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 CA081217014Engine · making metal(CAN) DURING T/O CLIMB, THE ENGINE OUT LIGHT CAME ON AND THE CREW ELECTED TO SHUT THE ENGINE DOWN AND RETURN TO THE POINT OF DEPARTURE FOR AN UNEVENTFUL SINGLE LANDING. GROUND INSPECTION SHOWED OIL FILTER BYPASS INDICATORS ACTIVATED AND METAL WAS FOUND ON THESDR USAABB08174Bolt · looseFLT 816 EN ROUTE. DURING DESCENT, FLT RECEIVED AN INDICATION OF NO OIL PRESSURE IN NR 2 ENGINE. CREW SHUTDOWN NR 2 ENGINE. LANDED WITHOUT FURTHER INCIDENT. SINGLE ENGINE TIME APPROX 15 MIN. MX FOUND MAGNETIC CHIP DETECTORS OF NR 2 ENGINE CONTAMINATED. RSDR DL76L081696Engine · making metalLARGE PIECE OF FERROUS METAL FOUND IN ANGLE GEAR BOX CHIP DETECTOR. FOUND LARGE METAL CHIP OBSTRUCTING VALVE. REPLACED ANGLE GEAR MCD AND HOUSING WILL NEED LEAK CK PER MM. REMOVED AND REPLACED NR 1 ENG PER TRANSMITTAL 1T148AD.SDR SWIA200820609Engine · overspeedFLT 5700 - RIGHT NP WENT TO 103 PERCENT DURING TAKE OFF. ACCOMPLISHED ENGINE RUNS, UNABLE TO DUPLICATE.SDR UALA2008120406752Engine · hot startNR 1 ENG HOT START, MAX EGT 768. (EXCEEDS 535). SEE EICAS ENG EXCD FOR MAX EGT AND DURATION. CREW COMMENTS: NO FUEL INITIATED DURING START. INSPECTED ENGINE INLET AND EXHAUST. RAN ENGINE IN GATE START WAS NORMAL. CREW STATED IT HAD EGT INDICATION ON PUSHSDR DXTA2008120503386Engine · stoppedRT ENGINE QUIT WHEN THROTTLE WAS BROUGHT TO IDLE.SDR ZZDA2008179Engine · failedDURING CLIMBOUT OF 14,500 HEARD A LOUD BANG. LOST NR 2 ENGINE. NORMAL DESCENT. RAN QRH. LANDING WEIGHT 102,400, MAX TGT 1148. REMOVED AND REPLACED NR 2 ENGINE ON TASK CARD 603 AS REQUIRED. LEAK AND OPS CHECKED GOOD. POWER ASSISTANCE TEST PASSED.SDR UPS08854080Engine · flamed outINSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT. ENGINE RELIT ON IT'S OWN. PERFORMED FIRST FOUR STEPS OF DC-8 M/M 71-00-00-1 FIG 139 UP TO INSPECT FUEL FILTER. FILTER KIT ON ORDER. REPLACED NR 3 FUEL FILTER PER AMM 73-10-02-4. LEAK CHECK OK. ACCOMPLISHED STEPSDR CA081210009Engine · odor(CAN) DURING CRUISE, THE PILOTS NOTICED OIL ODOR AND MIST IN THE CABIN. THEY TURNED THE AIR BLEED FROM THE ENGINE OFF AND THE MIST AND ODOR DISAPPEARED. SOON AFTER, OIL PRESSURE FLUCTUATIONS AND THEN A DROP IN PRESSURE OCCURRED. THE PILOTS SHUT DOWN THE ENGSDR SWIA200820601Engine · sluggishFLT 7790 - RIGHT ENGINE VERY SLOW TO SPOOL UP ON TAKEOFF; RECEIVED AN AUTOFEATHER AURAL WARNING WITH SWITCHES IN CORRECT POSITION. COMPLETED RIGHT ENGINE TRIM ADJUSTMENTS.SDR UPS08554083Engine · faultyINSPECTION