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 SIMA20120930007Engine · defectiveON FLIGHT 4307 THE CREW REPORTED THE COCKPIT SMELLED OF BURNING OIL. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH ETN EM-72-034R4 ENGINE ODOR EVENT TROUBLESHOOTING SUPPLEMENT WHICH VERIFIED ENGINE 1 AS ODOR SOURCE. SUBSEQUENTLY COMPLIED WITH R-R FIMSDR UHLA2012093000313Engine · leakingSTRONG BURNT SMELL ON TAKEOFF ROLL, NO SMELL NOTED WITH APU BLEED ON, SMELL RETURNED ON APPROACH. FERRIED A/C TO IND. REMOVED AND REPLACED E1.SDR ASMF201210009Engine · intermittentACFT REJECTED TAKE AT 70 KNOTS WITH A GROSS WEIGHT OF 268 000 KG DUE TO RIGHT ENGINE STRONG EXPLOSION WITHOUT ADVISE ON ENGINE PARAMETERS OR EXCEEDS IN CREW CABIN WAS LISTENING. MX PERFORMED FIM 71-05 TASK 807 PROCEDURE; A RT ENGINE STALL INSPECTION IAW MM 71SDR REXA2012009281371Engine · malfunctionedON FLIGHT 4021 DURING CLIMBOUT OF CLT AT 4000FT LOUD POP WAS HEARD, NR 1 ENGINE N1 AND N2 ROWED BACK WITH ITT SPIKE TO AROUND 960. THE CREW THEN PROCEEDED TO SHUTDOWN THE ENGINE WITHIN 1.5 MINUTES. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. SDR UALA2012092705459Engine · faultyDUE TO PREVIOUS HISTORY OF RIGHT ENGINE HPSOV MSGS, PERFORM PNEUMATIC HEALTH CHECK OF THE HPSOV-HPC. PER MM 36-00-99-PG 514, STEP C. PAY PARTICULAR ATTENTION FOR SENSE LINE LEAKS. CORRECT ANY DISCREPANCIES FOUND. REMOVED ACCT ECM. REPLACED #2 ENGINE.SDR CA121003008Oil System · high pressure(CAN) AFTER T/O, THE CREW OBSERVED THE NR 2 ENGINE INTO THE RED BAND ACCOMPANIED BY A MASTER CAUTION WARNING. THE ENGINE WAS SHUTDOWN AND THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE AN UNEVENTFUL SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT TROUBLSDR CA121003006Engine · vibration(CAN) DURING TAKEOFF ROLL ENGINE SUFFERED VIBRATIONS.SDR ERAA20120065Engine · malfunctionedOIL PRESSURE ON NR 2 ENGINE OBSERVED BELOW 65 PSI BUT NO WARNING OR CAUTION LIGHTS. REDUCED POWER TO 75NH AND FEATHERED ENGINE NR 2. ITT SPIKED AND ENGINE NR 2 FUEL CUTOFF SELECTED AS TEMP INDICATION WAS RAPIDLY PASSING 850. EVENTS HAPPENED AT 16,000- LEVELSDR ASOA20120925140Engine · smokeLAV SMOKE WARNING ON CLIMB-OUT WITH ELECTRICAL BURNING ODOR. ACFT WAS FERRIED TO FOR NR 2 ENGINE CHANGE.SDR UALA2012092405397Engine · leakingON ENGINE BLEED AIR, BOTH AIR CONDITIONERS OUTPUT VERY NASTY CONDITIONED AIR. BOROSCOPE INSPECTED NR 1 ENGINE 3RD STG BEARING FOUND OIL IN COMPRESSOR UPLOADED PIC TO RVI SITE. REPLACE ESN 726513 PER MM. REPLACED ESN 726513 WITH ESN 726621 IN POS 01 PER TOD SDR RJEF20120925Engine · bird ingestionDURING TAKEOFF OF THE AIRCRAFT FOR FLIGHT TAI-396 FROM