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 SWAA2018021219546Valve · openTHE NR 2 ENGINE FAILED AT FL 370 WHILE IN DESCENT TO FL 350. R & R THE VALVE IAW MM.SDR UIEA2018020500179Bolt · missingFOUND A BOLT AND BUSHING MISSING ON THE NR 2 ENGINE 11TH STAGE COOLING AIR TUBES AT THE 4 O'CLOCK POSITION. INSTALLED THE BOLT IAW AMM 75-24-03.SDR DALA2018020100602Engine · vibrationNR 2 ENGINE VIBRATION DURING CLIMB OUT, N1 1.5 AS POWER INCREASED, VIBRATION INCREASED. R & R TCC AIR VALVE IAW AMM 75-24. R & R THE ENGINE OIL FILTER AND CHECKED CHIP DETECTORS, NO METAL. PERFORMED LPC BOROSCOPE 6 THRU 17 STAGE. HPT 1-3 STAGE; LPT 3RD STSDR AALA201802059024Engine · odorUNDETECTABLE ODOR NOTICED IN COCKPIT DURING FLIGHT. CABIN OK. FLEW OVER 1 HOUR AT 16,000 FT. AIRCRAFT WAS GROUNDED. REPLACED ENGINE ASSENBLY.SDR CALA2018020200397Engine · malfunctionedON ARRIVAL, RAMP REPORTED SEEING FLAMES AND SMOKE FROM THE LEFT ENGINE ON SHUTDOWN . THE ENGINE FUEL VALVE LT STATUS MESSAGE, FIM PROCEDURE CARRIED OUT IAW 73-22-00-810-801-N00, THE LEFT ENGINE WIRING CHECKED IAW WDM 76-21-71, CHECKED NORMAL. RELAY K76104, RSDR SWAA2018020619541Engine · stalledAIR TURNBACK/DECLARED EMERGENCY, 250 KTS/13000 FEET NR 1 ENGINE STALLED. N1 RPM DROPPED MOST ENGINE INDICATIONS WERE EVEN WITH THE OTHER ENGINE. AFTER REDUCING POWER TRIED TO PUSH ENGINE BACK UP. STRAIGHT BACK IN STALLING AGAIN. R&R NR 1 ENGINE PER MT.SDR QMLA2018012918011Engine · making metalEN ROUTE TO BASE, THE ENGINE CHIP LIGHT ILLUMINATED. LANDED. MAINTENANCE PULLED THE MAGNETIC PLUGS FROM ENGINE AND DISCOVERED NUMEROUS SIGNIFICANT FERROUS SLIVERS AND DEBRIS ON BOTH.SDR GTIA2018012902372Seal · leakingDURING ARRIVAL, APU WAS NOT ON TURNED OFF, NR 2 BLEED AND NR 2 PACK CLOSED THE CROSS BLEED AND ODOR SUBSIDED. DURING TSM 71-00-00, FOUND THE NR 2 ENGINE DEOILER SEAL LEAKING OIL. R & R THE DEOILER SEAL IAW AMM 72-60-31 NO LEAKS NOTED.SDR ASOA201801297004Engine · odorACFT WAS OUTBOUND, CREW SMELLED ODORS OF SMOKE AND RETURN TO BASE. MAINTENANCE R & R THE ENGINE IAW AMM 72-00-00, AND CHECKLIST OF 71-00-00. ALL LEAK AND OPS CHECKS PERFORMED.SDR DCGA201801230044Engine · making metalDURING CRUISE FLIGHT AND ENGINE CHIP LIGHT INDICATION OCCURRED. THE PILOT PERFORMED A PRECAUTIONARY LANDING. MAINTENANCE DISCOVERED METAL FLAKES ON UPPER AND LOWER ENGINE CHIP PLUG. PER MAINTENANCE MANUAL INSTRUCTION IT WAS DETERMINED THAT THE ENGINE ASSEMBLY SDR M3XA2018012202Engine · making metalPL FOR ENGINE CHIP LIGHT AND LANDED WITHOUT INCIDENT. ON INSPECTION, IT WAS DETERMINED THAT CHIPS WERE MORE THAN ALLOWED IN MFR MANUAL FOR RETURN TO SERVICE.SDR DXTA2018012100499Transducer · inoperativeDURING CRUISE, THE RIGHT ENGINE N1 ROLLED BACK APPROX 5 TO 7 PERCENT. SIGNIFICANT YAWING WAS NOTICED AS THE ENGINE ROLLED BACK AND THEN RESUMED NORMAL POWER. FELT LIKE WHEN ONE ENGINE COMPUTER GOES OFFLINE AND THEN RESUMES. DEEC DOWNLOADS REVEALED FAULT CODESDR P5CA2018012200009Acoustic Liner · damagedNR 1 