TYPE:N/A RT PACK EXTREME ODOR/FUMES WHEN OPERATING SHUT DOWN RT PACK & FUMES EXTINGUISHED. ACCOMPLISHED NR 2 ENG PWR RUN PER MM 71-00-00-5. OIL FUMES EMITTED FROM NR 2 ENG WITH EITHER PACK L OR R SELECTED AND ENG ABOVE GRD IDLE. FUMES DISSIPATED SDR 2008FA0000854Spur Gear · brokenGAS PRODUCER TRAIN IDLER SPUR GEARSHAFT PN: 23038229. SHEARED IN HALF, PRODUCING METAL IN OIL. WHEN TECHNICIAN DISASSEMBLED GEARBOX FOUND THAT GEARSHAFT WAS THE SOURCE OF THE METALSDR CA081201005Gasket · leaking(CAN) THIS ENG WAS NOTED TO HAVE A OIL LEAK COMING FROM THE BOTTOM OF THE DIAPHRAGM AT THE 2 BOTTOM BOLT HOLES CLOSEST TO THE CHIP DETECTOR. THE GASKET WAS NOTED TO BE STICKING OUT AND NOT SEALING PROPER. UPON FURTHER INVESTIGATION THE OLD STYLE GASKETS PN 310SDR CA081210010Engine · power loss(CAN) DURING CLIMB AFTER T/O, ENGINE POWER LOSS OCCURRED (AT APPROX 300 FT ALTITUDE). THE ENGINE WAS SECURED AND A TURNBACK INITIATED. THE ACFT MADE A SINGLE ENGINE LANDING. POST EVENT INSP FOUND FRACTURED HP BLADES. MFG WILL CONTINUE INVESTIGATING THE EVENT ASDR C2XA08CL123Engine · faultyCLE - FLIGHT 2311 - THE CREW REPORTED AT FL320 THE NR 2 ENGINE ITT STARTED INCREASING SLOWLY TO 860 WITHOUT FULL THRUST. ASSENTING AT 91PERCENT N2 THE ENGINES HAD A 30 DEGREE DIFFERENCE. THE FUEL FLOW WAS ALSO NOTED TO BE 30 PPH HIGH. MAINTENANCE INSPECTED ASDR CA081203007Engine · making metal(CAN) DURING CLIMB AT FL60, THE CREW NOTICED A LOW ENGINE OIL PRESSURE LIGHT, FOLLOWED BY A POPPING NOISE. THE ENG WAS SHUTDOWN AND THE ACFT WAS DIVERTED BACK TO BASE. GROUND INSP FOUND THE TURBOMACHINE CHIP DETECTOR COVERED WITH METAL SHAVINGS AND THE LP AND SDR DL777081650Engine · fluctuatesRT ENG PARAMETERS FLUCTUATED AND ENG PWR SHORTFALL AT FL390 WITH ENG RESPONSE EICAS MSG. PERFORMED QRH 7.25 AND DESCENDED TO FL310. CORRECTED PROBLEM. FUEL TEMP WAS -22 AND OAT -56. MTC IN PROGRESS.SDR ABXA200812050267Engine · failedAT APPROXIMATELY 600 FEET ON TAKEOFF, RIGHT ENGINE COMPRESSOR STALLED. EGT EXCEEDANCE OF 1053 DEGREES WAS RECORDED. ENGINE FAILED ON FINAL. REPLACED RIGHT ENGINE IAW JOB CARD 7010.SDR UALA2008112606673Engine · making metalMETAL IN NR 1 ENGINE CHIPS AND OIL SCREEN.SDR ZESA2008016Bearing · debondedON 11/25/08 CREW REPORTED "ENGINE CHIP DETECT R". MAINTENANCE INSPECTED THE CHIP PLUG WITH NO METAL FOUND. ON 12/13/08 CREW REPORTED INTERMITTENT ILLUMINATION OF THE SAME LIGHT. MX REMOVED CHIP DETECTOR AND FILTER WITH NO METAL FINDINGS. ON 02/09/09 THE SASDR CA081203003Engine · malfunctioned(CAN) SHORTLY AFTER TAKE