GE CF6-80C2B6F
Service difficulty reports · 1,456
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 = 'CF680C2B6F' 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 = 'CF680C2B6F' 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 CA040225012Actuator · stuck(CAN) EICAS MESAGE AILERON LOCKOUT, FOUND RT AILERON LOCK OUT ACTUATOR STUCK IN THE EXTEND POSITION, ACTUATOR REPLACED.SDR CA040216001Odor · detected(CAN) THE FLIGHT EXPERIENCED AN ACRID ODOR IN THE COCKPIT. AC DECLARED AN EMERGENCY LANDING AND CARRIED OUT THE QRH. AC SENT TO HANGAR FOR INVESTIGATION.SDR CA040122005Wire · chafed(CAN) FAULT: LT ENGINE HYD. ALT. CURRENT MOTOR DRIVEN PUMP (ACMP)POWER FEEDER WIRES FOUND CHAFFING AND ARCHING ON STRUT STRUCTURE. STRUC. DAMAGE WAS ALSO NOTED DUE TO ARCHING.SDR CA040120005Engine · flamed out(CAN) ON TAXI OUT LT ENGINE FLAMED OUT, WITH OIL ODOR IN THE CABIN. RETURNED TO GATE, AIRCRAFT CHANGED, ENGINE REPLACED IAW 71-00-02 CONF.SDR DL76K031125Engine · making metalON CLIMBOUT 22,000 LEFT ENGINE COMPRESSOR STALL APPROX 5-6 TIMES. MOMENTARY FUEL ODOR IN CABIN. BOROSCOPE INSPECTION NR 1 ENGINE HPC, COMBUSTION CHAMBER, AND HPT NO DAMAGE FOUND, WENT FOR ENGINE RUN UNABLE TO COMPLETE DUE EGT IDLE 800 DEG. AFTER RUN FOUND MSDR CA031028001Rod End · unsafetied(CAN) RT ELEVATOR LOST MOTION DEVICE TO ELEVATOR CONTROL ROD END AT LOST MOTION DEVICE NOT IN SAFETY. ROUTINE INSPECTION DURING A M01 CHECK FOUND THE ROD END WAS NOT IN SAFETY. LOCKWIRE COULD BE INSERTED THROUGH THE INSPECTION HOLE. THE WITNESS SEAL FROM THE SDR P5CA0300974Engine · shutdownNR 3 ENGINE SHUTDOWN DUE TO NO OIL QTY - FL 350 OIL PRESSURE 45. DURATION OF SHUTDOWN - 45 MINUTES. REMOVED AND REPLACED NR 3 ENGINE PER MM 71-00-00 AND ATLAS MX JOB CARD A71710GTI. ENGINE OPS CHECK GOOD PER MM 71-00-00.SDR CA031027002Panel · missing(CAN) RT HORIZONTAL STABILIZER LOWER TRAILING EDGE ACCESS PANELS AFT SUPPORT BEAMS MISSING 7 HORIZONTAL ATTACH BOLTS BASED ON THE CONDITION OF THE AREA IN WHICH THE DISCREPANCIES WERE FOUND AND THEFACT THAT THE ACFT WAS ON A M01 CHECK INDICATES THAT THE ACFT WSDR CA030919003Control Panel · malfunctioned(CAN) A/C HAD A DUAL ATC FAILURE AFTER DEPARTURE LHR. UK ATC WOULD NOT LET THE A/C PROCEED SO RETURNED TO LHR. OVERWEIGHT LANDING CHECK CARRIED OUT. ATC CONTROL PANEL CHANGED AND NO FURTHER FAULTSDR DL76G030581Engine · failedON TAKEOFF ROLL, ABORTED AT 100 KTS DUE TO NR 2 ENG FAILURE. FLAMES REPORTED COMING FROM THE FRONT AND REAR OF THE ENG. ENG EXPERIENCED A COMPRESSOR STALL. ENGINE CHANGE IN WORK IN BOM.SDR CA030528013Slide · deployed(CAN) LT O/H WING CHUTE WAS ACCIDENTALLY DEPLOYED BY FLT OPS DURING A TRAINING SESSION. THE CHUTE DID NOT DEPLOY COMPLETELY. THE LOWER SECTION OF THE CHUTE WAS PREVENTED FROM COMPLETE DEPLOYMENT BY THE IB SIDE. CONFIRMED, OPERATOR NEVER CHANGED OR REMOVED THISDR UPS03640696Compressor · vibrationAT FL 330 RT ENG COMPRESSOR STALLED. 