ENGINE, BETWEEN THE 9 & 12 O'CLOCK ACOUSTICAL PANEL HAS A 3 INCH DIAMETER HOLE. REMOVED AND REPLACED THE ACOUSTICAL LINER SEGMENT IAW AMM 72-33-01.SDR I5EA2018012200001Engine · flamed outDURING DESCENT, THE NR 1 ENGINE FLAMED OUT, RAN CHECKLIST AND ACCOMPLISHED STARTER ASSIST RESTART, LANDED AT NEAREST AIRPORT. TROUBLESHOT THE SYSTEM IAW AMM 71-00-42, FIG 9, VERIFIED NO WATER IN FUEL, PERFORMED FUEL FILTER , AND START LEVER CHECKS , INSPECTSDR RAIA201801170001Engine · malfunctionedNR 1 ENGINE EXECEEDENCE DURING FLIGHT, PRECAUTIONARY SHUTDOWN PEFORMED. R & R THE NR 1 ENGINE. OPS AND LEAK CHECKED GOOD.SDR CALA2018011200113Engine · odorAT IDLE DESCENT WITH HIGH PRESSURE VALVES OPEN, A NOXIOUS OILY ODOR. REPLACE THE NR 1 ENGINE IAW MM 71-00-02.SDR UIEA2018011100055Ecu · failedAFTER ENGINE START , IDLE DISAGREE EICAS MESSAGE. REMOVED AND REPLACED ECU. OPS CHECKED NORMAL IAW AMM 73-21-15.SDR RJEF20180110001Engine · malfunctionedDURING FLIGHT, THE NR 1 ENGINE HAD A STALL CONDITION AND EGT OVERLIMIT, DUE THAT SITUATION THE AIRCRAFT DIVERTED. UNEVENTFUL LANDING. CARRIED OUT THE CORRESPONDING FAILURE ANALYSIS. FOLLOWED THE INSTRUCTIONS OF TSM 71-00-00-810-808-A, PERFORMED BORESCOPE SDR ASAA2018010823114Fault Message · false activationNR 2 ENGINE SHOWS A SHORT TERM FAULT 75-30802. THE T25 SIGNALS DISAGREE. ACFT GROUNDED. PERFORMED T/C 78273000, VERIFIED THE NR 2 ENGINE HAVE NO FAULTS MESSAGES PRESENT ON THE LAST 3 FLT LEGS. IAW 75-33 TASK 805 THE NR 2 ENGINE EEC BITE GROUND TESTS PASSED WSDR DALA2018010900173Engine · making metalATB/IFSD - RETURNED TO ATL DUE TO RIGHT ENGINE COMPRESSOR STALLS WITH VIBRATIONS AT TOP OF CLIMB. PULLED THE ENGINE BACK TO IDLE. CREW FOLLOWED QRH AND SHUT DOWN ENGINE DUE TO VIBRATIONS. EMERGENCY DECLARED. MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINE DASDR UIEA2018010700019Engine · malfunctionedDURING THE NR 2 ENGINE START, THE ENGINE ADVANCED TO 35 PERCENT N1 AND 74 PERCENT N2 ON ITS OWN AND RECEIVED IDLE DISAGREE EICAS. TROUBLESHOT IAW FIM 71-05 F/T 844. PERFORMED ENGINE RUNS IAW AMM 71-01-02. INDICATIONS NORMAL, OK FOR SERVICE.SDR DALA2018010800124Engine · failedRETURNED TO DEPARTURE DUE TO RIGHT ENGINE COMPRESSOR STALLS WITH VIBRATIONS AT TOP OF CLIMB. PULLED THE ENGINE BACK TO IDLE. CREW FOLLOWED QRH AND SHUT DOWN ENGINE DUE TO VIBRATIONS. CORRECTIVE ACTION: MAINTENANCE FOUND METAL IN TAIL PIPE AND TURBINE DAMAGE. SDR CALA2018010700084Engine · abnormalSTRONG MUSTY ODOR ON DESCENT. REMOVED AND REPLACED NR 1 ENGINE REF WC 19-7100-1-0900.SDR IPXA2018010825233Engine · smokeEXCESSIVE SMOKE FROM THE NR 1 ENGINE AFTER SHUT DOWN. SERVICED WITH 2 QTS OF OIL IAW MM 71-00-00-0501. TESTED, NO DEFECTS NOTED.SDR PNSA2018010501Engine · auto shutdownRIGHT ENGINE FAILURE, DID NOT ATTEMPT RESTART. ENGINE AUTOSHUT DOWN IN FLIGHT.SDR UIEA2018010800041Circuit Card · failedRIGHT ENGINE SPEED CARD MESSAGE DISPLAYED. REMOVED & REPLACED THE NR 2 ENGINE N2 SPEED CARD IAW AMM 73-21-54. OPS CHECKED