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 SWAA2016051851899Engine · leakingCREW REPORTED STRONG ENG OIL SMELL IN CABIN WHILE IN DESCENT. R & R NR 2 ENG IAW MT.SDR AALA201605169006Engine · slowABORTED TAKEOFF. ACFT WAS GNDED. NR 2 ENG SLOW TO SPOOL ON TAKEOFF ROLL, FLIGHT CREW ABORTED TAKEOFF, BETWEEN 25 & 30 KNOTS & RETURNED TO THE GATE. ACCOMPLISHED TSM TASK 73-00-00-810-881-A, NR 2 ENG ACCELERATION TESTED NORMAL, FADEC TESTED NORMAL, NO FAULTSSDR ZP7A201605090001Engine · failedLEFT ENGINE FAILURE IN FLIGHT. FLUCTUATION IN ITT TEMP BEFORE FAILURE RISE AND FALL. ATTEMPTED TO RESTART. NO LIGHT OFF.SDR AALA201605109001Engine · faultyAIRCRAFT WAS GNDED. DURING CRUISE NR 1 ENG EXPERIENCED COMPRESSOR STALL ACCOMPANIED BY HIGH EXHAUST GAS TEMPERATURES. ENG WAS SHUT DOWN. FLIGHT DIVERTED, EMER WAS DECLARED. R & R NR 1 EN IAW JOB CARD 26L40071001.SDR AALA20160509014Engine · leakingAIRCRAFT WAS GNDED. FLIGHT CREW REPORTED AN OILY SMELL IN COCKPIT MOST OF FLIGHT THAT SEEMED WORSE ON THE GND. ISOLATED ODOR SOURCE TO BE NR 1 ENG. R & R NR 1 ENG.SDR ASMF20160620010Engine · damagedIAW REMOTE DIAGNOSTIC SYSTEM, THE LT ENGINE HAD A SHARP DECREASE OF EGT HOT DAY MARGIN, AS WELL AS AN INCREASE OF EGT AND FUEL CONSUMPTION. MAINTENANCE PERSONNEL PERFORMED THE LT ENGINE BORESCOPE INSPECTION OF THE HIGH PRESSURE TURBINE AND COMBUSTION SECTION SDR E3MA20160506001Engine · making metalDURING FLIGHT THE OVER SPEED CAUTION ILLUMINATED FOLLOWED BY CHIP A CHIP CAUTION FOR THE NR 2 ENG. THE PILOT TRIED TO BURN THE CHIP & WAS UNSUCCESSFUL. THE PILOT LANDED SAFELY AT THE NEAREST AIRPORT & DURING SHUTDOWN OF THE ENG THERE WAS A LOUD BANG. DISCOVSDR QXEA2016050300288Engine · surgesDURING CLIMB OUT, WITH THE POWER LEVERS AT RATED DETENT AND MCL ON, THE ENGINES SURGED SLIGHTLY. IT IS UNCERTAIN WHICH ENGINE SURGED BUT IT WAS ENOUGH TO MAKE THE AIRPLANE YAW SLIGHTLY. DIVERTED, LANDING UNEVENTFUL. INTEROGATED CDS FOR ENGINE FAULTS AND FOUSDR 29GA2016050400004Engine · failedDURING CLIMBOUT AT APPROXIMATELY 1000 FT, INITIATED THE CLIMB CHECKLIST FLOW, THE NR 2 ENGINE FAILED IN FLIGHT. A CONTINUOUS LOUD THUNK WAS HEARD COMING FROM NR 2 ENGINE. COMPLETED BORESCOPE OF RT ENGINE COLD SECTION IAW MM 72-00-00. AFTER DFDR DOWNLOAD COSDR CALA2016050200283Engine · malfunctionedAT FL380 LT ENG LOST 50% POWER & SLIGHT VIBRATION OCCURRED, REDUCED TO IDLE. NO FURTHER VIBRATION OR ABNORMAL INDICATIONS, DECIDED TO OPERATE AT IDLE DECLARED EMER & DIVERTED. SUSPECT NR 4 BEARING FAILURE ON NR 1 ENG. R & R NR 1 ENG IAW WC 29-7100-1-0900, &SDR