OFF OIL MIST IN CABIN WAS DETECTED. THE ACFT IMMEDIATELY TURNED BACK, DECLARED AN EMERGENCY, AND LANDED. THE LOCAL AIRWORTHINESS AUTHORITIES ARE INVESTIGATING THE EVENT. POST FLIGHT INSP REVEALED OIL IN THE VICINITY OF THE P2.2 BLEED VSDR CA081203002Engine · malfunctioned(CAN) ON TAKEOFF ROLL WITH PASSENGERS ON BOARD POWER WAS ADVANCED THROUGH 70 PERCENT TORQUE. A THUD AND GRINDING NOISE WAS HEARD FROM THE RT SIDE. TAKEOFF WAS ABORTED AND AC RETURNED TO THE GATE. ENG TO BE REMOVED AND SENT FOR INVESTIGATION. MFG WILL CONTINUSDR SIMA200833602Engine · smokeON FLIGHT 4553, AFTER 80 KTS ON TAKEOFF ROLL COCKPIT BECAME HAZY WITH SMOKE ACCOMPANIED BY ODOR. ABORTED TAKEOFF. SMOKE DISSIPATED FAIRLY RAPIDLY. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED NR 1 ENGINE OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SSDR DXTA2008112603373Engine · shutdownDURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROUGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUTDOWN.SDR UALA2008112406649Engine · damagedNR 1 ENGINE - CRACK FOUND IN 6-7 AIR SEAL.SDR DLM88081640Engine · smokeDURING CRUISE, FLIGHT ATTENDANT REPORTED SMOKE IN CABIN. BOTH AFT LAV SMOKE DETECTORS WERE GOING OFF. ENGINE ANTI-ICE ON, LT PACK TURNED OFF SMOKE OUT. CAPTAIN DECLARED EMERGENCY ON APPROACH. LANDED AT SCHEDULED DESTINATION. REPLACED NR 1 ENGINE.SDR CA081125020Engine · making metal(CAN) PILOT REPORTED NR 2 ENG CHIP LIGHT ILLUMINATED AT TOP OF CLIMBOUT, IMMEDIATELY FOLLOWED BY A SURGE AND POWER LOSS. PILOT PREPARED FOR A RUN-ON LANDING. NR 2 ENG WAS SECURED, PASSENGERS WERE BRIEFED AND TRAFFIC AND DISPATCH WERE ALERTED. NR 1 ENG WENT TOSDR UALA2008112406648Engine · damagedMETAL FOUND IN MASTER CHIP DETECTOR AND NO ROTATION OF ENGINE WITH ASSOCIATED ENG CONTROL, EEC C1 AND PMA MESSAGES.SDR UALA2008112106607Engine · bird ingestionRTFL DUE TO BIRD STRIKE. PERFORM NR 1 ENG BURNOUT PROCEDURE DUE TO ODOR IN CABIN (BIRD STRIKE NR 1 ENGINE). REMOVE NR 1 ENGINE DUE TO LPC STG 1 BOOSTER DAMAGE AND LINER SEPARATION.SDR C8GA20080032Engine · damagedFLT 201 FROM MIA TO CCS - AFTER TAKEOFF WITH FLAPS RAISED APPROX 1800 FEET AND CLIMB THRUST SELECTED, 3 QUICK COMPRESSOR STALLS WERE HEARD AND FELT FROM THE NR 1 ENGINE. APPROPRIATE CHECKLIST WAS PERFORMED, EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SDR ASAA0853807Engine · surgesJUST PRIOR TO LEVEL OFF AT FL 340 NR 2 ENG BEGAN TO SURGE BETWEEN 80 PERCENT AND RED LINE ON N1 GAGES N1 INDICATION RED BOXED MOMENTARILY TWICE EGT N2 FUEL FLOW WERE SURGING AS