OK.SDR CNMA2018010001Engine · vibrationAT 25000 FT STILL CLIMBING RIGHT ENGINE GAVE OUT A LOUD BANG FOLLOWED BY HIGH VIBRATION , LOW N1 AND HIGH N2. EGT APPEARED TO BE NORMAL. CORRECTIVE ACTION:RIGHT ENGINE REMOVED & REPLACED IAW OAI WC 71-R07-RSDR HDNA2018F00066Engine · making metalENGINE CHIP INDICATION. PILOT FOLLOWED EMERGENCY PROCEDURE AND SHUT ENGINE DOWN AND PERFORMED RUN-ON LANDING. UPON INSPECTION OF CHIP DETECTOR FOUND CATEGORY 1 SLUDGE TYPE MATERIAL. PERFORMED PENALTY RUN WITH NO DEFECTS NOTED.SDR 2018FA0000085Engine · making metalAIRCRAFT POWER WAS APPLIED BY CREW FOR ENGINE START. CREW OBSERVED ENGINE CHIP DETECTOR LIGHT CAME ON. REMOVED BOTH CHIP DETECTORS AND FOUND SIGNIFICANT METAL ON BOTH PLUGS. AIRCRAFT WAS GROUNDED.SDR 2018FA0000084Bearing · failedDURING A SCHEDULED AIRFRAME EVENT NR 3, AND ENGINE 150 HOUR INSPECTION, SIGNIFICANT METAL WAS FOUND ON BOTH ENGINE CHIP DETECTORS AND IN THE OIL SIDE OF THE CEFA FILTER ASSEMBLY. ENGINE WAS REMOVED AND SENT TO ENGINE SHOP FOR REPAIR. ENGINE WAS REINSTALLED SDR 2018FA0000083Engine · making metalAIRCRAFT POWER WAS APPLIED, CREW OBSERVED ENGINE CHIP DETECTOR LIGHT CAME ON, WENT OFF AND THEN STAYED ON. REMOVED BOTH CHIP DETECTORS AND FOUND SIGNIFICANT METAL ON BOTH PLUGS. AIRCRAFT WAS GROUNDED.SDR HYIA2017010500001Engine · shutdownPILOT REPORTED THE RIGHT ENGINE SHUTDOWN IN FLIGHT. OPENSDR 2018FA0000090Bearing · failedDURING A NORMAL ENGINE SHUTDOWN, EXCESSIVE ENGINE NOISE WAS NOTED. SIGNIFICANT METAL WAS FOUND ON BOTH ENGINE CHIP DETECTORS. ENGINE WAS REMOVED AND SENT TO ENGINE SHOP FOR REPAIR. ENGINE WAS REPAIRED AND REINSTALLED. IT WAS RELAYED THAT THERE WERE SEVERASDR SWAA2018010218709Engine · damagedAIR TURNBACK, LEFT ENGINE VIBRATION 4.1. PULLING BACK WILL REDUCE. R&R NR 1 ENGINE FAN BLADE PLATFORM PER MT.SDR UIEA2017123102456Engine · vibrationVIBRATION MONITOR FOR THE LEFT LOW PRESSURE TURBINE, MAXED OUT AT 5.0 DURING CLIMB OUT WITH ASSOCIATED ENGINE HUM. DURING CRUISE FLIGHT 4.4 AND VIBRATION INDICATED. DURING DESCENT NOTICEABLE VIBRATION FELT AND HEARD ASSOCIATED WITH LEFT LPT HIGH VIBRATION INDSDR CALA2017122804626Line · cloggedLEFT ENGINE, AFTER START AND STARTER CUTOUT, N1 17%, SHOULD BE 22%, AND N2 AT 52%, SHOULD BE 58%. WITH NO THROTTLE RESPONSE. FOUND PS3 OUT OF SIGNAL FAULT. BLEW OUT PS3 LINE IAW FIM 73-26-0 0-810-803. COMPLIED WITH ENGINE RUNS AND EEC BITE AGAIN AND FOUND NSDR 2VKA2017122803Engine · making metalDURING FLIGHT, THE AIRCRAFT YAWED LEFT AND THE ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE PILOT LANDED THE AIRCRAFT IN A FIELD. MECHANIC INSPECTED THE ENGINE CHIP DETECTORS AND FOUND EXCESSIVE METAL ON THE DETECTORS. THE ENGINE WAS REPLACED.SDR AALA201712299015Engine · overtempAFTER LANDING, THE NR 1 ENGINE OVERTEMPED AT IDLE, OIL PSI WENT TO ZERO. SHUTDOWN THE NR 1 ENGINE. FOLLOWED ECAM, FIRE PUSH BUTTON, NO INDICATION OF FIRE. REPLACED THE NR 1 ENGINE IAW JC 26L40071004. OPS AND LEAK CHECKED GOOD. AIRCRAFT