SWAA2016050251481Engine · shutdownINFLIGHT SHUTDOWN, DIVERSION & DECLARED EMER. SHORTLY AFTER TAKEOFF NR 1 ENG SHUTDOWN. R & R NR 1 ENG IAW MT.SDR WX0A2016042973145Engine · failedNUMBER 2 ENG FAILED DURING GO AROUND. DISCHARGED NR 1 FIRE BOTTLE. R&R NR 2 ENGINE PER T/C 71-400-001. ALL OPS AND LEAK CHECKS GOOD.SDR SWAA2016042951439Engine · malfunctionedINFLIGHT SHUTDOWN & DECLARED EMER. NR 1 ENG OIL FILTER BYPASS, ENG SHUTDOWN IAW QRH. R & R NR 1 ENG IAW MT.SDR YENA20160425353Engine · making metalDIVERTED, CREW REPORTED ENGINE NR 1 WAS EXPERIENCING HIGH VIBRATIONS AFTER TAKEOFF. CREW ALSO REPORTED EGT WAS 60 DEGREES HOTTER AND FUEL FLOW WAS 400 LBS INCREASED COMPARED TO ENGINE NR 2. INITIAL INSPECTION AND ENGINE WALK AROUND WAS PERFORMED. FOUND METALSDR REXA2016041900608Engine · contaminatedON TAKEOFF SMELL BEGAN AT 400' SMOKE AFT LAVATORY ILLUMINATED. FLIGHT ATTENDANT REPORTED NO SMOKE NOR HEAT, JUST SMELL. AT AROUND 100' SMOKE AFT LAVATORY EXTINGUISHED. SMELL BEGAN TO DISSIPATE, CONTINUED FLIGHT. ON DESCENT AT AROUND 12000' STRONG SMELL BEGSDR DALA2016041803161Turbine Case · crackedLEFT ENGINE AFT VIBRATOR ISOLATOR THERMAL OVERHEATING FROM CRACK IN TURBINE CASE. R & R AFT VIBRATIONS ISOLATOR IAW MM.SDR AALA20160417001Engine · out of trimAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL NR 2 ENG WOULD NOT MAKE TAKEOFF POWER. TAKEOFF ABORTED AT APPROX 40 KNOTS. ACCOMPLISHED MCM 71-91-08 & FOUND NR 2 ENG IDLE LOW. ACCOMPLISHED ENG TRIM IAW MCM 71-91-73. ENG ACCELERATION & POWER WITHIN LIMITS.SDR AALA201604159007Engine · stalledAIRCRAFT WAS GNDED. NR 1 ENG STALLED AT FL 350. NOISE & VIBRATION FELT & POWER REDUCED ON ITS OWN TO APPROX 50%. POWER WAS REDUCED TO IDLE & ENG IDLED NORMALLY. ENG SURGED & STALLED TWICE BEFORE POWER WAS BROUGHT TO IDLE. FLIGHT CREW DECLARED AN EMER, LANSDR 29GA2016041300001Engine · shutdownENGINE SHUTDOWN IN FLIGHT. AFTER TAKEOFF, LT ENGINE MAKES A LOUD BANG FOLLOW BY MULTIPLE BANG. ENGINE FAILS AND RE-START AGAIN. WITH NO TORQUE ITT WENT RED LIGHT AFTER ENGINE RE-START ITSELF CAP HAD NO CONTROL OF TORQUE. R & R NR 1 ENGINE IAW TC 71-00-01. SDR T17A201604154013Engine · power lossPILOT REPORTED RT ENG EXPERIENCED SLOW ROLLBACK ON BASE & FINAL APPROACH. THE APPROACH & LANDING WERE UNEVENTFUL. AFTER LANDING THE ENG WAS SECURED. PERFORMED NORMAL PERFORMANCE CHECK IAW AMM 71-00-00. UPON COMPLETING SEVERAL PERFORMANCE CHECKS NO ISSUES FSDR AALA20160411017Engine · failedAIRCRAFT WAS GNDED. DURING TAKEOFF ROLL A PAX REPORTED SEEING FLAMES COMING FROM THE NR 1 ENG TAIL PIPE. NO INDICATION RECEIVED IN COCKPIT. ABORTED TAKEOFF AT APPROX 80 KNOTS. FOUND OIL PUDDLING IN EXHAUST FLAME ARRESTOR AREA. R & R 1 ENG IAW MCM 71-94-01SDR AALA201604099004Engine · slowAIRCRAFT WAS GNDED. 