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 P5CA2020081700285Start Valve · malfunctionedRIGHT ENGINE START VALVE INOPERABLE (APPLIED MEL 80-00-02-01 WITH MDDR 132891, CAT 'C'. C/W MAINT PROCEDURE, MCC MIZ TIME 007. LP 1131722 ITEM 4: REMOVE AND REPLACED RIGHT ENGINE STARTER VALVE OPS NORMAL PER AMM 80-11-02/401. ITEM CLOSED DMI # 132891, NOTIFIEDSDR UIEA2020081741771Anti-Ice Valve · malfunctionedEICAS L ENG ANTI ICE AFTER ATTEMPTING TO TURN OFF. PERFORMED QRH IN FLIGHT. REMOVED AND REPLACED L/H ENGINE ANTI-ICE VALVE IAW AMM 30-21-03. OPS CK GOOD.SDR UIEA2020072301606Warning Message · false activationLEFT ENG EEC C1 STATUS MESSAGE. COMPLIED WITH ENG RUNS IAW AMM 72-00-00. NO STATUS MESSAGE PRESENT. COMPLIED WITH A BITE OF THE LT PIMU IAW FIM 73-21 FT 885. NO MESSAGES PRESENT.SDR KCSA202007201710Engine · vibrationDURING TAKEOFF AS NOSE GEAR LIFTED OFF SIGNIFICANT NOSE GEAR VIBRATION FELT. REMOVED NOSE WHEEL ASSYS IAW B767-300 AMM 32-45-02. PERFORMED WHEEL EXAMINATION IAW B767-300 AMM 32-45-03. NO DEFECT FOUND. PERFORMED INSPECTION/CHECK OF NLG TIRES IAW B767-300 AMM 32SDR P5CA2020062520201Anti-Ice System · unknownENGINE ANT-ICE IN AUTO REMAINED ON FOR THE LAST 13 MIN OF FLIGHT WITH CLEAR SKIES. 48 C. LT & RT ENG THERMAL NACELLE ANTI-ICE VALVES OPERATION CHECK COMPLETED IAW AMM 30-21-03-714. ALL OPS & INDICATIONS NORMAL.SDR P5CA2020060200169Guide Vane · delaminatedFIVE OF OGV'S ON RT ENGINE FOUND DELAMINATED AT 9 O CLOCK LOOKING FROM AFT. PERFORMED TEMPORARY REPAIR AS PER EO 1972A783. REPEAT INSPECTION EVERY 3 FLT CYCLES FOR THE INTEGRITY. PERMANENT REPAIR NEED BEFORE 25 FLT CYCLES. RAISED NON-MEL #129103.SDR P5CA2020061700169Guide Vane · damagedFIVEOF OGV'S ON RT ENGINE FOUND DELAMINATED AT 9 O`CLOCK LOOKING FROM AFT. PERFORMED TEMPORARY REPAIR IAW EO 1972A783, REMOVED AND REPLACED THE NR 2 ENGINE FAN CASES OGV'S IAW AMM 72-33-04.SDR IPXA2020056255744Skin · delaminatedINSPECTION TYPE:ETOPDELAMINATION ON #2 ENG R/H FAN COWL AT 2 O'CLOCK POSITION. DELAM APPROX 3" LONG BY 2" WIDE RUNNING PARALLEL TO THE ENGINE AXIS. PEELED UP AND THICKNESS 1/64". C/W WITH E.O. B767-7110-76630-A AND ITEM PLACED ON DEFERRAL WITH INSPECTION DUE ISDR UIEA2020051501038Pump · leakingDURING ROUTINE MX FOUND #1 ENG DRIVEN PUMP LEAKING FUEL(<P>REMOVED AND REPLACED LH ENGINE FUEL PUMP ASSY PER AMM 73-11-01/401, PERFORMED FUEL LEAK CHECK ON LH ENG DUE TO ENGINE FUEL PUMP REPLACEMENT, RAN ENG AT ALL POWER SETTING IAW 71-00-00, NO LEAKS.</P>)SDR UIEA2020051401021Engine · malfunctionedAFTER TAKEOFF HAD SMOKE/FUMES IN COCKPIT(<P>PERFORMED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION REF AMM 05-51-56. REMOVED OIL CONTAMINATION FROM THE AIR CONDITIONING AND PNEUMATIC SYSTEM REF AMM 21-00-21-102.