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 UIEA2021011500064Engine · oil consumptionHIGH OIL CONSUMPTION #2 ENGINE. RH ENG CHANGE COMPLETE IAW W/CARD A-71-999-04-02 ENG. RUN COMPLETEDSDR UIEA2021010800019Filter · warning messageSTATUS MESSAGE LT ENGINE FUEL FILTER. REMOVED AND REPLACED FUEL FILTER ELEMENT OF ENGINE NR 1, IAW AMM 73-11-02. NO LEAKS THEN PERFORMED WET MOTER, THEN RAN ENGINE NR 1, PER AMM 71-00-00. THIS CLEARS STATUSS MESSAGE LT ENGINE, FUEL FILTER OPERATIONS CHECKS SDR UIEA2021010900022Anti-Ice Valve · stuckRT ENGINE A/I VALVE INTERMITTENTLY STICKS WHEN OPERATING. REMOVED AND REPLACED RT ENGINE COWL ANTI ICE VALVE, IAW AMM 30-21-03. PERFORMED OPERATIONS TEST AND LEAK CHECK, FOUND GOOD.SDR UIEA2021010700016Eec · malfunctionedR ENG EEC EICAS MESSAGE ( ELECTRONIC ENGINE CONTROL (EEC) SYSTEMS, EEC NORM MODE (CF6 FADEC) )(<P>TRANSFERRED TO MDDR 140560 CAT C DUE DATE 16 JAN 21 MEL 73-21-01-03 CAT 3 RESTRICTED</P><P>DATE 7 JAN - LP 1246285 ITEM 3 - ONT- TROUBLESHOT PER FIM 73-21 FT 874 SDR UIEA2021010600013Carbon Seal · leakingNR 2 ENGINE REQUIRES DRAIN LINES TO BE CAPPED DUE TO HIGH OIL CONSUMPTION. CAPPED THE NR 2 ENGINE STARTER, IDG, HYD PUMP/ FUEL PUMP AND HMU DRAIN LINES, PER AMM 71-71-00 AND PER MM 2020P-525. TRANSFERRED TO NON-MEL 140508, MCC NOTIFIED. DUE IN 10 FLT CYCLESSDR UIEA2020122702618Pimu · malfunctionedAFTER RT ENGINE START, RT ENGINE EEC IN ALT MODE. TRANSFERRED TO DMI 140096, IAW DDG/MEL 73-21-01-03. CAT C DUE 06JAN21. MCC NOTIFIED. PLACARD INSTALLED. A/C CAT III RESTRICTED. REMOVED AND REPLACED L ADC (OFF PART: PN 4040800-906, SN 93103896, PER FIM TSDR P5CA2020122600408Warning Message · false activationEICAS STARUS MESSAGE "RT OIL FILTER", OIL PRESSURE NORMAL, IAW AMM 71-00-00-862-0120-H03 POWERPLANT OPERATING LIMITATIONS. THIS MESSAGE "RT OIL FILTER" DISPLAYED BRIEFLY WITH OIL PRESSURE WITHIN NORMAL RANGE IS NORMAL. OK TO CONTINUE.SDR UIEA2020122202610Unknown · unknownNUMBER 1 ENGINE START VALVE LIGHT FAILED TO ILLUMINATE, ENGINE START VALVE LIGHTS, -200/-300. TRANSFERRED TO MDDR 139877, IAW MEL 80-00-01-01, CAT C. PERFORMED ENGINE START 2X, START VALVE LIGHT ILLUMINATES & EXTINGUISHES AT START AND AT 50% N2 EACH ATTEMPT.SDR UIEA2020122102604Panel · openON POST FLIGHT INSPECTION, PANEL WAS FOUND OPEN. PERFORMED PNEUMATIC LEAK TEST, IAW BOEING 767 AMM 71-00-00. NO LEAK DETECTED. CLOSED PANEL, IAW BOEING 767 AMM 78-31-14.SDR UIEA2020121702589Warning Message · false activationBLEED AIR UNAVAILABLE. AFTER DEICING ACCOMPLISHED POST DE-ICE CHECKLISTS, PER FCOM VOL 1. ENGINE RUN REQUIRED DUE TO ENTRY M1. PERFORMED BITE ON AIR SUPPLY CONTROL SYSTEM, IAW B767 AMM 36-23-00 AND FOUND NO FAULTS. SEE ENTRY M3 FOR ENGINE RUN. M3: PERFORMSDR UIEA2020121302550Status Message · false activationRT ENGINE SPEED CARD STATUS MESSAGE AFTER ENGINE START. PERFORMED FIM 73-21 F/T 