MGA TO MIA, THE PILOT IN COMMAND REPORTED BIRD STRIKE ON ENGINE 1 AND SO THE TAKEOFF PROCEDURE WAS ABORTED. ENGINE 1 WAS INSPECTED PER AMM 05-51-19-200-001-A AND FOUND EVIDENCE OF BIRD STRIKE. LOW COMPRESDR CLCA20120920001Engine · power lossON FINAL APPROACH, ENGINE NUMBER 3 POWER INDICATOR ROLL BACK. NO RESPONSE FORM THROTTLE, PERFORMED NON-ALERT ENGINE SHUTDOWN CHECKLIST. NOTE TEMPERATURE 750 DEGREES, AND FELT MINOR BUMP AT ROLL BACK. PERFORMED BORESCOPE INSPECTION, AND TESTING IAW FIM 70-00SDR UALA2012092005328Engine · stalledDURING POWER ASSURANCE TEST AT NR 2 ENG, GOT STALL AT ENGINE DISACCELERATION. TEMPERATURE DID NOT EXCEED 548 EGT. PERFORMED TBS 71-00-00-81 0-809-A. INSPECTED ENGINE INLET & EXHAUST OK. FADEC SYSTEM TEST PER AMM, BURNER PRESSURE SENSOR TUBE & PURGED LINE SDR UALA2012092005324Engine · stalledNR 1 ENGINE STALL RECORDED. STALL WAS RECORDED IN ECM DOWNLINK AND WAS NOT REPORTED BY FLT CREW. REQUIRES TROUBLESHOOTING PER TSM 71-00-00-810-808-A WITHIN 10C. LOOKED IN NR 1 ENGINE FRONT AND BACK, NO DAMAGE NOTED AT THIS TIME, FURTHER TROUBLESHOOTING. UNSDR CA120924005Engine · power loss(CAN) DURING CLIMB, PASSING FL180, THE CREW OBSERVED THE ENGINE TORQUE INDICATING ZERO. THEY IMMEDIATELY REDUCED THROTTLE AND THEN THE CONDITION LEVER, ACTUALLY SHUTTING DOWN THE ENGINE, NO MASTER CAUTION WARNING OCCURRED. THE CREW DECIDED TO RETURN TO THE DEPSDR UALA2012091905310Engine · shutdownNR 1 ENGINE IFSD. EPCS MSGS (S SVA OR FCU- EEC,P SVA OR FCU-EEC) ECS-MSG (L ENG LOW N1, L FUEL ON SOL, L ENG OIL PRESS. L ENG SEC CONT, L ENG PRI CONT) CHECKED CHIP DETECTORS AND ENGINE EXHAUST NO METAL FOUND. CREW COMMENTED FUEL CUTOFF LEVER NEVER MOVED TO SDR CA120924003Engine · overtemp(CAN) AFTER A SCOOPING OPERATION, THE ENGINE SUFFERED AN OVERTEMP TO 962C, 19 SEC. FOLLOWED BY IFSD. THE ACFT LANDED SAFELY AND THE ENGINE WAS REMOVED AND FORWARDED FOR REPAIRS. NO DETAILS ON ENGINE CONDITION ARE AVAILABLE AT THIS TIME.SDR CALA2012092000618Engine · smokeAFTER TAKE OFF, TOWER REPORTED LT ENGINE TRAILING VISIBLE BLACK SMOKE, ALL COCKPIT INDICATIONS NORMAL. F/A REPORTED STRONG BURNING ELECTRICAL ODOR TOWARDS REAR OF CABIN. AIR RETURN, PERFORMED AMM TASK 05-51-58-910-801C1, CHECKED SATISFACTORY. MX TEST FLIGHSDR 3SVAN441BD91912Engine · flamed outRIGHT ENGINE FLAMED OUT ON CLIMBOUT OF ANC. PLIOT SECURED THE ENGINE AND RETURNED TO BASE.SDR CHQA20120917352Engine · failedCREW REPORTED THAT DURING FLIGHT THAT THE ENGINE 2 OIL PRESSURE DROPPED INTO THE AMBER RANGE AND THE ENGINE ITT ROSE INTO THE RED. THE CREW SHUT DOWN THE ENGINE IN FLIGHT, RAN THE CHECKLIST, AND DECLARED AN EMERGENCY. THE