GE CF6-80 series
Service difficulty reports · 1,092
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 = 'CF680' 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 = 'CF680' 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 UIEA2017102502045Blade · nickedNR 2 ENGINE FAN BLADE NR 3, HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE BLADE IAW AMM 72-31-02-308-045-H00. FPI OF THE FAN BLADE IAW AMM 72-31-02-308-045-H00. NO CRACKS NOTED.SDR UIEA2017102502044Blade · nickedNR 2 ENGINE FAN BLADE NR 19 HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE FAN BLADE IAW AMM 72-31-02-308-045-H00. FPI INSP OF THE BLADE IAW AMM 70-11-06-232-010-G00. NO CRACKS NOTED.SDR UIEA2017102502071Eec · failedDURING NR 2 ENGINE START, RIGHT IGNITION NR 2 BREAKER ON PS PANEL TRIPPED AND WILL NOT RESET. REMOVED AND REPLACED THE NR 2 ENG EEC IAW AMM 73-21-15-404-068-H00. COMPLIED WITH #2 ENG. MOTOR AND GROUND RUN IAW AMM 71-00-00-735-195-H03, AND 71-00-00-00. OPS CHSDR UIEA2017102602121Anti-Ice Valve · failedRIGHT ENGINE ANTI-ICE LIGHT. REMOVED AND REPLACED THE RIGHT COWL ANTI -ICE VALVE IAW AMM 30-21-03. RAN THE NR 2 ENGINE ANTI-ICE VALVE, OPERATES GOOD.SDR FDEA201710243043Control Unit · inoperativeAT ENGINE START, ATS SYSTEM ADVANCED UNCOMMANDED AT THE TIME OF A NR 2 ENGINE ROLLBACK. N2 ATTAINED APPROXIMATELY 87% BEFORE THROTTLES WERE MANUALLY RETARDED. REMOVED AND REPLACED FCU IAW 22-15-XX PERFORMED AFS/LANDS TEST IAW 22-00-XX ,22-40-XX, ALL TESTSDR P5CA2017101900362Compressor · stalledNR 1 ENGINE COMPRESSOR STALL ON DEPARTURE DURING CLIMB AT APPROXIMATEY 3000 MSL. OPENSDR UIEA2017091101630Warning Message · illuminatedRIGHT EEC EICAS MESSAGE AT 240 KTS.SDR UIEA2017091101634Clamp · unsecureFAN VIBRATION INDICATED HIGHER THAN 3.5 THROUGHTOUT CLIMB , PEAK INDICATION 4.2 AT FL 270. PERFORMED FIM 71-05 FT 852, NO DEFECTS NOTED, ENGINE RAN OK. TROUBLESHOOTING THE ENGINE VIBRATION FOUND COOLING DUCT CLAMP LOOSE AT 10 O CLOCK POSITION. TIGHTENED THSDR IPXA2017082721003Engine · overheatedRT ENGINE OVERHEAT MESSAGE, RAN QRH, PULLED ENGINE BACK 1 KNOB AND THE LIGHT WENT OUT. REMOVED AND REPLACED THE NR 2 ENGINE.SDR CALA2017082102815Tube · brokenDURING TAKEOFF POWER UP, THE LEFT ENGINE N1 FAILED TO REACH TAKEOFF THRUST, ONLY REACHED 89 PERCENT. FOUND BROKEN PS3 LINE. R & R THE LINE IAW AMM 73-21-24-206-001-H00. HIGH POWER RUN SATISFACTORY. AIRCRAFT OK FOR SERVICE.SDR DALA2017082306365Bracket · brokenFOUND SECTION OF BRACKET ON THRUST REVERSER SIDE BROKEN. BRACKET HOLDS STAND OFF FOR PRE COOLER DUCT. REMOVED AND REPLACED THE NR 2 ENGINE, INBD THRUST REVERSER HALF IAW SPC 73-7830-9-0014.SDR UIEA2017081501489Valve · malfunctionedRIGHT ENGINE SPAR VALVE OPERATIONAL CHECK UNSUCCESSFUL. RT ENGINE SPAR VALVE INDICATION INOPERATIVE. PERFORMED CONFIRMATION OF OPERATION IAW DDG 28-40-02.SDR UIEA2017050500713Fuel Control · faultedLT ENG