1ST STALL RT ENG VIB WAS 3.2 / 2ND VIB WAS 5.0. ENG THRUST WAS RETARDED TO IDLE. ON SHUTDOWN ENG READINGS WERE N1L 28.3 R28.7 EGTL 411 R480 N2L 69.0 R 72.0 FFL 1.3 R1. 5. R/R NR 2 ENG PER TC 6002 AND TC 6001. NO DEFECTS NSDR CA030304003Cooling Fan · failed(CAN) SMOKE IN COCKPIT . STOPPED AFTER 20 SECS. AFTER LANDING IN ANC STATUS MSG. 'FWD EQ EXH FAN' AND C/B H21 LWR EQUIP PANEL 'FWD EXH EQUIP COOL FAN ' TRIPPED.FWD EQUIPMENT COOLING FAN REPLACED AS PER AMMSDR CA030313005Fan · failed(CAN) SMOKE IN COCKPIT, DISSAPATED AFTER LANDING WITH A STATUS MESSAGE 'FWD EQ EXH FAN' AND FOUND C/B H21 LWR EQUIPEMENT PANEL 'FWD EXH EQUIP COOL FAN' POPPEDSDR CA030226001Compressor · stalled(CAN) REJECTED TAKE OFF AFTER COMPRESSOR STALL ON THE LT ENGINE AND RISE IN TEMP AT 155 KNOTS, ALL 8 TIRES WENT FLAT (FUSES BLOWED OUT).SDR CA030205004Windshield · cracked(CAN) ON CLIMB OUT OF YVR, RT WINSHIELD SHATTERED. ACFT CONTINUED TO YUL.SDR CA030115001Alternator · broken(CAN) ORIGINAL WRITE UP STATED, LT ENGINE OIL QUANTITY SLOWLY DROPPED TO ZERO DURING CRUISE. OIL TEMP STEADY AT 3 DEGREES ABOVE RT ENGINE. OIL PRESSURE FLUCTUATED AT 2-10 PSI BELOW RT ENGINE. LT ENGINE EICAS MESSAGE SHOWING. AIRCRAFT PROCEEDED TO YVR WITH LT ESDR DL76K021444Shutoff Valve · failedON START ATTEMPT NR 1 ENGINE, NO LIGHT OFF. OBSERVED ENGINE VALVE LIGHT REMAINED ILLUM AFTER SELECTING FUEL CONTROL SWITCH TO RUN. REPLACED FUEL SHUTOFF SOLENOID VALVE ASSY PER M/M.SDR DL76G021429Idg · failedON CLIMBOUT, RT GEN OFF LOST RT AC BUSS. BUSS RESET. RT GEN WOULD NOT RESET. FELT VIBRATION AT 310 KTS. FOUND -C- PHASE OPEN ON IDG. REPLACED IDG. OPS CK OK ON RUN-UP. REF VIBRATION, VISUAL INSP OF EXTERIOR OF A/C NO DEFECTS NOTED. PERFORMED FLT CONTROSDR DL76K021408Panel · damaged_ON TAKE OFF FROM LGA A/C BEHIND FLT 471 NOTICED PANEL DEPA RTING A/C. PART RETREIVED WAS FOUND TO BE ACOUSTICAL PANEL FROM FAN EXIT CASE. A/C DIVERTED TO JFK DUE TO ENGINE VIBRATION REPLACED PANEL AND BSDR DL76K021114Engine · shutdownSHORTLY AFTER T/O CREW NOTICED A LOUD THUD AND LT ENG SHUT ITSELF DOWN. FLAMES WERE REPORTED COMING FROM ENG ON T/O BY GROUND PERSONNEL. A/C RTN ATL. REPLACED