WELL. E 1.5 CHECKLIST FOLLOWED AT POWER REDUCTION EVERYTHING SMOOTHED OUT AND ENG RSDR CA081125016Engine · shutdown(CAN) DURING CRUISE AT FL190, THE ENGINE SPOOLED DOWN UNCOMMANDED. EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED AND A SINGLE ENGINE LANDING WAS ACCOMPLISHED. MFG WILL CONTINUE INVESTIGATING THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED.SDR C2XA08IA240Engine · malfunctionedIAH - FLIGHT 2574, THE CREW REPORTED A LAV SMOKE DETECTOR WARNING DURING CLIMB. THE AIRCRAFT RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NUMBER TWO ENGINE, OPERATIONALLY CHECKED WITH NO DEFECTS, AND THE AIRCRAFT WASSDR HALA2008111700856Fan Blade · distortedETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE FAN BLADE 17 IS DISTORTED 1ST STAGE FAN. INSPECTED NR 1 ENGINE 1ST STAGE FAN BLADE 17. DISTORTION IS WITHIN LIMITS PER AMM 72-31-02-226-007-G00 SECTION U. RAN NR 1 ENGINE ALL PARAMETERS WITHIN TOLERANCE NO EXCESSISDR HALA2008111700855Fan Blade · distortedETOPS SIGNIFICANT SYSTEM, FOUND NR 1 ENGINE FAN BLADE 18 IS DISTORTED 1ST STAGE FAN. INSPECTED NR 1 ENGINE 1ST STAGE FAN BLADE 18. DISTORTION IS WITHIN LIMITS PER AMM 72-31-02-226-007-G00 SECTION U RAN ENGINE ALL PARAMETERS WITHIN TOLERANCE NO EXCESSIVE VIBESDR CA081125012Engine · failed(CAN) DURING CRUISE, WITH NO WARNING THE LT ENG SHUTDOWN ACCOMPANIED WITH A LOUD NOISE. THE FIRE WARNING FOLLOWED AND THE CREW DISCHARGED BOTH FIRE BOTTLES BEFORE DIVERTING THE FLIGHT WHERE A SINGLE ENGINE LANDING WAS ACCOMPLISHED. POST FLIGHT INSP REVEALED THSDR CA081125015Engine · making metal(CAN) DURING CRUISE FLIGHT, THE NR 1 ENG CHIP DETECTOR LIGHT ILLUMINATED. THE PILOT "BURNED" THE CHIP DETECTOR AND THE LIGHT WENT OUT. SHORTLY AFTER THE LIGHT CAME ON AGAIN AND THE PILOT BURNED AGAIN AND THE LIGHT WENT OUT. HE DECIDED TO ABORT THE MISSION AND SDR ASAA0853779Spinner · wornSPINNER FRONT CONE MISSING MORE THAN 20 PERCENT OF BLACK ANODIZED COATING. REMOVED AND REPLACED SPINNER CONE REF MM 72-21-01.SDR ASAA0853773Engine · making metalFOUND MATERIAL IN AFT SUMP CHIP DETECTOR NR 2 ENGINE FOUND APPROX 4 PIECES ALL NON MAGNETIC. THE LARGEST APPROX 0.400". UNABLE TO DETERMINE MATERIAL. RAN ENGINE NR 2 AT HIGH PWR PER CHIP ANALYSIS MANUAL. SENT MATERIAL TO SEA FOR EVALUATION. NO PARTICLES NOSDR AALA200802522Engine · vibrationDFW INFLIGHT - AT CRUISE NR 2 ENGINE VIBRATIONS WERE ABOVE 2.0. FLUX BETWEEN 3.0 AND 1.6. CREW SHUT DOWN ENGINE. LANDED DFW WITHOUT INCIDENT. COMPRESSOR AND TURBINE BLADES CHECKED OKAY. REPLACED NR 