GE CF6-80C2B7F
Service difficulty reports · 405
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 = 'CF680C2B7F' 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 = 'CF680C2B7F' 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 UIEA2019042974054Engine · fluctuatesAFTER POWER WAS REDUCED TO IDLE FOR DESCENT, THE LEFT ENGINE WOULD FLUCTUATE FROM 45% TO 52% N1. N2 AND FUEL FLOW WOULD FLUCTUATE AS WELL.(<P>PERFORMED VISUAL INSPECTION OF ENG IAW AMM 71-00-00, NO DEFECTS NOTED @ THIS TIME. PERFORMED VISUAL INSP AT CONNECTORSSDR UIEA2019042203925Engine · vibrationLEFT ENGINE FAN VIBES REACHED 4.3 DURING CLIMB OUT.(<P>PERFORMED ENGINE RUN AND VIBE INDICATIONS NML PER AMM 71-00-00 PER FIM 71-05 FT 805. NOTE: VIB LEVELS CAN SUDDENLY SPIKE AT TRANSIENT LEVELS OF ENGINE SPEEDS.</P>)SDR UIEA2019042203926Strut · seizedFWD R/H COWLING FAN STRUT SEIZED ENG #2.(<P>REMOVED AND REPLACED FWD RH FAN COWLING STRUT PER AMM 71-11-11 CHECK NORMAL.</P>)SDR UIEA2019042203924Warning Message · false activation15 MIN PRIOR TO DESCENT, FL400, L ENG EEC MODE R ENG EEC MODE CAUTION MSG. CONTINUED FLIGHT IN ALTN MODE.(<P>PERFORMED IDLE RUN #1 AND #2 ENG EEC. OPS CHECK GOOD IAW AMM 71-00-00.</P>)SDR UIEA2019041503879Blade · nickedNR 2 ENG HAS 1 EACH FAN BLADE WITH A SMALL NICK ON L/E 3/4 OF AN INCH FROM BLADE TIP. BLENDED #2 ENG #37 FAN BLADE IAW B767 AMM 72-31-02. FOUND TO BE WITHIN LIMITS IAW B767 AMM 72-31-02.SDR UIEA2019040803825Gasket · failedDURING LEAK CHECK OF HMU FOUND FUEL METER LEAKING FUEL AT GASKET SPLIT LINE.(<P>REMOVED AND PERFORMED FUEL AND HEAT EXCHANGER GASKET AS PER AMM CH 79-21-01. LEAK CHECK GOOD. PERFORMED ENGINE #2 TEST IDLE RUN AS PER AMM 71-00-00 .CHECKS NORMAL, REF ITEM LOG PG SDR UIEA2019040863816Shutoff Valve · failedAFTER START OF RIGHT ENGINE. THE RIGHT ENGINE FAILED ( SLOWLY ROLLED BACK) THE EICAS MESSAGE RIGHT ENGINE FUEL VALVE WAS OBSERVED AND THE ENGINE VALVE LIGHT FLICKERED (<P>REMOVED AND REPLACED RIGHT FUEL CUTOFF SOLENOID VALVE IAW AMM REF 73-21-20. NO HELP. SEE SDR UIEA2019030503478Blade · nickedENGINE NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES HAVE NICKS ON THE LEADING EDGES.(<P>BLENDED OUT ENG NR 1 SEVERAL FIRST STAGE FAN ROTOR BLADES LEADING EDGES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION ON THE BLENDED AREAS.SDR UIEA2019030503477Igniter · damagedENGINE NR 1 BOTH IGNITER PLUGS ARE DAMAGED.(<P>REMOVED AND REPLACED NR 1 ENGINE IGNITER PLUGS IAW AMM 74-21-02. OPS CHECK NORMAL</P>)SDR UIEA2019030503475Igniter · damagedENG NR 2 BOTH IGNITER PLUGS ARE DAMAGED.