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 P5CA2018110500341Warning Message · false activationLEFT ENGINE EEC C1 STATUS MESSAGE. PERFORMED A PIMU BITE IAW FIM 71-01-00/101. BITE TESTED GOOD. MESSAGE CLEARED.SDR UIEA2018110102472Sensor · malfunctionedLEFT ENGINE BLEED EICAS, DURING FLT. QRH COMPLETED. REMOVED AND REPLACED PRV EXIT PRESSURE SENSOR. OPS CHECKED GOOD, ACFT OK FOR SERVICE IAW AMM 36-21-08. PERFORMED POWER ASSURANCE TEST IAW 71-00-00-735-394-H03. ALL INDICATIONS SATISFACTORY AND NO FAULTS NSDR P5CA2018103000337Magnetic Seal · malfunctionedCAPPED # 2 ENGINE DRAIN LINES STARTER, IDG,FUEL PUMP,HMU AND HYDRAULIC PUMP AS PER AMM 71-71-00 & ECM 2018P-704 FOR 10 FC ( ACTUAL FC 20490 ) ( DUE TO HIGH OIL CONSUMPTION )(<P>TRANSFER TO NON MEL MDDR 101809 FOR AMM 71-71-00 FOR 10 FC</P><P><BR DATA-MCE-BOGUSDR UIEA2018102602360Engine · vibrationLT ENG VIB PEAKED 4.6 ON TAKEOFF. MAINTAINED 2.0-2.6 IN CRUISE. EVENT RECORD PRESSED ON CLIMBOUT. PERFORMED FAV TRIM BALANCE ON LEFT ENGINE IAW AMM 72-31-00. AFTER WEIGHT CONNECTION FOUND TO BE WITHIN OPERATIONAL LIMITS AT THIS TIME.SDR P5CA2018092650298Engine · abnormal#1 ENGINE TRIM BALANCE REQUIRED.(<DIV>PERFORMED #1 ENGINE TRIM BALANCE IAW 72-31-00-705-119. PER MCC GLEN ITEM IS NOT RII.</DIV>)SDR P5CA2018091100282Packing · damagedFOUND NR 1 ENG A-SUMP OIL LEAK. IAW AMM 72-31-03-004-001 & 72-31-03-404-005 REV 125 REPLACED PACKING. IAW 71-00-00-795-034 REV 125 PERFORM IDLE LEAK CHK RESULT. NO LEAK FOUND 3. COMPLETED THIS JOB AND CONDITION CHECK NORMAL.SDR P5CA2018091100221Acoustic Liner · brokenBROKEN MID ACOUSTIC LINER NR 2 ENG FAN CASE NEAR 12 O'CLOCK. IAW AMM 72-33-01-004-001 AND AMM 72-33-01-404-011 REV 125 REPLACED NR 2 ENG MID ACOUSTIC LINER.SDR P5CA2018091100220Acoustic Liner · brokenNR 2 ENG FAN CASE FWD ACOUSTIC LINER PLASTIC COVER BROKEN. IAW AMM 72-33-01-004-001 REV 125 RMV ACOUSTIC LINER. RBF J/C ATTACHING SHEET 0137454 REPAIR ACOUSTIC LINER. IAW AMM 72-33-01-404-011 REV 125 INSTALL ACOUSTIC LINER.SDR P5CA2018091100219Packing · damagedSEEPING OIL NO 1 ENG AND LOWER SIDE AT FWD HORIZONTAL DRIVE SHAFT HOUISING OIL SEEPING. IAW AMM 80-11-02-002-001 AND 80-1-02-402-009 AND 72-63-02-0040995 AND 72-63-02-404-016 AND 80-11-01-004-001 AND 80-11--01-404-012 REV 125 REPLACED PACKING. IAW AMM 71-00-00SDR IPXA2018082033021Manifold · brokenNUMBER 2 ENGINE, FROM APPROXIMATELY 5 - 6 O'CLOCK POSITIONS, TCC MANIFOLD WAS BROKEN, TWO 1/2 INCH DIAMETER TUBES HAVE SEPARATED FROM MAIN MANIFOLD. REPLACED TCC MANIFOLD IAW AMM 75-24-03-401.SDR UIEA2018082001752Extension · damagedLEFT ENGINE FAN ACUSTIC LINER SEGMENT MISSING. REMOVED AND REPLACED FLOW PATH EXTENSION POSITION 4 O' CLOCK AS PER AMM 72-33-00-308-104-H00.SDR HALA2018080100355Erosion Shield · looseLEFT ENGINE EXIT STATER VANE LEADING EDGE ERROSION FOIL