2 ENGINE ON 14 NOV AT DFW DUE TO VIBRATIONS. SYSTEM GROUNSDR CA081125010Oil System · leaking(CAN) DURING CRUISE AT FL270, THE PILOT NOTICED OIL ODOR AND SMOKE IN CABIN. HE ELECTED TO SHUTDOWN THE ENG AND SHORTLY AFTER, PERFORMED A UNEVENTFUL SINGLE ENGINE LANDING. POST FLIGHT INSP AND GROUND RUNS REVEALED OIL COMING OUT OF THE INLET AND COMPRESSOR BLSDR CA081114006Bearing · corroded(CAN) RECEIVED NEW BEARING FROM WHS 290 WITH CORROSION ON BEARING JOURNAL AND ROLLERS. CURE DATE ON PACKAGE IS 0206, BEARING PN SB3208A-1. BATCH PN 0605118341. HSI HAVE BEEN INFORM OF VARIOUS BEARINGS DELIVERED THAT HAVE SIGNS OF CORROSION ON THEM.SDR ASAA0873765Engine · surgesAPPROX 1500' AGL ON TAKEOFF RT ENG SURGE/STALL APPROX 3 TIMES RIGHT AFTER POWER REDUCTION. SLIGHTLY HIGH EGT RT ENG A/T OFF AND POWER REDUCTION PER QRH ENG RAN NORMALLY J HOOK INSPECTION FAILED. DAMAGE NOTED ON THE HPC BLADES. EVIDENCE OF BIRDSTRIKE. NR 2 SDR CA081125008Engine · malfunctioned(CAN) DURING CLIMB, THE CREW FELT A SUDDEN YAW AND OBSERVED NR 2 ENGINE TEMP GAGE AT MAX. READING ACCOMPANIED BY AN EEC FAULT. NO UNUSUAL NOISES WERE REPORTED BUT PERSONNEL IN THE REAR OF CABIN REPORTED A SPIKE OF FLAME FROM THE EXHAUST. THE CREW ELECTED TO SHSDR DXTA2008111303352Engine · malfunctionedRIGHT ENGINE QUIT ON LANDING ROLL OUT.SDR DXTA200811113349Engine · unknownRT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES IDLE. REMOVED LT/RT ENG LWR COWLS FOR ACCESS. RE-RIGGED RT FDV TO FUEL CONTROL RD. ADJUSTED RT THROTTLE CABLE. INSPECTED LT FDV TO FUEL CONTROL RIGGING AND THROTTLE RIGGING AT FCU NO DEFECTS NOTED. RASDR CA081125006Engine · flamed out(CAN) DURING SHORT FINAL, UPON REDUCING THE POWER TO IDLE, THE ENGINE FLAMED OUT. THE EVENT OCCURRED AT AN ALTITUDE OF APPROX. 100 FEET AND THE CREW LANDED THE ACFT SINGLE ENGINE. NOV. 12 2008: ENGINE FLAME-OUT EVENT OCCURRED WHILE DEPLOYING THE THRUST REVERSDR DL77L081530Engine · malfunctionedPERFORMED EA 54-41523-14 ORIG REMOVED STARTER GEARSHAFT AND TGB REMOVED AND REPLACED. REMOVED AND REPLACED NEC TUBES AND BRACKETS FOR ACCESS. PERFORMED TEST NO FAULTS DRY MOTOR NO LEAKS COMPLETED EA 54-471523-14 ORG OPERATED NR 1 ENG PER 71-00-00-700-805 TESSDR ASAA0853756Engine · surgesRIGHT ENGINE N1 SURGE AT 32FL DURING CLIMB. REDUCED POWER AND RETURNED TO ANC. ENGINE REPLACEMENT IN PROCESS. WILL BE SENT TO GE FOR ANALYSIS.SDR DXTA2008111203349Engine · shutdownRIGHT ENGINE QUIT ON LANDING APPROACH ABOUT 100 AGL THROTTLES AT IDLE.
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