PASSENGER O2 MASKS WERE ALSO DEPLOYESDR U5QA20120919044Engine · bird ingestionAFTER DEPARTURE, CREW NOTICED AN ODOR INDICATIVE OF A BIRD STRIKE. ENGINE INDICATIONS WERE NORMAL. DURING CLIMB, ODOR DIMINISHED UNTIL UNDETECTABLE IN CRUISE. DURING DESCENT, ODOR GRADUALLY RETURNED. AFTER LANDING, INVESTIGATED ENGINES AND FOUND REMAINS OFSDR CA120924002Oil System · low pressure(CAN) WHILE TAXIING TO TAKE-OFF POSITION, THE PILOTS OBSERVED HIGH ENGINE TEMPERATURE AND LOW OIL PRESSURE WARNING WITH AN ASSOCIATED UNUSUAL HIGH-PITCHED NOISE. SHUTDOWN THE ENGINE AND RETURNED TO THE RAMP. TROUBLESHOOTING ONGOING.SDR UALA2012091705215Engine · flamed outNR 2 ENGINE FLAMEOUT WITH NO DEFINITIVE CAUSE FOUND. NR 2 ENGINE FMU CHANGE. REPLACE FUEL CONTROL UNIT MR73233 PCN 621-9037. REPLACED EEC PCN 481-9246 MR73237 PER MM (P/N 1B7486 - SERIAL# 67 - POSIT #2). REPLACE ENGINE FUEL PUMP PCN 615-9007 MR73150 PER MMSDR ASOA20120916076Engine · leakingTHE CREW REPORTED SMOKE IN THE COCKPIT AND CABIN IN FLIGHT. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND REPLACED THE NR 1 ENGINE. OPS CHECKED GOOD.SDR SWAA2012091707706Engine · failedINFLIGHT SHUTDOWN/DIVERSION/DECLARED EMERGENCY. CLIMBING THROUGH 22,000 FEET LOUD BANG FROM RIGHT ENGINE WITH ASSOCIATED YAW. NR 2 ENG ROLLED BACK AND INDICATED OVERTEMP. R&R NR 2 ENGINE PER MT.SDR CA120924004Engine · failed(CAN) THE ENGINE EXPERIENCED A FAILURE DURING TAKEOFF. INVESTIGATION FOUND THAT 3 OF THE P/T BLADES ON THE 2ND STAGE DISK WERE BROKEN IN THE FIR TREE AREA AND THE REST BROKEN OFF ABOVE THE PLATFORM AREA. THE DAMAGE WAS CONFINED TO THE POWER SECTION AND IS UNSDR FDEA201209153333Engine · failedPASSING 1500 AGL ON DEPARTURE CLIMB OUT, ENGINE NR 1 COMPRESSOR STALL. N1 RPM FLUCTUATIONS +- 15 PERCENT WITH AUDIBLE POPS AND BANGS. RAN CHECKLIST FOR ENG 1 COMPRESSOR STALL. DUMPED FUEL TO MAX GROSS LAND WEIGHT. SECURED DUMP AND RETURNED TO DEPARTURE. SDR CA120917020Engine · unknown(CAN) ON DEPARTURE THE CREW RECEIVED AN "ENG 1 FADEC ALTERNATOR" ECAM MESSAGE. AFTER 90 MINUTES THE NR 1 ENGINE OIL QTY WAS OBSERVED RAPIDLY DECREASING AND IN CONSULTATION WITH MOC/DISPATCH THE FLIGHT DIVERTED.SDR CA120924001Engine · power loss(CAN) DURING TAKEOFF, THE ENGINE COULD NOT ACHIEVE THE COMPUTED N1 REQUIREMENT OF 94.1 PERCENT. THE ENGINE ONLY REACHED 90 PERCENT, WITHOUT COMPUTER LIGHT OR FAULT INDICATIONS. ALL OTHER PARAMETERS MATCHED THE N1 AT 90 PERCENT. TROUBLESHOOTING IS ON-GOING.SDR SIMA20120914003Engine · malfunctionedON FLIGHT 4304 THE CREW ABORTED TAKEOFF, LOW SPEED (40 KNOTS) DUE TO VISABLE SMOKE AND OIL SMELL IN COCKPIT. SMOKE ALSO VISABLE IN CABIN AS