GE CF6-80C2D1F
Service difficulty reports · 536
Newest first. General aviation reporting is voluntary.
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 engine_model_key = 'CF680C2D1F' 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 engine_model_key = 'CF680C2D1F' 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 EVAS091022Engine · flamed outNR 2 ENGINE FLAMED OUT AFTER START. NR 2 ENGINE WET MOTORING AND DRY MOTORING. NR 2 ENGINE IDLE RUN TEST NML IAW AMM 71-00-00SDR CA021121002Fairing · damaged(CAN) PANELS 462EL AND 462FL FOUND MISSING OFF NR 2 ENGINE PYLON AND NR 1 TRAILING EDGE FLAP AND CANOE FAIRING FOUND DAMAGED ON WALK AROUND. AIRCRAFT WAS ON A DELIVERY FLIGHT AFTER HAVING UNDER GONE A HEAVY MAINTENANCE VISIT IN SINGAPORE. AIRCRAFT RELEASED FROSDR EVA200203EngineCAPT REORTED :FIRE WARNING INTERMITTEM,ACRAS DOWNLINK MSG:NO.1 ENG N2 VIB 5.0,EGT 2022,A/C AIR RETURN TO ANC. MAINTENANCE GOUND INSPECTION,1.FOUND NO.1 ENG TAIL PIPE BROKEN, N1 SIEZED, BIG CHIP FOUND AND TWO FIRE BOTTLES DISCHARGED. 2.NO.1 ENG LEVER ARM STG #SDR 02FDEA00062Fire Loop · faultyAFTER ROTATION NR 1 ENG FIRE DET NR 1 FAULT CAME ON. REMOVED AND REPLACED FDCU AS PRECAUTION PER MM 26-11. REMOVED AND REPLACED NR 1 LWR TURBINE FIRE DET LOOP-B PER MM 26-11-03-4. CLOSED AND LATCHED NR 1 ENG COWLING PER MM 71-10-00.SDR 02FDEA00011Bolt · looseDURING PFM NR 44 CHECK FOUND RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE.SDR 02FDEA00012Bolt · looseDURING PFM NR 61 B-CK FOUND BOTH LT & RT AFT MOUNTING BOLT OF CTR LANDING GEAR TRUNNION PIN PILLOW BLOCK LOOSE.SDR 01EVA006Engine · unserviceable1.AIRCRAFT LOW SPEED T/O ABORTED (ABOUT 95 KTS) DUE TO "ENG FAIL" LT ON WITH "BAN" SOUD HEARD. AFTER ABORT ACTION COMPLETED. "ENG FAIL" RED LT WENT OFF. 2.GND VISUAL INSPETED NO. ENG EXHAUST SLEEVE, FOUND METAL CHIP AROUND INNER SURFACE, AND METAL CHIPS FOUND SDR 01FDEA00934Engine · making metalNR 2 ENG N1 FAILED TO ATTAIN T/O THRUST. MAINTENANCE FOUND METAL IN THE TAILPIPE.SDR 01FDEA00853Oil Cooler · leakingNR 1 ENG OIL QTY DROPPED 10 GAL. REMOVED AND REPLACED FUEL/OIL COOLER AND DRAINED AND FLUSHED ENGINE.SDR 01EVA005Engine · fire warning1.AIRCRAFT REG. NO.B-16110, "ENG 1 FIRE"WARNING ON CLIMB PASSING ABOUT 3000 FT. PROBLEM CLEAREDWHEN THROTTLE REDUCED. PROBLEM RECURRED WITH CLIMB POWER RESELECTED. RETURNED TPE WITH REDUCED POWER ON NO.1 ENGINE WITHOUT SHUTTING DOWN ENGINE.2.ON GROUND, MAINTENSDR EVA004Engine · broken1. A/C B-16408 :Captain report: In cruise found No.1 Engine Vibration 3.0 and EGT higher than other engine.2. On ground check found some metal chips in tail pipe. Request BSI.3.BSI found No.1 Engine HPC Stage 6 had several blades severe damage. 