CONTROL FAULT. REPLACE HYD FUEL CONTROL UNIT PER COMPANY REQUEST. REMOVED AND REPLACED HYDRO MECHANICAL FUEL CONTROL UNIT AND LEFT ENG EEC PART 1519M89P29 SERIAL LMDD7973 IAW AMM 73-21-14 AND SUBTASK 73-21-15-714-020-H00. PERFORMED TEST AND LEAK CHECK OSDR AALA201704289026Blade · brokenAIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE. LEFT ENGINE HAD MULTIPLE COMPRESSOR STALLS AT HIGH POWER DURING FLIGHT. LEFT ENGINE POWER REDUCED TO IDLE. LANDING UNEVENTFUL. FOUND A BROKEN BLADE. R & R THE ENGINE IAW MCM 71-93-0SDR UIEA2017040300503Rod End · wornRIGHT ENGINE COMPRESSOR CASE AT THE 9 O'CLOCK POSITION, TCC DUCT THREE SUPPORT RODS FOUND TO HAVE ROD END PLAY.SDR UIEA2017040300502Seal · detachedRIGHT ENGINE FAN CASE L/E SEAL UPPER PORTION, FOUND DETACHED.SDR UIEA2017040300501Drip Tray · tornRIGHT ENGINE AT THE 2 O'CLOCK POSITION, THE STRUT TO ENGINE FUEL HOSE DRIP SHIELD FOUND TORN.SDR UIEA2017040300499Blade · nickedRIGHT ENGINE, NR 31 FAN BLADE L/E FOUND WITH ONE NICK.SDR UIEA2017040300498Bypass Switch · no testLEFT ENGINE FUEL FILTER BYPASS SWITCH FAILED AN OPS TEST. THE BYPASS SWITCH WAS REMOVED AND REPLACED IAW AMM 73-34-01, REV 120. OPS TESTED IAW AMM 73-34-01 REV 120, AND FOUND SATISFACTORY.SDR UIEA2017040300497Connector · wornLEFT PACK COMPRESSOR OUTLET TEMP SENSOR TS41 FOUND THE ELECTRICAL CONNECTOR D00688 WORN. THE ELECTRICAL CONNECTOR WAS REMOVED AND REPLACED IAW WDM 21-51-12, REV 26. OPS CHECKED IAW 21-51-14, REV 120, AND FOUND SATISFACTORY.SDR IPXA2017030614797Engine · malfunctionedAIRCRAFT HAD DIFFICULTY CLIMBING THRU FL 31000. RT ENG FUEL FLOW AT .7 (700 LBS/HR), N1, EGT AND N2 WERE SIGNIFICANTLY BELOW LT ENG. CONDUCTED QRH ENGINE INFLIGHT. START CHECKLIST AND RT ENG STARTED WITH NO PROBLEMS. ENGINE OPERATED WITHIN ALL LIMITATIONSSDR UIEA2017030200252Blades · lack of lubeLEFT ENGINE FAN VIBRATION INDICATES 3.8 - 4.2 WITH STEADY CLIMB POWER. IAW MAINTENANCE ENGINEERING, COMPLETED FAN BLADE LUBRICATION IAW AMM 72-31-00. REMOVED FAN BLADES AND LUBRICATED. REINSTALLED. OPERATIONAL CHECKS AND VIBRATION OK ON ENGINE RUNS IAW MM 72-SDR UIEA2017030300297Blade · lack of lubeLEFT ENGINE FAN VIBRATION INDICATES 3.8-4.2 WITH STEADY CLIMB POWER. COMPLETED FAN BLADE LUBRICATION IAW AMM 72-31-00. REMOVED FAN BLADES LUBRICATED REINSTALLED .SDR IPXA2017030514720Fastener · missingINSPECTION TYPE: 2C, NR 2 ENGINE INLET COWL HAS A MISSING FASTENER. INSTALLED THE FASTENER IAW EA 011-7110-01-A6677, REV. I/R AND UPS EO MD11-7110-63395-A.SDR UIEA2017020700156Compressor · stalledAFTER TAKEOFF, EXPERIENCED A LT ENGINE COMPRESSOR STALL, NO ENGINE INDICATIONS DISPLAYED. INSPECTED EXHAUST FOR FOD, BOROSCOPED HPC STAGE 1, 6, AND 12 AND HPT STAGE 1 ALC IAW AMM 72.00.00. REMOVED AND INSTALLED BOROSCOPE PLUGS AND N2 DRIVE PAD IAW AMM 72.00.SDR UIEA2017011700047Tape · out of positionNR 1 ENGINE, INBD SIDE, 5:30 POSITION, COMBUSTION