(<P>REMOVED AND INSTALLED ENGINE NR 2 BOTH IGNITERS IAW AMM 74-21-02. OPS CHECK NORMAL.</P>)SDR UIEA2019030503474Blade · nickedNR 2 ENGINE HAS FAN BLADE WITH NICK BLADE MARKED.(<P>LOCATED AND BLENDED OUT NR 2 ENGINE FAN BLADE MARKED PER AMM 72-31-02-308-055-1-00.</P>)SDR UIEA2019022503378Blade · nickedNR 2 ENGINE LP COMPRESSOR ROTOR BLADE NR 20 HAS A NICK AT L/E CONTOUR. BLENDED THE NICK AND RAISED MATERIAL ON THE NR 2 FAN BLADE 20, MATERIAL LOSS AFTER REPAIR .028,MAX ALLOW .060, VERFIED CONDITION OF BLADE VIA NDT, BLADE FOUND TO BE SERVICEABLE, NO FURSDR UIEA2019022503377Blade · nickedNR 2 ENGINE LP COMPRESSOR ROTOR BLADE NR 1 HAS A NICK AT L/E CONTOUR. INSPECTED AND FOUND TO BE .0003" IN DEPTH, MAX ALLOWABLE .060". NR 1 FAN BLADE FOUND TO BE IN LIMITS AND SERVICEABLE IAW AMM 72-31-02-226-019.SDR UIEA2019022503382Blade · nickedFOUND COMPRESSOR BLADE ON THE NR 1 ENGINE WAS FOUND DAMAGED. FOUND THE NR 1 BLADE NICKED, MEASURED .064 DEEP. BLENDED NICK DOWN TO .094 IAW AMM 72-31-02-308-045-1400. PERFORMED FLOURESCENT PENETRATION INSPECTION IAW AMM 72-31-02 & NDT 70-11-06, NO DEFECSDR UIEA2019021983248Fuel Filter · warning messageR ENG FUEL FILT EICAS MSSAGE ON ALL CLIMB SEGMENTS(<P><SPAN>R/R / R/H ENGINE FUEL FILTER IAW AMM 73-11-02. OPS NORMAL LEAK CHECK GOOD.</SPAN></P>)SDR UIEA2019021403220Unknown · malfunctionedSTBY ENG INST. INOP(<P>PERFORMED BITE TEST.OPS TEST NORMAL IAW B767 AMM 77-41-00. PERFORMED ENGINE RUNS IAW B767 AMM 71-41-00-00, OPS CHECKS NORMAL IAW B767 AMM 71-41-00. DESCRIPTION AND OPERATION WHEN IN "ON" POSITION POWER IS SUPPLIED THRU ENGINES RUNNING ORSDR UIEA2019021193171Oil Filter · warning messageSTATUS MSG RH OIL FILTER(<P>R&R RH ENGINE OIL FILTER I.A.W A.M.M 79-21-04 PERFORMED ENGINE RUN FOR 10 MIN I.A.W 71-00-00 MESSAGE DID NOT RETURN, LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED. VERIFIED MASTER CHIP DETECTOR WITHIN LIMITS</P>)SDR P5CA2019020600022Engine · vibrationRIGHT ENGINE VIBRATION (FAN) INDICATES 4.3 & 5.0 AT CLIMB. THRUST FL 350 AT CRUISE INDICATES 1.4. EXAMINED THE ENGINE INLET AND EXHAUST IAW FIM 77-31-FT 808. OPS CHECK OK.SDR P5CA2018121320379Warning Message · false activationAFTER STARTING LEFT ENGINE WE RECEIVED L GEN OFF CAUTION MESSAGE MESSAGE CLEARED WITH QRH PROCEDURE THIS IS THE 4TH WRITE UP WITH REGARDS TO THIS ISSUE(<P>PERFORMED BPCU TEST CARRIED OUT AS PER FIM 24-20 TASK ACRD 801 FOUND LEFT GEN OVER FREQUENCY FOUND IDG SDR IPXA2018120236483O-Ring · leakingNR 2 ENGINE, NR 1 BEARING MANIFOLD WAS LEAKING. R & R THE BEARING MANIFOLD O-RING IAW 72-31-03-401.SDR UIEA2018111642613Case · corrodedCORROSION AROUND 3EA FASTENERS HOLES ON #1 ENG FAN CASE EXTERNAL SURFACE, LOCATED APPROX BETWEEN 7 AND 8 O CLOCK POSITION AND JUST BELOW THE ECU(<P>REMOVED CORROSION, EVALUATED AREA AND FOUND WITHIN LIMITS IAW GE CF6-80C2 ENGINE MANUAL 72-22-01. TREATED AND PRSDR UIEA2018111642615Heat Shield · torn#1 ENG COOLING DUCT HEAT SHIELD SECTION IS TORN, APPROX 3 O CLOCK POSITION JUST AFT OF THE UPPER IGNITER PLUG.(<P>REMOVED AND REPLACED HEAT SHIELD INSULATION BLANKET ON #1 ENGINE DUCT AT 3 O' CLOCK POSITION IAW GE CF680C2 ESM 72-00-0</P>)SDR UIEA2018111602631Doubler · corrodedCORROSION AROUND DOUBLER AT 6 O' CLOCK PSOTION IN FAN CASE #1 ENGINE(<P>ACCOMPLISHED REPEAIR ON ENGINE #1 FAN CASE AT 6 O' CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01.</P>)SDR UIEA2018111602632Doubler · corrodedCORROSION AROUND DOUBLER AT 5 O'CLOCK POSITION IN FAN CASE ENG #1(<P>ACCOMPLISHED REPAIR ON ENG #1 FAN CASE AT 5 O'CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01</P>)SDR UIEA2018111602633Doubler · corrodedCORROSION AROUND DOUBLER AT 7 O' CLOCK POSITION IN FAN CASE ENGINE #1(<P>ACCOMPLISHED REPAIR IN ENG #1 FAN CASE AT 7 O'CLOCK POSITION IAW GE CF6-80C2 ENGINE MANUAL 72-22-01.</P><P><BR DATA-MCE-BOGUS="1" /></P>)SDR UIEA2018110502513Circuit Breaker · trippedRIGHT ENGINE IGNITOR NR 1 STATUS MESSAGE. FOUND THE CIRCUIT BREAKER M1 TRIPPED FOR THE RT IGNITOR NR 1. RESET THE CIRCUIT BREAKER AND CLEARED THE MESSAGE. PERFORMED AN AUDIBLE IGNITION TEST ON THE RT ENGINE AND OPS TESTED GOOD IAW AMM 74-00-00.SDR UIEA2018110200473Transmitter · malfunctionedSTATUS MESSAGE EICAS DISAGREE, R & R THE NR 2 ENG OIL PRESSURE TRANSMITTER IAW AMM 79-32-01. OPS CHECKED GOOD IAW AMM 71-00-00.SDR UIEA201811022433Unknown · vibrationLEFT ENGINE N2 VIBRATION INCREASED TO 4.2 WITH THRUST AT IDLE, DECREASED WITH THRUST ADVANCED. PERFORMED AVM SYSTEM TEST IAW AMM 77-31-00-770-015-H00, NO FAULTS FOUND, VIBRATION WITHIN LIMITS.SDR IPXA2018100194543Blade · damagedPERFORMED A BORESCOPE INSPECTION ON THE NR 2 ENGINE IAW PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON THE LEADING EDGE, MEASURING DIMENSION GREATER THAN 5 EDGE HOLES IAW MM 72-00-00-206-363-H00, TABLE 680 FOR MAX SERVICABLE LIMITS.SDR IPXA2018093034543Blade · missingINSPECTION TYPE:N/A**SUPPLEMENTAL SDR** PERFORMED BORESCOPE INSPECTION #2 ENG PER PMC 6. FOUND 1ST STAGE