LOOSE. SECURED THE EXIT VANE LEADING EDGE EROSION STRIP WITH SPEED TAPE IAW AMM 72-33-02-206-000-N00 TABLE 602.SDR 2LCF201807174002Coupler · failedDURING THE CRUISE PHASE ON THE MIA - AMS ROUTE, THERE WERE FAULTS IN THE TRANSMISSION AND RECEPTION BY THE HF SYSTEM. THE CREW DECIDED TO RETURNED THE AIRCRAFT TO MIA STATION. AFTER THAT THE WIRING WAS CHECKED AND THE LT AND RT COUPLERS OF THE HF ANTENNAS WERESDR 2LCF2019F00026Relay · failedDURING THE CLIMB PHASE OF THE MIA - SCL ROUTE, THE CREW WAS PRESENTED WITH SEVERAL EICAS MESSAGES THAT FORCED THE CREW TO DECLARE EMERGENCY AND RETURN TO MIA. THE MESSAGES THAT APPEARED WERE "AUTOPILOT, AUTO THROTTLE, YAW DAMPER, FMC, LT REV INSULATION VALVE".SDR 2LCF20180711001Relay · failedDURING THE CLIMB PHASE OF THE MIA - SCL ROUTE, THE CREW WAS PRESENTED WITH SEVERAL EICAS MESSAGES THAT FORCED THE CREW TO DECLARE EMERGENCY AND RETURN TO MIA. THE MESSAGES THAT APPEARED WERE "AUTOPILOT, AUTO THROTTLE, YAW DAMPER, FMC, LT REV. INSULATION VALVE"SDR P5CA2018061280090Bleed Valve · malfunctionedAFTER ENGINE SHUTDOWN, THE RIGHT ENGINE BLEED DOES NOT SHUT OFF. OPS CHECKED THE ENGINE BLEED AND CYCLED THE PRSOV IAW AMM 36-11-09. VALVE OPERATED NORMALLY. OPS CHECKED GOOD.SDR UIEA2018060701052Warning Message · false activationRIGHT ENGINE CONTROL. IAW FIM 71-01-00, PERFORMED A RT ENG VBV FEED BACK RESISTANCE CHECK. CLEANED CONNECTORS, VBV ACTUATOR & HARNESS CHECKED GOOD. MESSAGE NOT SHOWN. PIMU CHANNELS A & B, NO FAULTS. PERFORMED AMM 71-00-00, TEST 12, ALT GROUND TEST. TESTEDSDR UIEA2018060801077Warning Message · illuminatedRIGHT ENGINE CONTROL. PERFORMED FIM 71-01-00, PERFORMED RT ENG VBV FEED BACK RESISTANCES CK. CLEANED CONECTORS, VBV ACT & HARNESS, CK GOOD. MSG NOT SHOW , PIMU CH A & B, NO FAULTS. PERFORMD AMM 71-00-00 TEST 12 ALT GROUND TEST, TEST GOOD, RAN RT ENG; IAWSDR P5CA20180601082Anti-Ice Valve · warning messageWHEN TURNING THE LT ENGINE ANTI-ICE SWITCH FROM ON TO AUTO, THE LT ENG ANTI-ICE EICAS MESSAGE ILLUMINATED. REPLACED THE ANTI-ICE VALVE. OPS CHECKED IAW AMM 30-21-03. OPS & LEAK CHECKED GOOD.SDR UIEA201805290975Blade · nickedDURING A PREFLIGHT INSPECTION, PILOT REPORTED A SMALL NICK ON THE LEDING EDGE SMALL NICK ON LEDING EDGE OF THE NR 8 FAN BLADE, ON THE LT ENGINE. PERFORMED AN INSPECTION IAW AMM 72-31-02-226-012-H00, AND FOUND TO BE WITHIN LIMITS, NO SHARPS EDGES OR CRACKS NOSDR UIEA201805290970Igniter · warning messageRIGHT ENGINE IGNITER NR 2 STATUS MESSAGE. REMOVED AND REPLACED THE NR 2 IGNITER IAW AMM 74-21-02. OPS CHECKED NORMAL.SDR UIEA201805220917Warning Message · false activationRIGHT ENGINE IGNITOR 2 STATUS MESSAGE. COMPLIED WITH TROUBLESHOOTING IAW FIM 71-01 TASK A33, NO DEFECTS NOTED. OK FOR SERVICE.SDR P5CA2018051800075Filter · warning messageRIGHT ENGINE FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED THE FUEL FILTER IAW AMM 73-11-03 . LEAK AND OPS CHECKED NORMAL.SDR IPXA2018052129809Compressor · damagedWHILE AIRBORNE, AT THE TOP OF DECENT, THE RIGHT ENGINE THRUST REDUCED TO IDLE POWER ABNORMALLY. AT IDLE THRUST, THE LEFT AND RIGHT ENGINES DIFFERED IN PARAMETERS SIGNIFICANTLY. THE RIGHT THROTTLE WAS UNRESPONSIVE FOR THE REMAINDER OF THE FLIGHT. STALL ISDR UIEA2018051400894Transmitter · failedNR 2 ENGINE LOW OIL PRESSURE LIGHT DOES NOT ILLUMINATE. R & R THE NR 2 ENGINE OIL PRESSURE TRANSMITTER IAW AMM 79-32-01. OPS CHECKED GOOD.SDR UIEA2018051200882Light · no indicationNR 2 ENGINE OIL PRESSURE LOW LIGHT DOES NOT ILLUMINATE. REMOVED AND REPLACED RT OIL PRESSURE LIGHT IAW AMM 33-13-00, OPS CHECKED GOOD.SDR UIEA2018050100816Filter · warning messageLEFT ENGINE FUEL FILTER EICAS MESSAGE FOR 5 MINUTES DURING CLIMB OUT. NO SECONDARY INDICATIONS, STATUS MESSAGE REMAINED. REMOVED AND REPLACED THE LT ENGINE FUEL FILTER ELEMENT IAW AMM 73-11-02, OPS & LEAK CHECKED GOOD.SDR UIEA201805010814Hmu · malfunctionedLEFT FUEL CONTROL, ENGINE VALVE INDICATION INOPERATIVE. REMOVED AND REPLACED THE LT ENGINE HMU IAW AMM 73-21-14. OPS & LEAK CHECKED OK.SDR UIEA2018042750798Warning Message · illuminatedEICAS IDLE DISAGREE.SDR UIEA2018042750801Filter · failedRIGHT FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED THE RIGHT ENGINE FUEL FILTER IAW AMM 73-11-02. LEAK CHECKED OK. STATUS MESSAGE NO LONGER PRESENT.SDR UIEA2018042500794Transmitter · leakingFOUND A LEAKING PRESSURE TRANSMITTER ON THE NR 2 ENGINE. DEACTIVATED THE PRESSURE TRANSMITTER IAW AMM 73-33-01. REMOVED AND REPLACED, AND REACTIVATED THE NR 2 ENGINE FUEL PUMP PRESSURE TRANSMITTER IAW AMM 73-33-01-402-033-H00. OPS & LEAK CHECKED GOOD.SDR HALA2018042400183Engine · malfunctionedDURING CRUISE FLIGHT, THE NR 2 ENGINE FUEL FLOW 400 LBS AN HOUR HIGHER, NR 2 ENGINE EGT 25 DEGREE'S C HIGHER THAN NR 1. RAN BOTH ENGINES FOR 5 MINUTES ON GROUND IAW AMM 71-00. RIGHT ENGINE WITHIN LIMITS AT THIS TIME, NOTIFIED MOC.SDR FDEA201804201072Cap · unsecureDURING CRUISE AT 340FL, NOTICED THE RIGHT ENG OIL PRESSURE AT 29 & DROPPING WHILE RT OIL QUANTITY WAS 2 & ALSO DROPPING. TEMP REMAINED NORMAL, DIVERTED. AT BLOCK-IN, RIGHT ENGINE OIL QTY WAS 2 QTS, SETTLED AFTER 5 MINUTES TO 14 QTS. FOUND OIL SERVICE CAP NOSDR UIEA2018041700717Circuit Card · malfunctionedAFTER ENGINE START RECEIVED AN EICAS MESSAGE FOR IDLE DISAGREE. REMOVED AND REPLACED THE M644 CARD IAW AMM 73-21-11. OPS CHECKED OK.SDR UIEA2018041800731Warning Message · false activationEICAS MESSAGE FOR THE LT ENGINE CONTROL, AFTER ENGINES START. ACCOMPLISHED EICAS ERASE PROCEDURE, FAULT ERASED. TROUBLESHOT IAW FIM 73-21 878, AND NO FAULTS LOGGED ON LP. INSPECTED THE LT ENG EEC FOR SECURITY, OK. ALSO VERIFIED TEST 11 OF AMM 71-00-00, SDR UIEA2018041600714Adc · malfunctionedAFTER