REPORTED BY FLIGHT ATTENDANT. THE AIRCRAFT WAS REMOVED FROM SERVICE. THE AIRCRAFT WAS INSPECTED TO THE EXTENT NECESSASDR CA120917016Engine · power loss(CAN) SECURED NR 1 ENGINE DURING CLIMBOUT. DURING CLIMBOUT, FLIGHT CREW HEARD A, POP/BANG. SCANNED ENGINE INSTRUMENTS AND NOTICED LOSS OF HORSEPOWER AND DECAYING RPM ON NR 1 ENGINE. E-HANDLED NR 1 ENGINE TO SHUTDOWN AND FEATHER PROPELLER. ABORTED THE LOAD SDR SIMA20120913001Engine · overtempON FLIGHT 2829 THE CREW REPORTED THAT ON CLIMBOUT HAD A NR 2 ENGINE OVERTEMP INDICATION. THE CREW REDUCED THRUST AND LEVELED OFF AT 10,000 FEET. THE CREW CONTACTED ATC, DECLARED AN EMERGENCY AND COMPLETED THE AOM VOL 1 CHECKLIST. THE AIRCRAFT LANDED WITHOUTSDR KKYA20120919001Engine · overtemp"ENGINE" EICAS ON TAKEOFF ROLL. LEFT ENGINE OVERTEMP.SDR SWAA2012091407624Engine · failedDIVERT/DECLARED EMERGENCY/ENGINE SHUT DOWN. ON CLIMBOUT NR 2 ENGINE LOUD BAND AND SHUTDOWN. REMOVED AND REPLACED NR 2 ENGINE PER MT.SDR CA120918006Engine · power loss(CAN) DURING FINAL APPROACH, THE OPERATOR REPORTED A SHIFTING AND DECREASE OF TORQUE ON THE RT ENGINE. THE POWER LEVER WAS PUSHED FORWARD TO COMPENSATE THE TORQUE DECREASE BUT WHEN PASSING THE FINAL APPROACH POINT THE CREW NOTICED THAT THE TORQUE WAS AT 0. NSDR UALA2012091205140Bolt · shearedNR 1 ENGINE BORO PORT "F" HAS ONE SHEARED BOLT AND ONE BOLT WITH GALLED THREADS. BOLT WAS REMOVED AND INSERT REPLACED ON 2 EA ATTACH HOLES.SDR SIMA20120910002Engine · malfunctionedFOR FLIGHT 3259 - THE RAMP PERSONNEL REPORTED ON TAXI IN SMOKE WAS COMING FROM NR 1 ENGINE. SMOKE SMELLED SOMETHING LIKE BURNING ELECTRIC WIRING. THE AIRCRAFT WAS REMOVED FROM SERVICE. PERFORMED OPERATIONAL CHECK OF LEFT ENGINE IAW AE3007A MM 72-00-00. SMOSDR SWIA201231767Engine · faultyWITH LOW POWER SETTINGS AND BLEED PACKS IN AUTO/LOW, CABIN FILLS WITH SMOKE. (FLT 7802) REPLACED RIGHT ENGINE ASSEMBLY. P/N OFF: PW11813, S/N OFF: AP0019.SDR AALA20120910001Engine · failedLBB - INFLIGHT DFW-SAN. CREW REPORTED RIGHT ENGINE OIL QUANTITY LOSS AND VIBRATIONS. RIGHT ENGINE WAS SHUTDOWN (SINGLE ENGINE TIME 15 MINUTES). EMERGENCY DECLARED FLIGHT DIVERETD LBB LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT SDR UALA2012091005067Engine · faultyTOP OF DESCENT FLIGHT DECK HAD A FAINT SMOKY SMELL FOR 3-4 MINS. DUE TO HISTORY OF OIL SMELL, REVIEW TROUBLESHOOTING ACP'D (CHP 21, 36, 49, 71, 72, 79), IF OIL SMELL IS REPORTED AGAIN, TO PREVENT IRREG OPS, REPLACE LEFT ENGINE PER AMM71-00-02 (401). LABEL RESDR N6WA2012090801Unknown · vibrationRT ENGINE FAN VIBRATION IN YELLOW 5.0, OBSERVED DURING FLIGHT. INSPECTED FAN BLADES, NO DEFECTS FOUND IAW AMM 