4.Engine ChangeSDR EVA003Engine · flamed out1. AIRCRAFT B-16103 DURING CRUISE 5 MINUTES BEFORE TOD, "ENG 2 RPM LO" LEVEL 2 ALERT APPEARED. FOLLOWED CHECK LIST, AIR RESTART WAS SUCCESSFUL.2. ON GROUND, CHECK CFDS NO RELATED FUALT FOUND.3. CHECK ENGINE CONDITION ALL NORMAL. EEC TEST PASS. PERFORM ENGINE RSDR EVA002Engine · fod1. AIRCRAFT B-16107 DURING T/O RUN IN BRU, A/C NO.3 ENGINE BIRD STRIKE. VIBRATION JUMP UP TO 4.2 & FELT BY THE CREW. CAPTAIN S/D THE ENGINE, DUMP FUEL AND AIR RETURN TO BRU.2. ON GND, VISUAL CHK FND 3 FAN BLADES DAMAGED.3. PFM BSI ON #3 ENGINE, ALL COND NML.4.SDR 20010423CW003Ignition Switch · failedPILOT REPORTED NR 2 ENGINE, LOW RPM WARNING APPEARED, LEVEL 2 WITH N 1 25 PER CENT, EGT, 100 THEN WENT TO 0. NR 2, 40 PER CENT, OIL QTY 20, RECOVERED AFTER IGN OVRD SELECTED DURING STARTED DESCENT. MAINTENANCE RAN NR 2 ENGINE WITH BOTH A AND B IGNITSDR 01FDEA00042Turbine · damagedON T/O, NR 1 ENG HAD SEVERE VIBRATION AND EVM TURBINE INDICATIONS. NO REDUCTION WITH REDUCED POWER, SECURED NR 1 ENGINE AND RETURNED TO PEK. MX FOUND METAL IN TAILPIPE AND LAST STAGE TURBINE SEVERELY DAMAGED. *S/D* REMOVED AND REPLACED NR 1 ENG PER WORK CASDR WRLA20011Bullet · delaminatedUPON DEPARTURE, AIRCRAFT EXPERIENCED ENGINE VIBRATION OF UNKNOWN ORIGIN IN NR 1 POSITION. EMERG PROCEDURES C/W, AND ACFT RETURNED TO DEPARTURE STA WITHOUT INCIDENT. UPON INSP BY WORLD AIRWAY MAINT REP, DISCOVERED THE NOSE CONE (SPINNER) ON NR 1 ENGINE HAD DESDR 00FDEA00323Check Valve · brokenY-DUCT, CHECK VALVE, FLAPPER''S ARE BROKEN. REMOVED AND REPLACED CHECK VALVE WITH SERVICEABLE UNIT (S/N AEX10641) ON.SDR 00FDEA00274Clamp · brokenLEFT HAND WHEEL WELL UPPER AUX TANK FUEL SUPPLY LINE, RETAINING CLAMPS ARE ALL BROKEN.SDR 00FDEA00305Clamp · brokenLT WHEEL WELL - UPR AUX TANK FUEL SUPPLY LINE, RETAINING CLAMPS ARE ALL BROKEN. ADJUSTED FWD MT BRACKET ASSY WHICH REMOVED PRELOAD ON CLAMP & REPLACED BROKEN CLAMPS (4 EA) PER SMP.SDR 20000407SH011Rccb · failedLAX/TPE - RIGHT EMER AC BUS'' OFF MESSAGE DURING FLIGHT. DIVERTED TO CTS WITH LIMITED INSTRUMENT. ''REAC SENS RELAY/INTFC'' CURRENT FAULT FOUND ON CFDS, BUT PERFORM EPU R-T-S TEST PASS AND CHECK ALL FUNCTIONAL NORMAL. FOR MAINTENANCE PREVENTION, REPLACED RCCSDR 00FDEA00068Warning System · activatedTWO MINUTES AFT T/O, NR 1 & 2 ENG FADEC MAINT L-1 ALERT. A/C RETURNED TO MEM.SDR AALA20000219Engine · vibrationMIA - FLT 1769 - DURING TAKEOFF, VIBRATION FOLLOWED BY HIGH EGT ON NR 3 ENGINE. HYDRAULIC PUMPS TURNED OFF.. SHUT NR 3 ENGIEN DOWN AND VIBRATION STOPPED. RETURNED AND LANDED MIA WITH INCIDENT. REPLACED NR 3 ENGINE. SYSTEM GROUND CHECK NORMAL OPERATION. (SDR 00FDEA00043Bleed Valve · malfunctioned00-24 - AC AIR TURN BACK DUE TO NR 1 BLD LOW ALERT. NR 2 BLD WAS ALREADY DEFERRED. NO LEAKS NOTED, FOR T/S MANUALLY CLOSED AND LOCKED APU LOAD BLD VALVE. REMOVED AND INSTALLED APU LOAD BLEED VALVE REF WRI 49-50/5443. PRESSURE DECAY TEST ALL PASSED. A/C OSDR 99FDEA00517Compressor · stalled99-299, COMPRESSOR STALLS NR 3 ENG, FLT LEVEL 320.SDR AALA991751Engine · stalledMIA - FLT 1769 - ON CLIMB-OUT FROM MIA, NR 