ENGINE.SDR CA020916009Coffeemaker · failed(CAN) ON DECENT CREW REPORTED SMOKE IN AFT GALLEY AND LOUD POPPING SOUND, GALLEY COVERED IN WHITE DUST. NOTIFIED ATC/MAINT/DISPATCH. MTCE SUSPECTED COFFEEMAKER HOT WATER BLEW PLUG, AIRCRAFT LEFT WITH UTILITY BUSES OFF/REAR GALLEY CB'S PULLED. AREA INSPECTEDSDR CA020830011Light · miswired(CAN) SECOND OBSERVERS UTILITY LIGHT FOUND MISWIRED AT TERMINAL BLOCK. THIS FINDING WAS RESULT OF A CAMPAIGN TO CHECK FOR SIMILAR PROBLEM ON 767 FLEET. LIGHT SOCKET PRODUCES SPARKS IF INADVERTENTLY TOUCHED BY A GROUNDING OBJECT. TERMINAL BLOCK REWIRED CORRSDR DL76G021003Engine · failedLEFT ENGINE SURGED. REPLACED #1 ENGINE. SDR CA020828003Control Unit · failed(CAN) CABIN CREW REPORTED 'PASSENGER READING LIGHT NOT WORKING IN Y CLASS.' THE 1ST OBSERVATION BY MAINT NOTED THAT IN CENTER SECTION OF AFT CABIN, ROWS 19DEF TO 36DEF, CALL LIGHT ILLUMINATED AT SEAT 36DEF, 26DEF & APPROXAMITELY ROW 20 OR 21DEF. CALL LIGSDR CA020826004Control Unit · failed(CAN) AIRCRAFT REQUIRES LARGE AMOUNTS OF RIGHT RUDDER TRIM IN ORDER TO FLY STRAIGHT 250 KTS RANGE REQUIRES 2.5 UNITS OF RT RUDDER TRIM. 300 - 325 KTS REQUIRES 3.5 UNITS.BOTH LT INBD AILERON PCUS REPLACED AND RIGGED AS PER AMM 27-11-48SDR CA020826003Cooling Fan · failed(CAN) INTERMITTENT LOUD SQUEEL IN FRONT CABIN AND GALLEY WAS FOLLOWED BY MOMENTARY SMOKE IN FLIGHT DECK AND FWD EQUIPMENT BAY FAN STATUS MESSAGE WITH ASSOCIATED CB POPPING.FORWARD EQUIPMENT COOLING FAN REPLACED AS PER AMM.SDR CA020801008Bolt · sheared(CAN) AT TRIP CHECK DAMAGE FOUND TO LT WING TO FLAP FAIRING, MLG SHOCK STRUT DOOR, AND JURY STRUT DOOR. INVESTIGATION FOUND SHOCK STRUT DOOR MID ATTACH BOLD HAD SHEARED ALLOWING SEPERATION OF DOOR FROM STRUT. NEW FAIRING PANEL FABRICATED, JURY STRUT DOOR TSDR CA020801003Actuator · failed(CAN) RT AILERON LOCKED OUT DURING FLIGHT AFTER LEAVING YVR. RT LOCK OUT ACTUATOR REPLACED PER AMM 27-11-44 PG 1-12 OPERATION CHECKED SERVICEABLESDR CA020801001Actuator · binding(CAN) SPOILER LEVER FEELS TO HAVE MORE TENSION (BINDING) WHEN DEPLOYING AND RETRACTING. REPLACED SPEEDBRAKE MECHANISM AND TESTED PER AMM 27-62-04-002-114SDR CA020530012Stator · destroyed(CAN) AFTER LANDING BRAKE TEMP LIGHT ON RIGHT FOREWARD INNER MAIN. TEMP WENT TO 9 WITH AUTOBRAKE SETTING AT 2 FOR LANDING. NR 3 MAIN WHEEL AND BRAKE REMOVED. BRAKE INNER STATOR DISINTEGRATED AND CAUSED JAMMING OF BRAKE. TIRE DEFLATED DUE FUSE PLUG OVERHEAT. SDR CA020528006Projector · inoperative(CAN) NO PROJECTOR IN CABIN B WORKED FOR SAFTY DEMO. (L1075533) ELECTRICAL