HPT BLADE MISSING MATERIAL ON LEADING EDGE MEASURING DIMENSION GREATER THAN 5 EDGE HOLES. REFER TO AMM 72-00-00-206-363-H00 TABLE 680 FOR MAX SVCABLE LIMISDR P5CA201808220205Packing · leakingOIL TRACE ON THE HORIZONTAL DRIVE SHAFT OF THE NR 1 ENGINE. REPLACED THE NR 1 ENGINE HORIZONTAL DRIVE SHAFT HOUSING PACKING IAW AMM 72-63-02-004-005 AND AMM 72-63-02-404-016 REV.124. PERFORMED A HORIZONTAL DRIVE SHAFT LEAK CHECK, NO LEAKS FOUND IAW AMM 7SDR P5CA201808220204Fuel Line · dentedFOUND THE NR 2 ENGINE UP SIDE STRUT FUEL LINE DENTED AND OUT OF LIMITS. REPLACED THE NR 2 ENGINE UP SIDE STRUT FUEL LINE IAW AMM 28-22-07-004-012-28-22-07-404-104, 28-22-07-404-008, AND 28-22-07-404-126, REV 124. LEAK CHECKED GOOD IAW AMM 28-22-07-404-126SDR P5CA2018082217195Spinner · erodedPANT PEELED ON THE NR 2 ENGINE SPINNER CONE. REPAINTED THE SPINNER CONE IAW ESM 72-21-10, REPAIR 6 REV 87.SDR UIEA2018081501704Blade · lack of lubeDURING CLIMB LT ENGINE VIB (FAN ) REACH 4.7 AT CRUISE VARIED FROM 1.4 TO 1.7 EVENT RECORD AT 1705Z REPAT WRITE UP. REFERENCES ITEM M9 FOR FAN BLADE RELUBE AND REMAPPING PERFORMED VIBRATION SURVEY TEST NR 6 IAW AMM 71-00-00 ENG VIBRATION WITHIN LIMITS ACCEPTANCSDR P5CA2018072600166Spinner · damagedPEEL OFF-PAINTING NR 2 ENGINE SPINNER CORE EXTERNAL SURFACE. CLEAN UP SURFACE AND APPLY THE COATING IAW ESM 72-21-10 REPAIR006 REV 87. COND CHK RESULT SATISFY.SDR P5CA2018072600167Liner · debondedDISBOND LINER SEGMENT NR 2 ENG FAN CASE FWD OUTER LINER SEGMENT AT 8 O'CLOCK POSITION 1. REPAIR THE BACKSHEET DISBOND AREA AND CURED THE ADHESIVE IAW EM72-22-02 REPAIR 004 REV 87. REPLACED THE BUMPER AND CURE THE ADHESIVE IAW EM 72-22-02 REPAIR 001 REV 87. FINSDR CALA2018060541404Line · leakingDURING FLIGHT, HAD A FUEL LEAK FROM THE NR 2 ENGINE, FLIGHT DIVERTED. FOUND A FUEL LINE FROM IDG FUEL OIL COOLER DAMAGED. THE LINE WAS REPLACED IAW AMM 24-11-10-424-007-001, IDLE LEAK CHECK TEST PERFORMED. FOUND ALL GOOD.SDR UIEA2018060401032Warning Message · false activationRIGHT EEC STATUS MESSAGE DISPLAYED. OPS CHECKED THE RIGHT EEC IAW FIM 73-21 FT 874, NO DEFECTS NOTED.SDR UIEA201805290959Filter · warning messageRIGHT ENGINE FUEL FILTER EICAS MESSAGE DURING CLIMB. MESSAGE DISAPPEARED AFTER 2 MINUTES. REPLACED THE FUEL FILTER IAW AMM 73-11-02 IAW FIM 73-11-FT803. OPS AND LEAK CHECKED GOOD.SDR UIEA2018052300943Transmitter · malfunctionedLEFT ENGINE OIL QUANTITY DECREASED TO 10 IN FLIGHT. SHOWS A DIFFERENCE OF .5 FROM LT AND RT. RT ENGINES QUANTITY WAS THE SAME ON