2 ENG SLOW TO SPOOL TO FLEX POWER TAKEOFF ABORTED. FOUND NO FAULTS ON THE ECAM, ACCOMPLISHED ACCELERATION & DECELERATION TEST IAW AMM 71-00-00-700-011-B13 & BOTH ENGS WERE WITHIN LIMITS. ACFT WAS RETURNED TO SERVICE.SDR DALA2016040802706Engine · malfunctionedTHE CREW PERFORMED AN AIR TURN BACK DUE TO WINDSHEAR AND SUBSEQUENT DUAL ENGINE OVERSPEED. THE CAPTAIN FIREWALLED BOTH ENGINES AND BOTH WENT TO 2.2 EPR FOLLOWED BY COMPRESSOR STALLS AND AN ODOR IN THE CABIN. DURING INITIAL CLIMB-OUT CAPTAIN NOTICED AIRSPEED DESDR DALA2016060704397Engine · fireTHE CREW SAFELY ABORTED THE TAKEOFF AT LESS THAN 80 KTS DUE TO A FIRE INDICATION ON THE NR 1 ENGINE. THE FIRE WAS CONFIRMED, BUT THE CAUSE HAS NOT BEEN IDENTIFIED. MAINTENANCE HAS REPLACED THE NR 1 ENGINE.SDR C77A20160404025Engine · bird ingestionENGINE BIRD INGESTION ON CLIMB OUT. CREW NOTED ABNORMAL ENG INDICATIONS & VIBRATIONS. CREW DECLARED EMER & RETURNED. ENG WAS NOT SHUTDOWN. LANDED & TAXIED TO GATE NORMAL. NO PAX NOR CREW INJURIES. COMPLIED WITH A BIRD STRIKE INSPECTION IAW AMM 05-50-02 WSDR AALA20160402003Engine · power lossAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER NOT DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CRUISE, LT ENG THROTTLE 2 FULL KNOBS AHEAD OF RT ENG TO GET BALANCED POWER. THROTTLE SPLIT INCREASES WITH INCREASE IN ALTITUDE. R & R LT ENG.SDR CTYA2016040100000Engine · power lossPILOT REPORTED ENGINE RUNNING HOTTER THAN NORMAL, LACK OF POWER.SDR CALA2016033195236Engine · vibrationHEAVY VIBRATION 5 HRS INTO FLIGHT. SPARKS OBSERVED BY DEADHEADING PILOTS FROM TAIL CONE. ALL ENG PARAMETERS DISPLAY NORMAL ON EICAS, HOWEVER, WHEN POWER REDUCED TO 65% N1 VIBRATION CEASED. REPLACED NR 1 ENG IAW AMM 71-00-02 PG 401.SDR Q5Q2016F00001Blade · failedTHE REFERENCED ENGINE WAS REMOVED AND SENT TO MFG FOR O/H. MFG DETERMINED THAT A NUMBER OF HIGH PRESSURE TURBINE BLADES, PN 35C5521-01 WERE DEFECTIVE DUE TO CRACKS AT THE FILLET RADIUS. MFG MADE THE AIRWORTHINESS DETERMINATIONS BY HAVING THEIR O/H LINE PERSOSDR SWAA2016040450536Engine · stalledDIVERSION & INFLIGHT SHUTDOWN. DECLARED EMER INFLIGHT, AT FL 330 CRUISE NOTICED AN AIRFRAME VIBRATION WITH NO INCREASE IN ENG VIBRATION GAUGES. SMALL COMPRESSOR STALL POP & LT ENG ROLLED BACK TO 50% N2 HAD MOMENTARY SMELL OF SMOKE VIBRATION, CONTINUED WITH LSDR IPXA2016033101455Line · leakingENGINE