</P><P>LP 1130723 - M6: REMOVED AND REPLACED LESDR IPXA2020051155118Plug · damagedINSPECTION TYPE:ETOP#1 ENG 1ST STG HPT BORO PLUG DAMAGER/R BORO PLUG B3-1 AS REQ'D I/A/W AMM 72-00-00-206-363-H00.SDR UIEA2020051100973Engine · leakingDURING WALK AROUND, AFTER AIRCRAFT SITTING FOR 4 HOURS, FOUND PUDDLE OF OIL UNDERNEATH RIGHT ENGINE.(<P>RIGHT ENGINE REMOVED AND REPLACED. ACCOMPLISHED IAW ATLAS W/C A-71-999-04-02. ALL OPS CHK NORMAL.</P>)SDR UIEA2020050400942Solenoid Valve · faultyAFTER LEFT ENGINE SHUTDOWN INITIATED FUEL VALVE LEFT SIDE DID NOT CLOSE FOR FORTY SECONDS.(<P>REMOVED AND REPLACED LEFT ENGINE HP FUEL SHUTOFF SOLENOID VALVE IAW AMM 73-21-23. OPS CHECK GOOD.</P>)SDR UIEA2020040800715Eec · malfunctionedPRIOR TO ENGINE START, WITH SELECTION OF HYDRAULIC DEMAND PUMPS, APU AUTO SHUT DOWN DUE TO RIGHT EEC CB CHANNEL A.(<P>RESET CB, REF FIM 73-21 FT 885, NO FAULTS NOTED.</P><P>ITEM 2: APU STARTED FIRST ATTEMPT, NO APU WORK DONE, NO FAULTS NOTED. NO COLD SOAK REQUSDR UIEA2020033100585Warning System · false activationIDLE DISAGREE EICAS MESSAGE ON TAXI - IN.(<P>VERIFIED IDLE TRA ALL READ THE SAME (34.0) AND PERFORMED MCDP TEST 52. OPS CHECK GOOD. NO FAULTS FOUND PER B767 AMM 73-21-11.</P>)SDR UIEA2020030900395Igniter · defectiveRH ENG REQUIRED 2 START ATTEMPTS. AFTER START, R ENG IGNITOR 1 STATUS MESSAGE.(<P>PERFORMED PIMU BITE TEST, VISUAL INSPECTION OF IGNITOR SHOWS BAD. REMOVED AND REPLACED RH ENG #2 IGNITOR IAW AMM 74-21-02. OPS CHKS GOOD IAW AMM 74-00-00.<BR /></P>)SDR UIEA2020022850324Warning Message · false activationON AIRCRAFT INBOUND, FOUND LEFT ENGINE FUEL VALVE MESSAGE APPEARED ON ENGINE SHUTDOWN.(<P>PERFORMED ENGINE RUN IAW 71-00-00. LIGHT AND MESSAGE CLEARED. OPS NORMAL. FOUND NO FAULTS. PLACED FUEL / IGNITION CONTROL RELAY ON ORDER WITH MCC.</P>)SDR UIEA2020022630308Control Panel · malfunctionedNO LIGHT OFF LEFT ENGINE, START SELECTOR IN SINGLE. SUCCESSFUL START ON BOTH.(<P>TRANSFERRED TO MDDR #124988 IAW MEL 74-00-01B CAT C DUE DATE 04MAR20.</P><P>LP 822360 - M2: REMOVED AND REPLACED L ENG #2 IGNITION EXCITER IAW B767 AMM 74-11-01-004-001 (OFF PART:SDR UIEA2020022190281Igniter · failedATTEMPTED 2 STARTS ON RIGHT ENGINE. GOOD DUCT PRESSURE ROTATION, FUEL FLOWING IN SINGLE AND BOTH HAD NO LIGHT OFF.(<P>PERFORMED ENGINE RUN IAW AMM 71-00-00. ENGINE RUN GOOD. FAULTED RIGHT ENGINE IGNITION 2. TRANSFERRED TO MDDR 124867 IAW MEL 74-00-01A, CAT "A"SDR UIEA2020021400252Igniter · failedSTATUS MESSAGE "R ENG IGNITOR 2".(<P>ITEM TRANSFERRED TO MDDR #124654 IAW MEL 74-00-01A, CAT A, DUE DATE 15FEB20. TIME AND INITIALS 0327Z ACL.