TURBINE HAS MIGRATED FROM UNDER CLAMPS, TWO AREAS. REMOVED AND REPLACED ANTI CHAFE TAPE ON NR 1 ENGINE INBD SIDE 5:30 POSITION, COMBUSTION/ TURBINE AREA TUBING IAW SOPM 20-60-04</P>)SDR UIEA2017020200144Sensor · malfunctionedLEFT ENGINE OIL TEMP FLUCTUATES IN FLIGHT, READ DOWN TO 32*C WHILE RT SIDE READS 80*C, THEN INDICATION WENT BLANK. T/S IAW FIM 79-34 FT 807. REMOVED AND REPLACED LEFT ENGINGE OIL TEMP SENSOR IAW AMM 79-34-01 OPS AND LEAK CK GOOD.SDR ASAA2017012519552Shim · wornNR 2 ENGINE ALL 24 FAN BLADE SHIMS WORN. ACFT GROUNDED. REMOVED AND REPLACED THE FAN BLADE SHIMS IAW T/C 78472002.SDR CALA2017012000144Pump · faultyR N1 3 PCT LESS THAN L N1 AT TAKEOFF PWR. ALL OTHER INDICATIONS IN NORMAL RANGE. OK INFLT PER INBOUND CREW, SHOULD READ LEFT ENGINE WAS 3% LOWER N1 THAN RIGHT ENGINE. REPLACED NR 1 ENG FUEL PUMP DUE TO FAILED PRESSURE TEST PER AMM 73-11-01-705-001-H00. PER AMMSDR UIEA2016121201000Blade · damagedTHE NR2 ENGINE HAS 14 FAN BLADES HAVE NICKS ON THE L/E OF BLADES . BLENDED THE FAN BLADES IAW AMM 72-31-02-308-045-H00.SDR UIEA2016121200999Blade · damagedNR 1 ENGINE LP COMPRESSOR BLADES LEADING EDGES HAVE NICKS. BLENDED THE COMPRESSOR BLADES IAW AMM 72-31-02-308-045-400, & 70-11-06-232-001-1400.SDR P5CA2016120200303Line · leakingEICAS MESSAGE NR 3 ENG OIL PRESSURE, QUANTITY READ ZERO. INSPECTED AND FOUND THAT OIL LEAK FROM THE NR 3 ENG MAIN FUEL PUMP DRAIN LINE. SERVICED THE OIL SYS AND CAPPED MAIN FUEL PUMP DRAIN LINE THEN NO OIL LEAK NOTED AND OIL QTY NORMAL AFTER ENG RUN CHECK IASDR FDEA201607192527Feeder Cable · damagedAFT FUSELAGE COMPARTMENT AT BS 2033, DURING DEFECT RECTIFICATION, FOUND ONE FEEDER CABLE FOR ENGINE NR 2 WITH DEEP CUT AND ON EWIRING CLAMP WITH SIGN OF ARCING.SDR UIEA2016060300400Warning Light · illuminatedRIGHT ENGINE VALVE LIGHT DID NOT CYCLE DURING START.SDR IPXA2016051003155Skin · dentedINSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT, FOUND DENTED SKIN, NR 1 ENGINE EXHAUST SLEEVE BETWEEN NAC BS 333.5 AND BS 336 ,6 O'CLOCK LOCATION HAS DENT REF EGAT NRC FBU05050 EVALUATED DAMAGE IAW SRM 54-45-30-1A-1,DETAIL VII, REV 65.00.SDR IPXA2016050302881Skin · delaminatedRIGHT ENGINE COWL INBD SIDE LARGE ARE DELAMINATED 2 FOOT X 4 FOOT. DEFERRED CHIPPING AND MISSING PAINT ON NR 2 ENGINE INBD FAN COWL NO DELAMINATION FOUND IAW AMM 51-21-10-07. R & R RT ENG INBD FAN COWL IAW AMM 71-11-04/401.SDR 9WGA4352016042601Engine · leakingSMOKE IN UPPER CARGO COMPARTMENT AND COURIER COMPARTMENT, UNABLE TO GET RID OF IT, TO THE POINT IT WAS IRRITATING TO THROAT. CLOSE TO WEAR OXYGEN MASK. SUSPECT NR 3 ENGINE OIL LEAKING INTO BLEED AIR SYS.SDR AALA20160405022Filter · contaminatedAIRCRAFT WAS GNDED. AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED LT FUEL FILTER EICAS MSG. FOUND LT ENG FUEL FILTER CONTAMINATED. R & R FILTER IAW AMM 73-11-02. ACCOMPLISHED TAKEOFF POWER ENG