2 ENGINE COMPRESSOR STALLS PASSING 12,000 FOOT CLIMB POWER. AIRCRAFT RETURNED AND LANDED MIA WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL WITH ENGINE AT IDLE FOR THREE MINUTES PRIOR TO ENGINE SHUTDOWN. AIRCRAFTSDR AALA19991751Engine · stalledMIA - FLT 1769 - ON CLIMB-OUT FROM MIA, NR 2 ENGINE COMPRESSOR STALLS PASSING 12,000 FOOT CLIMB POWER. AIRCRAFT RETURNED AND LANDED MIA WITHOUT FURTHER INCIDENT. ALL INDICATIONS NORMAL WITH ENGINE AT IDLE FOR THREE MINUTES PRIOR TO ENGINE SHUTDOWN. AIRCRAFTSDR 99FDEA00324Engine · bird strike99-200 - ON T/O A LARGE BIRD STRUCK THE RT SIDE OF THE A/C. ENG MADE LOUD NOISE PWR REDUCED, VIB WENT AWAY, AND RETURN FOR LAND. FAN BLADES REPLACED SEE WRI 72-10/4339 AND 72-10/4336. REVERSER TRANSLATING COWL REPLACED PER 78-30/4338. PERF TRIM BALANCE ON SDR 99FDEA00144Engine · malfunctioned99-89 - NR 3 ENG N1 INTERMITTENTLY DROPS AND A/C SHUDDERS. REMOVED AND REPLACED NR 3 ENG AS PER MM 71-00-02-4. REF WORK CARD 71T0101.SDR 99FDEA00130Filters · contaminatedLEVEL 1 ENG 3 FUEL FILTER ALERT AND LEVEL 1 FUEL CONTAMINATION ALERT DISPLAY. CREW DUMP FUEL TO REDUCE DOWN TO MAX WT. REMOVED AND REPLACED ALL THREE ENG FILTERS PER 73-11-04-04-1.SDR AALA980833Bearing · failedSEA - FLT 128 - DURING CRUISE NRT-SJC, NR 3 ENGINE DID AN UNCOMMANDED SHUTDOWN DUE TO EGT SPIKE. FLIGHT CREW ACCOMPLISHED ENGINE SHUTDOWN CHECKLIST AND CONTINUED TO SJC AND LANDED WITHOUT FURTHER INCIDENT. NR 3 ENGINE WAS INSPECTED BY MX AND THE GEAR BOX WASSDR 97FDEA00640Engine · failedAFTER T/O, NR 2 ENG CVM TURB 5.0 AMBER BOX ACCOMPLISHED BY VIBRATION IN AIRFRAME (3000) PRECAUTIONARY SHUTDOWN AT APPROX 6000 EGT INTERMITTENTLY BLANK BEFORE SHUTDOWN REDUCED PWR TO 60 PERCENT N1 NO CHANGE IN VIBRATION. FOUND MAJOR TURBINE CASE DAMAGE DUE TO SDR 97FDEA00375Duct · rupturedNR 1 ENGINE TURBINE CASE COOLING DUCT RUPTURED. CAUSING HEAT DAMAGE TO COMPONENTS AND ELECTRICAL WIRING FOR THE FOLLOWING SYSTEMS. HYDRAULIC, ENGINE OIL TEMP AND PNEUMATIC. NO ASSOCIATED FIRE WARNINGS OR ALERTS. *S/D* REMOVED AND REPLACED THE NR 1 ENGINE.SDR 97FDEA00256Engine · failed97-0079 STA-MNL, ON ROTATION THE NR 2 ENGINE EGT WAS BOXED AND AMBER. BROUGHT ENGINE BACK TO IDLE AND EGT ROSE TO 982, THEN HEARD AND FELT LOUD BANG. SHUT NR 2 ENGINE DOWN, DID NOT DUMP FUEL AND MADE EMERGENCY LANDING IN MANILA. REMOVED AND REPLACED THE NUSDR 96FDEA01560Engine · crackedENGINE FAILED INSP PER EA 1-7220-31514, INSP OF FIRST STAGE BOOSTER VANES. FOUND NUMEROUS LOOSE AND MISSING FASTENERS BOOSTER CASE CRACKED IN SEVERAL PLACES. REMOVED AND REPLACED NR 2 ENGINE. RII COMPLETED, ENG RUN, LEAK AND OPS CHECK GOOD.SDR 96FDEA01540Engine · failedENGINE FAILED INSPECTION PER EA 7-7220-31529 INSP OF FIRST STAGE BOOSTER VANES.SDR 96FDEA01541Engine · failedENGINE FAILED INSPECTION PER EA 1-7220-31511 INSP OF FIRST STAGE BOOSTER VANES.
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