</P><P>LP 1185158, ITEM M4: REMOVED AND REPLACED R/H ENGINE #2 IGNITOR PLUG IAW AMM 74-21-02. PERFORMED IGNITOR SYSTEMSDR P5CA2020013000022Start Valve · failedDURING ENG START, EICAS "R ENG STARTER" MESSAGE DISPLAYED. IAW AMM 80-11-02 REPLACED THE RT ENG START VALVE AND OPERATION TEST NORMAL.SDR UIEA2020020300174Fan · vibrationLEFT ENG FAN VIB AT 5.0 DURING CLIMB AT CRUISE ALT. LEFT FAN VIB 1.9.(<P>REMOVED 38EA SERVICEABLE FAN BLADE FROM ESN 706465 AND INSTALLED SERVICEABLE ON LEFT HAND ENGINE IAW AMM 72-31-02. PERFORMED VIBRATION SURVEY IAW AMM 71-00-00, TEST #6 OPS CHECK GOOD, WITSDR UIEA2020012800139Engine · vibrationLEFT ENGINE FAN VIB 4.7 ON CLIMB. PERFORMED GENERAL VISUAL INSPECTION ON INLETS & EXHAUST. 1ST STAGE FAN BLADE VISUAL INSPECTION IAW FIM 71-05 FT 856. PERFORMED ENGINE RUN, ALL PARAMETERS WITHIN LIMITS ON GROUND IAW AMM 71-00-00.</P>)SDR UIEA2020012800135Cam · bentLEFT ENGINE HIGH VIBRATION DURING CLIMB OUT, INDICATED 5.0. PERFORMED FIM TASK 71-05 FT 852, CHIP DETECTORS, CLEANED AVM CONNECTORS, O/T ENG, FOUND UPPER LATCH RING INBOARD THRUST REVERSER BENT, NOT ENGAGED. REPLACED LATCH CAM, STRAIGHTENED STOP BRACKET, IAW SDR UIEA2020012200114Bleed Air Sys · malfunctionedLEFT ENGINE BLEED WAS CYCLING ON AND OFF ON APPROACH. PERFORMED FIM TASK 36-20 FT 803. NO FAULTS FOUND. ACFT OK FOR SERVICE.SDR UIEA2020012200112Indication Sys · malfunctionedRIGHT ENGINE OIL PRESSURE INDICATION WENT TO ZERO AFTER LANDING. PERFORMED RIGHT ENGINE IDLE RUN PER AMM 72-00-00. OIL PRESSURE WAS NORMAL DURING ENGINE RUN. NO DEFECTS NOTED AT THIS TIME. A/C OK FOR SERVICE.SDR UIEA2020011300058Unknown · malfunctionedDURING CLIMB OUT LEFT ENGINE VIB DISPLAYED 4.7 ON THE FAN, ENGINE SNAPSHOT TAKEN FL 31.1 AT 1010Z SAT -40 DURING CLIMB.(<P>LEFT ENGINE VIB BITE SELF TEST IS SATISFACTORY. NO MESSAGE AT THIS TIME. MAINTENANCE PAGE SHOWS 0+0 UNITS, WITHIN LIMITS I.A.W AMM 77-31-SDR P5CA2020010800005Packing · damagedFUEL MINOR SEEPING FROM ENG 2 FUEL FILTER DIFF PRESSURE SWITCH JAM NUT.(<P>REMOVED AND REPLACED JAM NUT PACKING. OPS TEST GOOD AND NO LEAK FOUND IAW AMM 73-34-01.</P>)SDR CALA2019120902171Transmitter · inoperativeNUMBER 1 OIL PRESSURE INDICATOR SHOWS NO READING. ALL OTHER ENG INDICATIONS NORMAL LOCKED TO HAVE SFO CALL TOMC TO CONFIRM REPAIRS ARE SUFFICIENT UNLOCKED FOR SFO UPDATE REMOVED OIL PRESSURE TRANSMITTER #1 ENGINE REF AMM 79-32-01-004-071-HOO. INSTALLED OIL PRESDR UIEA2019120656007Oil System · lowAFTER 05:55 FLIGHT, FOLLOWING DAILY CHECK, AIRCRAFT BLOCK-IN WITH 18 QTS OIL QUANTITY. FOUND NO LEAKS AROUND ENGINES. SERVICED ENGINE OILS TO PROPER OPERATING LEVEL IAW AMM 12-13-01.SDR P5CA2019120280221Inlet · crackedFOUND ENG 1 