RUN WITH NO FURTHESDR FDEA201512103970Hmu · malfunctionedCRUISE FLIGHT AT FL 350L, ENG NR 2 N 1, EGT & FUEL FLOW BECAME UNSTABLE, CONTINUOUSLY FLUCTUATING. ENG STABILIZED ONCE ON DESCENT BEGAN & WAS NORMAL THROUGH LANDING & TAXI. REPLACED HMU & FUEL PUMP.SDR IPXA2015110995622Heat Exchanger · damagedATB, EMERGENCY DECLARED, NR 2 ENGINE LOW OIL PRESSURE. CREW SHUTDOWN ENGINE AND RETURNED TO DEPARTURE UNEVENTFULLY. R & R NR 2 ENGINE FUEL/OIL HEAT EXCHANGER IAW AMM 79-21-02.SDR P5CA2015110900173Oil System · lowLOW OIL QUANTITY IN CRUISE. GOT DOWN TO 2 QTS INDICATED. INSPECTED NR 1 ENGINE IAW AMM 72-00-00 AND FOUND LEAKAGE FROM B-SUMP SCAVANGE DRAIN TUBE. R & R NR 1 ENGINE IAW BOOTSTRAP METHOD IAW W/C E2023.SDR IPXA2015100794502Line · rupturedDURING CLIMB, LEFT ENGINE FAILED. AIR RETURN. R & R RUPTURED FUEL LINE.SDR UIEA2015060400295A/C Pack · stiffLEFT THROTTLE EXTERIOR STIFF TO ADVANCE, RATCHETS WHEN THRUST LEVER ADVANCES. COMPLIED WITH FIM 76-11 FAULT TREE 805. THROTTLE LEVER FORCE IS 5 LBS, AUTO THROTTLE TEST 10 OK.SDR UIEA2015031800183Connector · dirtyDURING DESCENT ENG 1 BECAME UNRESPONSIVE TO THROTTLE MOVEMENT. EGT WAS 659 DEGREES & CLIMBING WITH THROTTLE AT IDLE. PRECAUTIONARY SHUTDOWN ACCOMPLISHED, NO CMC MSG FOUND 1. PERFORMED VISUAL CHECK ENG INTAKE, TAIL PIPE & MAG CHIP DETECTOR, METAL NOT FOUND ISDR UIEA2015021600123Unknown · smokeWHEN POWER WAS RETARDED FOR DESCENT SMOKE & FUMES ENTERED COCKPIT. STRONG TURBINE OIL SMELL. REF EO 1972556 PART 1 ACCOMPLISHED. OIL CONSUMPTION VERIFICATION & ENG BLEED DEACTIVATION.SDR IPXA2015013085502Connector · failedNR 2 ENGINE OIL PRESSURE INDICATION INOPERATIVE, ALL OTHER INDICATIONS NORMAL . AIR TURN BACK. R & R OIL TRANSMITTER CONNECTOR SWPM 20-10-13 PARA 13.SDR ABXA20150115011Rib · crackedNUMBER 2 INBD CORE COWL NR 3 RIB FROM AFT CRACKED. REMOVED NR 3 RIB & LOWER DOUBLER. WELDED RIB IAW PSM 900-7-2-1 NR 1 REV 50. REINSTALLED IAW SRM 51-40-02. SDR INFO, CRACKED LENGTH 2.5 INCHES, PN 314T1210-17, SN NSN, PART NAME RIB. ACFT WAS GNDED.SDR AALA20141224011Pressure Switch · inoperativeLEFT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. RETURNED TO DEPARTURE, EMERGENCY DECLARED AND LANDED UNEVENTFULLY. REPLACED THE PRESSURE SWITCH.SDR FDEA201411243875Indicator · inoperativeON INITIAL CLIMB OUT, NR 2 ENG OIL PRESS GAUGE DROPPED FROM NORMAL READING IMMEDIATELY TO ZERO PSI, ON RT ECAM, ADVISORY FLASHED & THE ENG PAGE INDICATED ZERO PSI FOR THE NR 2 ENG. THROTTLE NR 2 POSITIONED TO IDLE QRH COMPLIED WITH. TOTAL TIME OF ZERO OIL PSDR FDEA201410042970Duct · damagedDURING TAKEOFF AFTER 90 KNOT CALL RECEIVED ENGINE FAIL LIGHT. NR 3 ENGINE N1 WAS ERRATIC, NO VIBRATION. PERFORMED RTO BLOWN REVERSER DUCTS DAMAGED N1 SENSOR HARNESS. R & R Y-CHECK VALVE,PRSOV & DAMAGED TUBING AND ATTACHING HARDWARE IAW AMM 78-31-07-4 OPS C
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