FAIL LIGHT ON T/O ROLL. REJECT ACCOMPLISHED DUE TO ENGINE MONITORING DATA SHOWING LOW PB PRESSURE NR 2 ENGINE, PERFORMED ENGINE CHECK 3, PB SENSE LINES. FOUND NR 2 ENGINE PB FLEX, PN 51U78 HAS SEVERE AIR LEAK. REPLACED LINE, PERFORMED ACCEL/DECEL TESTSDR AALA201603299010Engine · leakingAIRCRAFT WAS GNDED. DURING DESCENT THE FLIGHT CREW REPORTED A DIRTY SOCK SMELL IN THE CABIN, RESULTING IN THE CREW RECEIVING MEDICAL EVALUATION. FOUND EVIDENCE OF OIL WETTING IN THE HPC SECTION OF THE NR 1 ENG. REPLACED IT IAW TASK CARD 26L40071001. A SATISDR ASAA2016032716107Warning Light · false activationNR 2 ENGINE CONTROL LIGHT ILLUMINATED ON GROUND. ACFT GROUNDED. REF FIM 73-06, TASK 801, PERFORMED ELECTRONIC ENGINE CONTROL BITE TEST ON NR 2 ENGINE ELECTRONIC ENGINE CONTROL, BITE TEST PASSED. ENGINE CONTROL NORMAL. ACFT OK FOR SERVICE. ENGINEERING REQUESDR AALA201603289008Engine · odorRETURNED, ACFT WAS GNDED. RT AFTER ROTATION, THE CREW NOTED A STRONG SMELL OF BURNING OIL & HAD SMOKE IN THE COCKPIT. THE CREW OXYGEN MASKS WERE USED IN THE COCKPIT ONLY SINCE THERE WAS NO SMOKE & ONLY AN ODOR IN THE CABIN. DECLARED AN EMER & THE ACT RETURNSDR K2DA2016032520151Engine · making metalDURING NORMAL CRUISE FLIGHT, THE PILOT REPORTED THE ENG CHIP LIGHT ILLUMINATED. THE PILOT PERFORMED A POWERED PRECAUTIONARY LANDING ON A PRIVATE, CLEARED LOT WITHOUT INCIDENT. AFTER INVESTIGATION OF THE CHIP PLUGS, BY A CERTIFICATED MECHANIC, IT WAS DISCOVERSDR F3LA2016032600014Engine · leakingAFTER TAKEOFF THE FLIGHT CREW RECEIVED A CARGO & LAVATORY SMOKE MSG. THE ACFT RETURNED TO THE FIELD & MX DISCOVERED OIL WETTING IN THE NR 2 ENG COMPRESSOR. MX REMOVED ENG SN 575632 & INSTALLED SERVICEABLE ENG 575640 IAW MPD TASK CARDS MP 71042-01, MP 71042-0SDR C77A20160325012Engine · failedENGINE FAIL CASS MSG. ENG AUTOMATICALLY SHUT DOWN IN FLIGHT.SDR GTIA2016032301509Drain Line · chafedTHE CONNECTOR THAT ATTACH THE FIRE BOTTLE AND FIRE BOTTLE DISTRIBUTION PIPE BECAME LOOSE, CONNECTOR NOT SAFETIED AND BACKED OFF FROM THE FIRE BOTTLE BACK AS FAR AS POSSIBLE, CONTACTING A DRAIN LINE AND CHAFED A HOLE IN THE DRAIN LINE.SDR WX0A2016032873110Engine · overspeedON APPROACH AT 6000 MSL, AUTO-THROTTLE COMMANDED FULL POWER & DISCONNECTED, RESULTING IN BOTH ENGS OVER SPEED. AIRSPEED WAS 170 KTAS EPR 2.10-2.12 N1 APROX 105% & FLASHING LESS THAN ONE SECOND.SDR 2016FA0000288Clamp · missingTHIS TCF MODULE, HAS BEEN REMOVED FROM ENGINE INCOMING VISUAL INSPECTION, 72-54-00, OBSERVED 24 TRIPOD CLAMPS AND NUTS WERE MISSING ON THE 1ST FORWARD ROW, ON OUTER SIDE. DUE