INNER INLET COWL RIVET AREA CRACK (0.5" X 0.5") AT SIX O'CLOCK POSITION;REMOVED AND REPLACED L ENG INLET COWL IAW AMM 71-11-01. TAI DUCT LEAK CHECK SATISFACTORY.SDR CALA2019112702102Ecu · malfunctionedL ENG COMPRESSOR STALL W/ VISIBLE TORCHING EICAS L ENG CONT STAT US NOW L ENG EEC C1 ACCOMPLISH FIM TASK 71-05-00-815-848-N01 AND AMM 72-00-00/601 UNUSUAL CONDITION INSPECTION. CARRIED OUT FIM TASK PER 71-05-00-815-848-H01 AND UNUSUAL CONDITION INSPECTION AS PSDR UIEA2019112205944Warning Light · illuminatedON APPROACH, IDLE DISAGREE DISPLAYED ON EICAS SEVERAL TIMES, THEN EXTINGUISHED.(<P>PERFORMED TROUBLESHOOTING PER FIM 71-05 FAULT TREE 846, AND NO DEFECTS FOUND ON BOTH ENGINES' IDLE READING AT THIS TIME.</P><P>NOTE: LP 1113292 - M5: NO IDLE DISAGREE FAULTS ON SDR UIEA2019102865791Igniter · failedOVERTEMP ON #1 DURING RELIGHT, SHUTDOWN AT FL 400. RELIGHT AT FL 310. VIA QRH "IN FLIGHT". REF ITEM #1: CREW REPORTED THAT AIRCRAFT WAS APPROACHING FUEL IMBALANCE. CREW SHUT OFF L FUEL PUMPS, FORGOT TO SELECT CROSSFEED. AS THEY WERE GOING TO SELECT CROSSFEED, SDR CALA2019102301793Attach Fitting · cracked#1 ENGINE LEFT REVERSER CENTER ACTUATOR ATTACH CASTING CRACKED, JUST FWD OF CASCADE VANES HAS 2 EACH CRACKS. #1 REVERSER TRANSLATED AFT FOR ACCESS BY SWINGSHIFT. LOCKED OUT P11 BREAKERS D5 D18 D19 & L6. DEACTIVATED #1 OB REV CDU BY REVERSING LOCKOUT PLATE AND SDR UIEA201910225760Lead · faultedITEM 1: STATUS MSG L ENGINE IGNITER 1. ITEM 2: INFO ONLY - NO LIGHTOFF L ENG, FIRST START USED BOTH IGNITERS. 2ND START GOOD, ENG START SWITCH REMAINS IN BOTH. SDR UIEA2019100435634Igniter · warning messageSTATUS MESSAGE FOR THE LT ENGINE IGNITER 1. REMOVED AND REPLACED THE LT ENGINE IGNITER NR 1 IAW AMM 74-21-02, OPS CHECKED NORMAL. REMOVED AND REPLACED THE LT ENGINE NR 1 IGNITING EXCITER IAW AMM 74-11-01, OPS CHECKED GOOD.SDR P5CA2019093028202Eec · malfunctionedLEFT ENGINE EEC C1 STATUS. PERFORMED BITE ON L ENG PIMU, FOUND EEC-CPU FAIL FAULT. PERFORMED FIM 71-01 FT A81 TO ITEM B1. REMOVED AND REPLACED THE STATOR AC GENERATOR IAW AMM 73-21-02. MESSAGE WAS STILL DISPLAYED. REMOVED AND REPLACED THE LT AC GENERATOR RSDR P5CA2019082200173Seal · leakingNR 1 ENG DRAIN LINE CHECK IAW AMM 71-00-00, STARTER DRAINED 30 CC, IDG DRAINED 60 CC. HYD PUMP, FUEL PUMP, AND HMU DRAINED 0 CC. ITEM M6: LEFT ENGINE IDG AND STARTER DRAIN LINES CAPPED FOR SEAL REPLACEMENT WITHIN 10 FLIGHT CYCLES PER ECM 2019-342. REMOVED ANDSDR UIEA2019081305047Inlet · scratchedSCRATCHES ON THE INLET, NR 1 ENG NOSE COWL, FROM 5 TO 7 O'CLOCK. REMOVED SCRATCH AND MEASURED THE REWORKED AREA; DEPTH = 0.003", LENGTH = 2.8", WIDTH = 1.2". IT IS WITHIN ALLOWABLE LIMIT IAW SRM 