NR 2 S/N OFF CAE311947, S/N ON CAE3117SDR 5092006N209CAEngine · shutdownA/C DEPARTED TUL BOUND FOR OLS, WHILE CLIMBING THROUGH 22,000 FT, A/C WAS STRUCK BY LIGHTNING. THE NR 1 ENGINE ROLLED BACK AND QUIT. THE NR 1 ENGINE WAS RESTARTED AND THE A/C DIVERTED TO OKC. MX INSPECTED A/C AND FOUND LIGHTNING STRIKE ON WING BELOW NR 1 ENSDR CA060510010Engine · making metalON ENGINE STARTUP, THE PILOT NOTICED A FLICKERING ENGINE CHIP LIGHT, SECONDS LATER THE CHIP LIGHT CAME ON SOLID. ENGINE WAS SEEN SMOKING AND OIL COMING FROM EXHAUST STACK. ENGINE WAS SHUTDOWN AFTER APP 1 MINUTE OF OPERATION. ENGINE HAS BEEN SENT TO OVERHAULSDR 2006UALA00885Engine · stalledNR 2 ENG STALLED IN CRUISE. LIGHTING STRIKE IS MOSTLY CAUSE OF STALL WARNING. NO DEFECTS FOUND DURING TROUBLE SHOOTING. REPLACED VSVA AS A PRECAUTIONARY PROCEDURE (NO FAULT FOUND).SDR TRAX200600156Engine · malfunctionedON DESCENT FROM FL290, LT THRUST LEVER LOCKED AND WOULD NOT RETARD WITH N1 90% ENGINE SECURED VIA LT ENGINE FIRE PUSH, AN EMERGENCY WAS DECLARED.SDR DLM88060345Engine · malfunctionedCREW REPORTED THE LEFT ENGINE OIL TEMP STARTED FLUCTUATING. TEMP WENT ABOVE 135 DEG AND THEN BACK TO NORMAL. TEMP THEN ROSE TO 165 AND CREW SHUT DOWN ENGINE PER QRH. NONE NOTED. MILLION AIR MTC AP 2664148, REPLACED LT ENG OIL TEMP BULB RAN ENG PER MM. CKSDR UIEA200600094Engine · damagedNR 4 ENGINE COMPRESSOR STALL 33,000. TAT-7, MACH .84, ENGINE SHUT DOWN. HIGH VIBRATION, EGT RISE. NO EXCEEDANCES. AIR TUR BACK. NR 4 ENGINE CHANGED IAW ATLAS AIR ENGINE CHANGES SHEET REV 15 JAN 02.SDR P5CA0601478Oil Filter · unknownDURING DESCENT NR 3 ENGINE OIL PRESSURE DROPPED TO 30 PSI AND LOW OIL PRESSURE LIGHT CAME ON. EGT WAS 600 DEGREES. WINDMILL OIL PRESSURE WAS 10 PSI FOR 40 MINUTES AFTER SHUTDOWN. CHECKED CHIP DETECTORS, FOUND CLEAN. REPLACED ENGINE MAIN OIL FILTER PER MM 7SDR CA060403019Engine · failedTHE ENGINE WAS REPORTED TO HAVE EXPERIENCED AN INFLIGHT SHUTDOWN. SUBSEQUENT INSPECTION REVEALED METAL DEBRIS ON THE ENGINE CHIP DETECTOR. P&WC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR 06FDEA1661Engine · failedATTEMPTED TAKEOFF ON 18L HAD SLIGHT COMPRESSOR STALL ON POWER APPLICATION. ABORTED TAKEOFF AND CHECKED ENGINE CONDITIONS ELECTED SECOND ATTEMPT DUE TO CROSSWINDS. ON SECOND ATTEMPT HAD ANOTHER COMPRESSOR STALL. 1ST STALL OCCURRED AT 1.5 EPR AND SECOND STALLSDR GUUA04290601Engine · seizedFLIGHT:9285 FLL/EYW DURING TAKEOFF ROLL LT ENGINE SEIZED ABORTED TAKEOFF RETURNED TO GATE. SUSPECT 2ND STAGE PT BLADE FAILURE. LAST PT BLADE INSPECTION: 21.1 HRS BLADES TIME SINCE NEW 8,985 HRS.SDR CA060531008Engine · failed(CAN) THE ENGINE WAS REPORTED TO HAVE LOST POWER IN FLIGHT LEADING TO A FORCED LANDING AND RESULTANT AIRFRAME DAMAGE. MFG WILL INVESTIGATE THE INCIDENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060531008)SDR AMTA200600297Warning Light · illuminatedNR 2 ENGINE CONTROL LIGHT ON AFTER ENGINE START. PERFORMED BITE CK IAW FIM. FOUND TBV DISAGREE. IAW FIM, FAULT NO LONGER ACTIVE. OK FOR SERVICE. (K)SDR CA060531013Engine · surges(CAN) DURING CRUISE THE ENGINE WAS REPORTED TO SURGE AND SUBSEQUENTLY FLAME OUT. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISEOF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060531013)SDR DL76L060326Engine · crackedFAILED BORO_TFR CRACKS NR 1 ENG REPLACED IAW 1T148, ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.SDR 06FDEA1626Engine · damagedPDIS 484 72-00 0008454 27APR06 DFW OPEN LOGPAGES: 00674359 RTO AT 110 KTS,SUSPECTED COMPRESSOR STALL ON NR 3 ENG. NO TEMPERATURE OR ENGINE LIMITS EXCEEDED. ENT BY: 094904 RPT BY: 096724 SHGN 27APR06 15:30 DFW INSPECTED TAILPIPE, FOUND TURBINE WISDR ASMF200604016Engine · failedAIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE THAT DURING LT ENGINE STARTING THE N2 INDICATION REACH THE RED RANGE. THE ENGINE WAS SHUTDOWN AND THE ABORTED ENGINE START CHECKLIST WAS ACCOMPLISHED. THE FIM PROCEDURE 73-22 WAS PERFORMED AND THE CODE 73-10101 SDR ASMF200604018Blades · brokenCAPTAIN REPORTED THAT DURING FINAL APPROACH AT VSA IT WAS A BIRD STRIKE ON THE RIGHT SIDE OF THE AIRCRAFT. THE RT ENGINE WAS INSPECTED, CLEANED AND OPERATIONAL TESTED IAW FIM 71-05 TASK 801, ALL CORRECT. AT ARRIVING TO MEX THE RT ENGINE WAS INSPECTED BY BIRDSDR CA060504004Engine · failedENGINE QUIT ON APPROACH, ONCE LANDED THE PILOT RESTARTED THE ENGINE AND TAXIED TO THE PARKING AREA. THE AIRCRAFT WAS INSPECTED AND IT SEEMS TO BE FUEL PRESSURE THAT WAS THE CAUSE OF THE ENGINE FAILURE. RIGGING AND MULTIPLE TESTS WERE CONDUCTED AND THE PROBLESDR CA060501002Engine · flamed out(CAN) ON TAKEOFF ROTATION THE ENGINE EMITTED A LOUD NOISE AND FLAMED OUT. TAKEOFF WAS ABORTED. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20060501002)SDR CA060501001Engine · failed(CAN) DURING CRUISE THE ENGINE EMITTED A LOUD NOISE ACCOMPANIED BY AN UNCOMMANDED POWER LOSS. THE ENGINE WOULD NOT RESPOND TO THROTTLE INPUT. A SUCCESSFUL DEAD-STICK LANDING WAS ACCOMPLISHED. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCSDR AMTA200600291Warning Light · illuminatedENGINE NR 2 CONTROL LIGHT ILLUMINATED AFTER ENGINE START. REMAINED ON. PERFORMED FIM PROCEDURES IAW FIM. NO DEFECTS NOTED. OK FOR SERVICE. (K)SDR QXEA200601138Engine · malfunctionedPDX - ON FLIGHT 2310, RETURNED TO FIELD, AFTER TAKEOFF FELT AND HEARD A THUMP FOLLOWED BY AN UPTRIM AND AUTO FEATHER NR 1 ENGINE FAILED, NO FIRE. RETURNED AND LANDED IN RDD. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE. OPERATIONAL CHECK GOOD. AIRCRAFT RETSDR UIEA200600088Engine · failedNORMAL TAKEOFF THRUST SET N1 100.1/OAT AND 03.*C WITH AUTOTHROTTLES ON AT 1500. AGL JUST AFTER CLIMB, THRUST SET TO 102.5, NR 4 ENGINE EXPERIENCED A MASSIVE COMPRESSOR STALL AT 2800, MSL. IMMEDIATELY REDUCED THRUST TO NR 4 ENGINE. STALL CEASED AT THAT TIMESDR DL76G060324Guide Vane · damagedNR 2 ENGINE S/N 704871 FAILED BOROSCOPE OF 2ND STAGE NOZZLE GUIDE VANES. ENGINE REMOVED.SDR CA060426003Engine · failed(CAN) DURING CRUISE, THE CREW NOTICED THE TIT SPIKED TO 1100 DEGRESS F. THE HORSEPOWER DECREASED AND THE ZONE 1 FIRE BELL SOUNDED. THE E HANDLE AWAS PULLED AND THE ENGINE WAS SHUT DOWN AND THE PROPELLER FEATHERED. THE AIRCRAFT LANDED. MAINTENANCE CREW INSPECTESDR CA060425018Engine · malfunctionedON TAKEOFF, THE NR 1 ENGINE AUTOFEATHERED AND THE NR 2 