WAS GROUNDED.SDR AALA201712279014Fan · out of balanceNR 2 ENGINE VIBRATION OF 1.5 UNITS FROM TAKEOFF TO START OF DESCENT, 2 HOURS. MAINTENANCE ACCOMPLISHED FAN TRIM BALANCE IAW MCM CARD 77-95-12SDR DALA2017122608896Pma · failedDIVERTED DUE TO LEFT ENGINE HAD AN IN FLIGHT SHUTDOWN. FOUND THE LEFT ENGINE PMA FAILED. PMA REPLACED, AND RUN-OUT INSPECTIONS COMPLETED. HIGH POWER RUNS COMPLETED AND NO LEAKS.SDR DALA2017122608877Engine · failedDIVERTED DUE TO THE NR 2 ENGINE FAILED DURING CLIMB OUT. CREW DID SHUT ENGINE DOWN. MAINTENANCE FOUND METAL IN THE TAIL PIPE AND TURBINE DAMAGE. THE ENGINE WAS CHANGED.SDR UIEA2017122302425Unknown · vibrationNR 1 ENGINE VIBRATION DURING FLIGHT. PERFORMED A HEAVY INSPECTION OF INLET , FAN EXHAUST DUCT & LPT, NO DISCREPANCIES NOTED , PERFORMED PIMU BITE CHECK ON THE NR 1 ENGINE VIBRATION BOX, NO FAULTS NOTED IAW FIM 71-05 FT 854. OK FOR SERVICE.SDR UIEA2017122502434Engine · odorSTRONG BURNING ODOR FOR ABOUT 5 MINUTES, AT FL 400. REMOVED AND REPLACED THE NR 1 ENGINE IAW AMM 71-00-02, LEAK CHECKED AND ENGINE RUNS GOOD.SDR SIMA20171222001Engine · failedDURING DECENT AT 5000 FT, STARTED SMELLING OIL, ALSO DURING ENTIRE FLIGHT. CHECKED OIL PRESSURE, WENT FROM 63 LBS TO 88 FLUXUATION THE ENTIRE FLIGHT. AFTER DESELECTING THE NR 1 PACK. THE ODOR WENT AWAY. RESELECTED PACK AND ODOR CONTINUED. AT ALL OTHER ASDR DALA2017122108917Engine · odorODOR PREVALENT AFTER TAKEOFF AND THROUGHOUT FLIGHT. ODOR STRONGEST FROM RT PACK ON THE NR 2 ENGINE BLEED. NO CONTAMINATION WAS FOUND. FOUND TURBINE OIL ODOR ISOLATED TO THE NR 2 ENGINE. SUSPECT ISSUE WITH BUFFER AIR VALVE. REPLACED NR 2 ENGINE BUFFER AIR VSDR 4DUA201712210001Engine · flamed outNR 2 ENGINE FLAMED OUT DURING TAXI FOR DEPARTURE. TROUBLESHOOTING IN WORK BY GO TEAM WITH AOG SUPPORT.SDR IPXA2017121924645Engine · failedREJECTED TAKE OFF, DUE TO A LOUD POP. SEVERAL OBSERVORS SAW FLAMES FROM THE LEFT ENGINE, REJECTION WAS ABOUT 100KTG. FOUND METAL PARTICALS IN THE TAIL PIPE. IAW AMM 72-00-00-206-096, PARA L, 3 A THE NR 1 ENGINE WAS REMOVED AND REPLACED.SDR 29GA2017121800002Engine · oil consumptionPRECAUTIONARY SHUTDOWN OF THE LT ENGINE DUE TO LOW OIL PRESSURE WITH FLUCTUATIONS. INSPECTED LT ENGINE, FOUND B-SUMP SCAVENGE LINE LOOSE, REMOVED ALL SCAVENGE SCREENS AND INSPECTED WITH NO DEFECTS FOUND IAW MM & TASK CARDS 79-11-07, 79-11-09. REMOVED CHIP DETSDR ASAA2017121522941Pin · out of positionDURING ACCOMPLISHMENT OF E/C SBCFM56-7B-72-0986 ENG S/N #2 ENG FOUND STAGE NR 2 ANTI-ROTATION PIN AT 9 O'CLOCK ROTATED ABOUT 80 DEG. ACFT GROUNDED. REPLACED THE NR 2 ENGINE IAW T/C 7847100, & 78471001.SDR O2GA2017121987202Engine · power lossDESCENDING THROUGH FL 180, EXPERIENCED LEFT ENGINE LOSS OF POWER. ADVANCING THE POWER LEVER HAD NO AFFECT ON ENGINE POWER. ALL ENGINE INDICATIONS CONTINUED TO ROLL BACK UNTIL ENGINE WAS NO LONGER PRODUCING POWER. CHECKLIST WAS FOLLOWED. ENGINE WAS SECURED AND
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