54-12-01-1A-1 DETAIL III REV. 110 AND JOB CARD ATTACHING SHEET COSDR UIEA2019081204992Relay · malfunctionedEICAS IDLE DISAGREES. REMOVED AND REPLACED SOLENOID RELAY K0433. REMOVED AND REPLACED AIR COND RELAY K207 IAW WD 73-21-19. ENGINE RUN UP NORMAL, NO MESSAGE IAW AMM 71-00-00.SDR UIEA2019080904990Pressure Switch · failedLT ENG LOW OIL PRESSURE LIGHTS INOP. REMOVED AND REPLACED L/H LOW OIL PRESSURE SWITCH IAW AMM 79-33-01. PERFORMED ENGINE RUN IAW AMM 71-00-00. NO FAULTS NOTED. THIS CLEARS MDDR #116023. PLACARD REMOVED.</P>)SDR UIEA2019080604960Seal · out of positionORANGE SEAL BY THE T2 SENSOR STICKING OUT ON THE LEFT ENGINE.(<P>REINSTALLED ORANGE SEAL BY THE T2 SENSOR IAW AMM 71-11-01.</P>)SDR UIEA2019062704601Bowl · damagedNR 1 ENGINE OIL SCAVENGE FILTER BOWL WAS DAMAGED. REMOVED, INSPECTED, AND INSTALLED THE NR 1 ENGINE OIL SCAVENGE FILTER BOWL IAW AMM 79-21-04 AND 79-21-08. NO DAMAGE NOTED. LEAK CHECK ACCOMPLISHED ON T/C T2031.SDR P5CA2019062860134Monitor · malfunctionedLEFT ENGINE VIBRATION, 5.0 AT IDLE DESCENT. REMOVED AND REPLACED AVM IAW AMM 77-31-03 CONDITIONER SELF TESTED GOOD. PERFORMED ENGINE VIBRATION SURVEY TEST 6 IAW AMM 71-00-00 (AFTER EVM REPLACEMENT). OPS CHECKED GOOD. FAN 0.8 - LPT - 0.1 - N2 - 1.08. ALL WISDR UIEA2019062754577Engine · surgesLEFT ENGINE WAS SURGING UP TO 9% N1 AT IDLE FROM TOP OF DECENT ALL THE WAY TO LANDING.(<P>PERFORMED FIM 71-05 FT 848. OPS CHECK NORMAL, NO MSG'S. PERFORMED ENGINE RUN OF LEFT ENGINE AT IDLE AND 28% N1, NO FLUX IAW 71-00-00. OPS CHECK NORMAL.SDR UIEA201906214542Blades · damagedFOUND BLADE #5, #8, #10, #34, #35 DAMAGED ON RT ENG. ALL DAMAGE IS WITHIN LIMITS IAW AMM 72-31-02. (LENGTH X DEPTH) : / #5 BLADE 1" X .04", #8 BLADE 1.5" X .06", #10 BLADE 1.75" X .11", #34 BLADE 2" X .12", #35 BLADE 2" X .12"(<P>TRANSFER TO MDDR 113488 NON-SDR P5CA2019061870123Blade · bent#1 ENGINE (ESN 702738) - FOUND HPT STAGE 2 BLADE1 OF BLADE DENT WITH 1 AXIAL CRACK 0.90MM AND 1 AXIAL CRACK 3.13MM IN LENGTH IN L/E AREA A. THE CONDITION IS ACCEPTABLE FOR 10 FLIGHT CYCLES PER 767-300 AMM 72-00-0-206-167-H00. NR 1 ENG HPT BLADE DENT AS PER POWSDR UIEA2019061434487Solenoid · malfunctionedL ENG FUEL VALVE EICAS AND LIGHT AFTER FUEL CONTROL SET FROM CUTOFF TO RUN. REMOVED AND REPLACED FUEL S/O SOLENOID IAW AMM 73-21-20. OPS CK AND LEAK CKS IAW AMM 71-00-00 TEST 3, OPS NORMAL, NO LEAKS.SDR UIEA2019061104464Blade · nickedFOUND TWO NICKS IN R ENGINE, FAN BLADES 4 AND 5.(<P>NICKS DEPTH WERE 1/16 (TH) INCH. MAX BLEND ALLOWED IS 1/2 INCH. BLENDED PER B767 AMM 72-31-02 AREA C. COMPLETED FPI INSPECTION PER B767 AMM 70-11-06-232-001-H00.
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