ENGINE UP TRIMMED. THE AIRCRAFT DIVERTED TO POINT OF DEPARTURE. MFG WILL INVESTIGATE THE EVENT AND WILL ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR A6WA200640159Engine · power lossREQUEST INSPECTION FOR POSSIBLE LIGHTNING STRIKE. ALTITUDE WAS 5000 FEET GEAR RETRACTED, FLAPS UP. ENGINE NR 2 POWER ROLLED BACK TO 29 PERCENT, N1 FOR TWO MINUTES, ENGINE POWER RECOVERED. NO OTHER INSTRUMENTATION MALFUNCTIONS NOTED. COMPLIED WITH INSPECTIOSDR HAEA200600189Engine · unknownAIRCRAFT DEPARTED MCI, CLIMBING THROUGH FL200 RT OIL PRESSURE LIGHT ILLUMINATED AND RT OIL PRESSURE READ ZERO. RT ENGINE SHUTDOWN, AIRCRAFT DIVERTED TO COU. LANDED WITHOUT EVENT. MAINTENANCE INSPECTED ENGINE AND FOUND BEE NUT LOOSE ON OIL LINE. TIGHTENED OSDR SIMA200611701Engine · odorLAVATORY SMOKE AT 2000 FT ON CLIMBOUT. SMELL IN AIRCRAFT. REPLACED ENGINE 1 AND ENGINE 2, OPERATIONAL CHECK OK. FCF SUCCESSFUL. AIRCRAFT RETURNED TO SERVICE. (K)SDR O3X04229241Engine · flamed outAIRCRAFT WAS IN CRUISE FLIGHT, WHEN THE RT ENGINE SHUTDOWN. EMERGENCY PROCEDURES WERE FOLLOWED. THE CREW ATTEMPTED AN ENGINE RESTART. ENGINE WOULD NOT ACCELERATE BEYOND 30 PERCENT. THE ENGINE WAS SECURED. AIRCRAFT LANDED SAFELY. MAINTENANCE NOTICED A LOUSDR Y2PA200600012Engine · unserviceableAFTER NORMAL TAKEOFF AT APPROX 50 FT IN THE AIR AND PRIOR TO GEAR RETRACTION. A VERY LOUD BANG WAS HEARD WITH AN ACCOMPANYING SHUTTER. CREW CONTINUED TO CLIMB OUT LEAVING GEAR DOWN. AN EMERGENCY WAS DECLARED WITH THE TOWER, SUBSEQUENTLY A NORMAL LANDING WASSDR SB06040Engine · failedPHL - FLT1447 - ON CLIMB-OUT FROM PHL, AT 12,000 FT, THE NR 2 ENGINE LOST THRUST AND WENT TO IDLE. PARTIAL THRUST CAME BACK BUT DECREASED AGAIN ON APPROACH. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT PHL. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND SDR MASA200601143Plug · looseASH 6164 LGB. EMERG LT ENG OIL PRESS MASTER WARNING AND INDICATION. RESECURED BORESCOPE INSPECTION PLUG.SDR CA060425017Engine · malfunctionedON TAKEOFF AND CLIMB, THE ENGINE WAS REPORTED TO EXHIBIT PARTIAL POWER LOSS AND WAS SHUTDOWN IN FLIGHT. POST-FLIGHT INSPECTION REVEALED NO ANOMALIES. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR SIMA200613201Engine · smokeDURING TAKEOFF ROLL, FA REPORTED SMOKE IN CABIN AND THEN CREW NOTICED SMOKE IN FLIGHT DECK. ABORTED TAKEOFF. REPLACED ENGINE NR 1. OPERATIONAL CHECK GOOD AIRCRAFT RETURNED TO SERVICE. (M)SDR DXTA200601350Engine · failedIN CLIMB AT FL 266, EXPERIENCED HEAVY COMPRESSOR STALL IN RIGHT ENGINE. CLIMB OUT WAS 97.3 N1 AT -10DEGREES C TEMP; RIGHT ENG ROLLED BACK TO APPROX 88% N1 FOLLOWED BY STRONG FUMES IN CABIN, O2 MASKS DONNED, CKLIST REVIEWED. LEVELED AT FL 270, 4 BOOMS AS IN: SDR DL764060283Engine · malfunctionedAT APPROX 1500 AFTER T/O WHILE SELECTING CLIMB PWR FROM CLIMB 1, RT ENG SURGED ABOUT 3 TIMES 5 PCNT N1. LT ENG WAS NORMAL. RT ENG OPERATED NORMAL THE REMAINDER OF FLT. REMOVED BORO PLUGS FOR STAGE 1 AND STAGE 12 HPT BORO. C/W BORO PER AMM 72-00-00-206-096.SDR 04202006CEngine · faultyRT ENGINE NOT MAKING T/O POWER. R&R RT ENGINE IAW 71-00-01S. OPS CHECK GOOD.
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