72-21-02. PERFORMED FAN TRIM BALANCE , OP'S CHECKED GOOD IAW AMM 71-00-00.SDR O2GA2012F00184Engine · bird ingestionBIRD INGESTION ON NR 2 ENGINE ON INITIAL CLIMB. EMERGENCY PROCEDURES FOLLOWED, NR 2 ENGINE SHUTDOWN AND RETURNED TO DEPARTURE.SDR CA120918007Engine · malfunctioned(CAN) THE OPERATOR REPORTED THAT SINCE 26 JULY, THIS ENGINE WOULD HANG OCCASIONALLY AT CRUISE WHEN THE POWER LEVER WAS RETARDED TO IDLE TO INITIATE DESCENT. THE PILOT WOULD EITHER WAIT FOR ENGINE TO DECELERATE OR HE WOULD MODULATE THE POWER LEVER UNTIL HE GOT SDR YENA20120907596Engine · leakingFLT 686 DCA-BOS, AIRCRAFT DIVERTED TO JFK DUE TO NR 1 ENGINE INDICATION OF RAPID OIL LOSS FROM 11.4 TO 7.2. FOUND OIL LEAKING ON NR 5 SUMP DRAIN. REMOVED AND REPLACED NR 1 ENGINE PER TASK CARD E190-71-00-01-400-801. OPS AND LEAK CHECK GOOD. ON THE SAME FLISDR ANCF2012090700129Engine · bird ingestionAFTER T/O IN CLO PASSING 6000FT, BIRD STRIKES RIGHT ENGINE IMMEDIATE RETURN, ENG VIBRATION WENT UP TO 9.2 N1, MODERATE VIBRATION OTHER PARAMETERS WERE NORMAL. IN ACCORDANCE WITH AMM 05-51-19 PB 601 TASK 72-00-00-200-006-A ITEM 4-A(8) AND B (2)(A)(B) BOROSCOPSDR V2JA2012091000001Engine · failedENGINE OIL LEAK. FIXED LEAK, RAN ENGINE, NO OIL LEAK WAS FOUND. DURING DEPARTURE, HEARD A NOISE IN AFT SECTION OF PLANE AND NOTICED A VIBRATION. SHORTLY AFTER, A SLOW DECREASE IN OIL PRESSURE ON ENGINE NR 1. BETWEEN 60 AND 70PSI, RAN ENGINE SECURING PROCSDR ASOA201209008138TEngine · smokeSMOKE WAS SEEN IN THE CABIN DURING ENGINE RUNS AND WAS ISOLATED TO THE NR 1 ENGINE. MX REMOVED AND REPLACED ENGINE IAW TASKCARD 6271001. ALL WORK WAS ACCOMPLISHED AND THEN RELEASED UPON COMPLETION OF OPS CHECKS AND LEAK CHECKS.SDR IXXA20120907023OEngine · stalledDURING TAKEOFF ROLL, CREW EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. TAKEOFF WAS REJECTED AT 85 KIAS AND 1.96 EPR. RETURNED BACK TO GATE. MX PERSONNEL PERFORMED A VISUAL INSPECTION OF NR 3 ENGINE, NO DEFECTS OBSERVED. ACCOMPLISHED ENGINE RUN UP TO SDR CA120917009Engine · malfunctioned(CAN) OCCASIONAL ROLLBACKS OCCURRED ON THE LT ENGINE AROUND 5-7 PERCENT DURING T/O PHASE, AS WELL AS AT ALTITUDE. POST FLIGHT TROUBLESHOOTING SHOWED FAULT CODES RELATED TO ENGINE INLET TOTAL TEMPERATURE PROBE SIGNAL COMING FROM THE ENGINE INPUT RESULTING IN TSDR CA120905002Case · corroded(CAN) ENGINE RETURNED TO MFG FOR MIDLIFE INSPECTION. DURING ENGINE DISASSEMBLY AT OGV RING REMOVAL IT WAS NOTED THAT EXTERNAL INTERMEDIATE CASING WALL HAD EXCESSIVE CORROSION THAT HAS HOLED THE CASING WALL AND GENERATED A 10" CRACK. ENGINE HAS ALSO EXCESSIVE
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