PRE-FLIGHT. REMOVED AND REPLACED THE LEFT ENGINE OIL QUANTITY TRANSMITTER IAW AMM 79-31-01.SDR UIEA201805160831Relay · deformedRIGHT ENGINE RESET CHANNEL A RELAY SURFACE FOUND DEFORMED. THE RELAY REMOVED AND REPLACED AS PER SWPM 20-81-00, REV. 67, ENGINE PIMU SYSTEM OPERATIONAL TEST CARRIED OUT IAW AMM 77-35-00, REV. 124. FOUND SATISFACTORY.SDR UIEA2018040800633Connector · unsecureSTATUS MESSAGE FOR THE RIGHT ENGINE CONTROL, CAUTION MESSAGE ON LANDING. FOUND A LOOSE CONNECTOR AT P114. SEATED AND SECURED THE CONNECTOR. OPS CHECKED IAW AMM 71-00-01 TASK A87-A88.SDR IPXA2018032927976Acoustic Liner · puncturedRIGHT ENGINE HAS SMALL HOLE IN FWD FAN CASE LINER ON PANEL 5,M APPROXIMATELY 8 INCHES FROM LOWER EDGE AND 15/16 INCH AFT PANEL EDGE 11/16 INCH LONGX 5/16 TALL. R & R THE ACOUSTIC LINER SEGMENT IAW MM 72-33-01-4.SDR P5CA2018032400056Anti-Ice System · malfunctionedENGINE ANTI-ICE TURNS ON IN AUTO MODE EVEN WHEN THERE IS NO VISUAL INDICATION OF ICE, NOR SAY ICING CONDITION. SUSPECTED ICE DETECTION SYSTEM INTERMITTENTLY AT FAULT. DDG 30-80-01-02 PO APPLY FOR ICE DETECTION SYSTEM PRIMARY INOPERATIVE.SDR CA180313020Proximity Sensor · false indication(CAN) AIRCRAFT ARRIVED IN YHM WITH EICAS CAUTION MESSAGE `LE SLAT ASYM` MAINTENANCE PERFORMED A PSEU BITE TEST AND FOUND NR 9 SLAT PROXIMITY SWITCH FAULTED. FAULTED SWITCH WAS FOUND TO HAVE BONDED PROTECTIVE COVER PLATE MISSING FROM HOUSIING OF THE SWITCH. ASDR UIEA2018021500232Heat Exchanger · leakingFOUND FUEL LEAKING FROM FUEL - OIL COOLER ON THE NR 1 ENGINE. REMOVED AND REPLACED THE FUEL- OIL HEAT EXCHANGER GASKET IAW AMM 79-21-01, LEAK CHECKED GOOD, FUEL - OIL HEAT EXCHANGER TESTED GOOD.SDR UIEA2018020600191Igniter · malfunctionedRIGHT ENGINE IGNITOR 2 STATUS MESSAGE. REMOVED AND REPLACED THE IGNITER IAW AMM 74-21-02, OPS CHECKED NORMAL , NO MESSAGE PRESENT,SDR UIEA2018020600183Warning Message · false activationLEFT ENGINE OIL FILTER STATUS MESSAGE AFTER ENGINE START. INSPECTED LEFT ENGINE OIL BYPASS SYSTEM AND OPS CHECKED GOOD IAW AMM 79-35-00</P>)SDR UIEA2018020100165Monitor · malfunctionedENGINE VIBRATION INDICATING SYSTEM HAS FLUCTUATIONS FOR THE RT ENGINE. REMOVED AND REPLACED THE ENGINE VIBRATION MONITOR IAW AMM 77-31-03.SDR UIEA2018020200166Warning Message · false activationLEFT ENGINE EEC EICAS MESSAGE DURING APPROACH. RAN THE LT ENGINE IAW FIM 73-21 F/T 874, NO MESSAGE. COMPLIED WITH A BITE PROCEDURES ON LP1MV. NO FAULT CODES. OPS CHECKED NORMAL.
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