CONNECTOR REMOVED FROM PROJECTOR PRIOR TO TAKEOFF AND FLIGHT CONTINUED WITH SYSTEM DEACTIVATED. FINAL FIX WAS NEW PROJECTOR INSTALLED AND SYSTEM CHECKED SERVICEABLE.SDR CA020509003Valve · leaking(CAN) DURING A M01 CHECK THE LEFT AND RIGHT HYDRAULIC SYSTEM EMPENNAGE FLIGHT CONTROL SHUTOFF VALVES WERE FOUND LEAKING.AFTER INVEASTIGATION , ONE OF THE L/H BOLT WAS SHEARED WHILE OTHERS WERE ENGAGED ONLY WITH A COUPLE OF THREADS. SIMILAR FINDINGS WERE FOUND SDR UPS02637961Linkage · brokenINSPECTION TYPE:ETOP COMPRESSOR STALL ON T/O AFTER V1. ALL ENGINE INDICATIONS NORMAL UNTIL IDLE POWER DESCENT. THEN NUMBER 2 ENGINE VIBRATION SHOWED 4.4 - 4.8 UNITS. FOUND 5TH STAGE VSV LEVER ARM BROKEN OFF AT APPROX 7 O'CLOCK POSITION. REMOVED AND REPLACESDR CA020502013Thrust Reverser · contaminated(CAN) BOTH REVERSERS ONLY DEPLOYED AT MID TRAVEL ON LANDING.FOUND MOISTURE TRAP IN THE THRUST REVERSERS CDU (CONTROL AND DRIVE UNIT). REMOVED ALL MOISTURE, FUNCTIONAL TEST CARRIED OUT, AIRCRAFT FOUND SERVICEABLE.SDR CA020502011Actuator · leaking(CAN) CENTRE SYSTEM HYDRAULIC QUANTITY MESSAGE ON EICAS ON TOP OF DESCENT. QUANTITY CONTINUED TO DROP SLOWLY DURING DESCENT AND FLAP/GEAR EXTENSION FOUND TO BE A LEAK FROM THE INBOARD RT ELEVATOR POWER CONTROL ACTUATOR (PCA). REPLACED ACTUATOR.SDR CA020502012Control Unit · failed(CAN) FLAP DISAGREE MESSAGE ON EICAS WHEN FLAP SELECTED TO RETRACT FROM 5 DEGREE TO 1 DEGREE ON TAKEOFF. ALTERNATE TE FLAP EXTENSION USED FOR LANDING. FOUND TO BE THE FSEU AT FAULT (FLAP SLAT CONTROL UNIT). REPLACED ELECT FLAP SLAT UNIT.SDR CA020328004Outflow Valve · failed(CAN) AFTER TAKEOFF, EICAS MESSAGE "CABIN ALT AUTO 1 APPEARED. AIRCRAFT DIVERTED TO LONDON (HEATHROW) LHR FOR FIX. OUTFLOW VALVE AND ACTUATOR REPLACED AS PER AMM 21-31-02. SYSTEM CHECKED SERVICEABLE.OUTFLOW VALVE -606832-21 ACTUATOR -2022480-6SDR CA020124006Filter · failed(CAN) FLIGHT CREW REPORT THAT THEY HAD A FUEL FILTER LIGHT ON EICAS FOR BOTH ENGINES. FOUND TO BE FINE MANUFACTURING DEBRIS (NEW AIRCRAFT). REPLACED TWO FILTERS AND DRAIN ALL RESERVOIRS, GROUND RUN AND LEAK CHECK CARRIED OUT. FLEET MANAGEMENT REQUEST TO HAVE BSDR CA020110001Engine · failed(CAN) ON TAKEOFF ROLL, AFTER N1 SELECTED ON MCP, ENGINE ACCELERATE NORMALLY TO 50 PERCENT AT 50 PERCENT ENGINE DID NOT ACCELERATE ANY FURTHER. ALL PARAMATERS NORMAL FOR BOTH ENGINES. AN AIRFRAME VIBRATION COULD BE FELT AT 25 - 50 PERCENT ON LT ENGINE. TASDR CA020104011Duct · damaged(CAN) LT ENGINE FIRE INDICATION AT 11,000 FEET IN CLIMB. ENGINE SHUT DOWN. FIRE BOTTLES