TO THE TCF WORKSCOPE APPLIED DURING THE QUICK TURN SHOP VISIT, THIS TCF AREA WAS NOTSDR E3MA20160318001Engine · making metalNUMBER 2 ENG DHIP LIGHT THAT WOULD NOT CLEAR AFTER ON FUZZ BURN APPLICATION. UPON INSPECTION, THE REAR BEARING CHIP PLUG WAS FOUND TO HAVE SIGNIFICANT BUILDUP OF METALLIC MATERIAL, N1=3478 N2=9543.SDR CA160318005Engine · malfunctioned(CAN) ENGINE OUT THROUGH 10000Ï¿½. FLIGHT CREW REPORT A LOUD BANG FOLLOWED BY A LARGE YAW, THEY ALSO NOTICED THAT THE ENGINE DISPLAY HAVE ERRATIC MOVEMENTS OF THE NH, TORQUE AND ITT ON ENGINE NR 1, IN ADDITION TO THIS, THEY MENTIONED THAT THE ENGINE INDICATIONSDR 2016FA0000137Cover · missingFOUND A REAR BEARING HEAT SHIELD AND COVER ON THE FLIGHT LINE. ALL THE ACFT THAT WERE IN FLIGHT WERE CALLED BACK FOR INSPECTION. INSPECTION REVEALED T94 WAS MISSING THE REAR OIL BEARING HEAT SHIELD AND COVER. THE THREAD INSERTS ON THE ENGINE APPEAR TO BE STSDR A6WA201643701Engine · malfunctionedDESCENDING THROUGH 5,000 FT, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN, MOVING FROM BACK TO FRONT. AT THE TIME THE APU WAS OFF. SMK CASS MSG WAS NOT DISPLAYED. SMOKE SMELLED ELEC. R & R RT ENG.SDR CA160316001Stator · damaged(CAN) ENGINE WAS RECEIVED FOR INVESTIGATION AND REPAIR AFTER THE OPERATOR REPORTED A DENT ON THE T/E OF AN LP BLADE AIRFOIL. DUE TO THE TIME ACCUMULATED BY THE HOT SECTION SINCE O/H, THE OPERATOR ELECTED TO PERFORM AN HSI AT THIS VISIT. THE OPERATOR ALSO ELESDR AALA201603159016Engine · odorAIRCRAFT WAS GNDED. INBD FLIGHT ATTENDANT REPORTED NOXIOUS CHEMICAL ODOR THROUGHOUT CABIN ON LANDING. REPLACED NR 2 ENG IAW JC 26L40071001.SDR UHLA201603110113Engine · failedPASSING THROUGH 11,000 FT, HEARD A LOUD BANG AND HAD AN ENGINE FAILURE OF THE NR 1 ENGINE. DECLARED EMERGENCY, LANDED WITHOUT INCIDENT. R & R THE NR 1 ENGINE IAW CR72-10-400-0001.SDR U5QA201603110076Engine · shutdownUPON ARRIVAL, DECLARED EMER, LANDED UNEVENTFUL. RT ENG SHUTDOWN INFLIGHT UNCOMMANDED. IN MX NOW ALONGSIDE OEM TECHNICAL ASSISTANCE. SUSPECT FADEC, PART ON ORDER.SDR 2016FA0000154Governor · inoperativeEPOXY CAME LOOSE FROM END OF DRIVE SHAFT. CLIP CAME LOOSE ALLOWING DRIVE SHAFT SPLINES TO WEAR AND CAUSE UNSTABLE GOVERNOR CONTROL.SDR AALA20160309004Engine · failedRIGHT ENG LOST OIL PRESS & QUANTITY DURING DESCENT. ENG SHUTDOWN. AN EMER WAS DECLARED. ENG WIND MILLED ABOUT 5 MINUTES. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. TOTAL SINGLE ENG TIME WAS ABOUT 10 MINUTES. R & R RT ENG IAW MCM 71-91-99. THE ACFT WAS
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