LANDING, AN IDLE DISAGREE MESSAGE ILLUMINATED. THE RT ADC WAS REPLACED, NO DEFECT NOTED AFTER PERFORMED 30 TEST.SDR UIEA2018041300699Indication Sys · malfunctionedLEFT OIL TEMP INDICATION LOST. PERFORMED AN OPS TEST OF THE OIL TEMP INDICATION SYSTEM IAW IAW AMM 79-34-00. SYSTEM TESTED NORMAL.SDR UIEA2018040900646Anti-Ice Valve · slowRT ENGINE ANTI-ICE VALVE SLOW TO CYCLE. PERFORMED OPS CHECKED THE RT ENGINE ANTI-ICE VALVE, OPS CHECKED GOOD IAW AMM 30-21-03.SDR UIEA2018040800634Anti-Ice Valve · malfunctionedEICAS MESSAGE FOR THE ENGINE ANTI-ICE SYSTEM. PERFORMED OPS CHECK OF THE RT ENGINE ANTI-ICE VALVE, OPS CHECKED OK IAW AMM 30-21-03.SDR HALA0218040900148Warning Message · false activationLEFT ENGINE EEC STATUS APPEARED DURING DESCENT, PASSING FL180. NO CURRENT FAULT DISPLAYED. TROUBLESHOT IAW FIM 71-01, FAULT TREE 803. FAULT DID NOT RETURN. OK FOR SERVICE.SDR UIEA2018040700626Switch · inoperativeLEFT EEC NORMAL LIGHT INOPERATIVE. REPLACED THE SWITCH, OPS CHECKED GOOD.SDR UIEA2018040600620Warning Message · illuminatedIDLE DISAGREE DURING DEPARTURE.SDR UIEA2018040600617Warning Message · intermittentEICAS MESSAGE FOR THE LEFT ENGINE FUEL VALVE DURING ENGINE SHUTDOWN. PERFORMED FIM FAULT TREE 808 BLOCK 11. PERFORMED WET MOTOR FOR LEFT ENGINE IAW AMM 71-00-00-H01, NO EICAS ADVISORY MESSAGE AT THIS TIME, BLOCK 21 STATES THIS WAS AN INTERMITTENT FAULT, OPS CSDR UIEA2018040400532Blades · damagedRIGHT ENGINE SHOWED A FAN VIBRATION UP TO 5 DURING TAKEOFF. REMOVED AND REPLACED THE NR 2 ENGINE 5 AND 6 BLADES IAW AMM 72-31-02.SDR UIEA2018040400534Blade · damagedNR 2 ENGINE, ONE HPC STAGE 1 BLADE WITH A L/E DENT AND CRACK. BORO BLENDED REPAIR TO THE BLADE IAW AMM 72-00-00.SDR UIEA2018040400535Hmu · malfunctionedIDLE DISAGREE MESSAGE, AT FLT IDLE AFTER STOWING THE THRUST REVERSER. R & R THE HMU IAW AMM 73-21-14. OPS CHECKED NORMAL IAW AMM 71-00-00.SDR UIEA2018040400536Blades · damagedNR 2 ENGINE BLADES 5 AND 6 ARE DAMAGED. R & R THE BLADES. OPS CHECKED NORMAL IAW AMM 72-31-02.SDR UIEA2018040500616Blade · damagedDURING TAKEOFF, A 4.9 VIBRATION ON FAN. REMOVED AND REPLACED THE NR 3 FAN BLADE IAW AMM 72-31-02 , TRIMMED VIBRATION IAW AMM 72-31-00, TRIM NOW 1.0 AT TAKEOFF, FAN LUBE COMPLIED WITH.SDR UIEA2018033000490Exciter · inoperativeDURING FIRST ATTEMPT, THE LEFT ENGINE START HAD NO EGT RISE, SECOND ATTEMPT SUCCESSFUL. NR 2 IGNITION ON THE LT ENGINE WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE LT NR 2 IGNITION EXCITER IAW AMM 74-11-01 AND REMOVED AND REPLACED THE LT NR 2 IGNSDR UIEA2018040300522Sensor · intermittentDURING CRUISE FLIGHT, N1 INDICATION FLUCTUATED INTERMITTENTLY, FOR THE NR 1 ENGINE. REMOVED AND REPLACED THE NR 1 ENG N1 FAN SPEED SENSOR IAW AMM 77-12-01. OPS CHECKED NORMAL IAW AMM 71-00-00.
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