DISCHARGED. AIRCRAFT RETURNED TO SYDNEY. FOUND ENGINE PNEUMATIC DUCTING RUPTURED AND ALSO HARNESS DAMAGED. HARNESS TEMPORARY REPAIRED AS PER PRODUCTION PERMIT 6-77-20/SDR CA011121017Control Handle · failed(CAN) ON APPROACH TO ST-JOHN, NF, WHEN SELECTED FLAP TO 5 DEGREES, FLAP DISAGREE EICAS MSG. CHECKLIST COMPLETED. EMERGENCY CALLED OUT. FLAP LEVER RVDT AND OUTBOARD SLAT PDU RVDT RE-ADJUSTED. FSEU RESETED AND FLAPS OPERATED SEVERAL TIMES. SYSTEM SERVICEABLE.SDR CA011114004Motor · failed(CAN) AFTER TAKEOFF AT 14,000 FT. LOSS OF BOTH AUTO CABIN PRESSURE CONTROL SYSTEMS. AIRCRAFT RETURNED TO ZURICH. AC MOTOR 2 REPLACED AS PER AMM 21-31-03 AND CHECKED SERVICEABLE.SDR CA010906008Controller · failed(CAN) SMELL AND SMOKE COMING OUT NR 2 GALLEY OVEN. OVEN CONTROLLER REPLACED. OPERATION CHECKED FOR ONE HOUR. NO SIGN OF VERHEATING, CONSIDER SERVICEABLE.SDR CA010905008Sleeve · shorted(CAN) A/C 381 M FOUND DURING UNRELATED ROUTINE MAINT IN AREA. EVIDENCE OF FIRE DAMAGE CAUSED BY SHORTED LEAD AT WASTER TANK DUMP VALVE HEATER SLEEVE. FIRE TRACK WAS FOLLOWED FROM SOURCE FWD THROUGH LIGHTNING HOLE OF ADJACENT STRUCTURE, & UPWARD ALONG FRAME TO SDR CA010622010Generator · failed(CAN) F/O'S FMC FAILED, F/O'S ADI & HSI FLICKERED CONTINIOUSLY. AUTO THROTTLE DROPPED OFF. SINGLE FMC MESSAGE & RESYNCHING OTHER FMC MESSAGE ALL COME ON. WHEN THE RIGHT GENERATOR BREAKER WAS OPENED & THE APU GENERATOR WAS PUT ON LINE, ALL SYSTEMS OPERATE NORMASDR CA010626038Acm · seized(CAN) DURING TAKEOFF, THE COCKPIT/CABIN FILLED WITH SMOKE. AIR CONDITIONING SUSPECTED. AIRCRAFT RETURNED. DEFFERRED AS PER MEL 21-51-07. RIGHT HAND ACM FOUND SEIZED.SDR DL76G010716Line · crackedENG OIL QTY IND ZERO, TEMP/PRESSURE IND NORMAL. QTY IND ZERO FROM EICAS COMPUTER AUTO AND RIGHT. ON LANDING OIL PRESS WENT INTO YELLOW WHEN REVERSE WAS APPLIED. SERVICED ENG OIL TO TOP (21 QTS) SPUN ENG. FOUND LINE CRACKED. LINE SCAVENGE LINE FROM ANGLE GSDR DL76G010585Eec · malfunctionedON DESCENT OUT OF 10,000 FEET, THE CREW NOTICED THE RT ENGINE ROLLING BACK AND FLAMED OUT. CREW WAS ABLE TO RESTART THE ENGINE SUCCESSFULLY. NO WATER IN FUEL SUMPS. RAN ENG AND VERIFIED CONT AND ENGINE PARAMETERS NML EEC REPLACED. CHECKED WIRING AND POWER SDR DL76G010480Controller · failedIR - L ENG BLEED OFF LIGHT CAME ON AFTER T.O. AT 2000FT. L DUCT PRESS <10 PSI. SYSTEM RECOVERED A FEW MIN LATER ONLY TO PRESENT AGAIN AT TOP OF CLIMB. L REV DID NOT OPEN ON LNDG. NO L ANTI-ICE. NO LT ENG BLEED FAULTS ON BITE MODULE. USING PNEUMATIC TEST EQ
Back to GE CF6-80C2B6F