871, SYSTEM IS OK. NO FURTHER FAULTS NOTED.SDR UIEA2020120202502Accelerometer · malfunctionedDURING CLIMBOUT LPT VIB WAS ERRATIC, POINTER MOVED BETWEEN 0 AND 5.0 FOR APPROX ONE MINUTE. NO VIBRATION WAS FELT IN FLIGHT DECK VIBRATION IN CRUISE FAN 0.6 N2 0.9. ACCOMPLISHED ENGINE RUN OF BOTH ENGINES AND NO VIBRATIONS NOTED, REF AMM 71-00-00. OKAY FOR SDR UIEA2020113002471Guide Vane · damagedNR 2 RT ENGINE INLET GUIDE VANE AT 7 O'CLOCK BOBBLED ON LEADING EDGE. ENTERED INTO NON-MEL NR 138612.SDR UIEA2020112402458Bleed Valve · stickingRT ENGINE BLEED VALVE STICKS CLOSED AFTER START AND REQUIRES HIGH PRESSURE/POWER TO OPEN (HIGHER THAN IDLE). PERFORMED ENGINE RUN AND FOUND BOTH ENGINES TO OPERATE NORMAL AT THIS TIME. ALSO PERFORMED BITE MODULE TEST, SYSTEM OPERATES NORMAL AT THIS TIME, REFSDR UIEA2020112302452Status Message · false activationRT ENGINE N2 ANALOG STATUS MESSAGE. PERFORMED PIMU BITE TEST, IAW 71-01 FT 810, NO FAULTS NOTED. OPERATIONS CHECK OK.SDR UIEA2020112202441Blades · nickedNR 1 ENGINE HAS FOUR EACH NICKED BLADES WITHIN LIMITS, PER AMM 72-31-02-308-045-H00 FIG 801 NR 5 .093X .062 NR 16 .062X .062 NR 28 .187X .062 NR 30 .156X .125. BLENDED OUT NR 1 ENGINE FAN BLADES NR 5, NR 16, NR 28, NR 30. FOUND WITHIN LIMITS, PER B767-300 AMSDR UIEA2020112202438Line · damagedNR 1 ENGINE OIL TANK OVERFILL DRAIN BREATHER LINE HAS OUTER SKIN DAMAGED, INBOARD SIDE OF ENGINE. REMOVED AND REPLACED NR 1 ENGINE TEFLON HOSE, AS PER B7674-300 AMM 70-50-00.SDR UIEA2020112202436Acoustic Liner · tornNR 1 ENGINE ACOUSTIC PANEL HAS TEAR, REQUIRES REPAIR OR REPLACEMENT LOCATED AT 5 O'CLOCK POSITION. REMOVED AND REPLACED DAMAGED ACOUSTICAL PANEL LINER AT NR 1 ENGINE BY 5 O'CLOCK POSITION, PER B767-300 AMM 72-33-01-009-001-H00, AMM 72-33-01-404-011-H00.SDR IPXA2020111762494Status Message · illuminatedINSPECTION TYPE: ETOP, ETOPS FILED OPEN. LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. DEFERRED IAW MEL 26-11-1-1B.SDR UIEA2020111802419Pump · seizedFOUND LT ENGINE FUEL PUMP SEIZED DURING BOROSCOPE. REMOVED AND REPLACED LT ENGINE FUEL PUMP, IAW AMM 73-11-01. PERFORMED ENGINE RUN, IAW 71-00-00. FOUND NO LEAKS, ENGINE PARAMETERS SATISFACTORY. NO FURTHER DEFECTS NOTED.SDR UIEA2020111702407Fire Detector · malfunctionedNR 1 ENGINE FIRE LOOP 2 STATUS MESSAGE. ITEM M5, FOUND PUSHED PIN ON CONNECTOR D4154B, RESEATED PIN 2. OPERATIONS CHECK IS GOOD AT THIS TIME, IAW WDM 26-11-11 AND AMM OPERATIONS CHECK 26-11-01. REMOVED AND REPLACED FIRE LOOP LOWER FWD, IAW B767 AMM 26-11-02SDR UIEA2020111902422Pump · seizedITEM M2-LT ENGINE HAS EVIDENCE OF BIRD STRIKE. NR 1 ENGINE ESN-702138 FOR BIRDSTRIKE, IAW B767 AMM 72-00-00-206-146. FOUND NO DAMAGE BY BIRDSTRIKE WITHIN THE LPC OR HPC. 18NOV20/1348170/ITEM M8/RIV-DURING BOROSCOPE OF NR 1 ENGINE HEARD GRATING NOISE WHILE TUSDR FDEA202011132839Skin · gougedNR 2 ENGINE INBOARD CORE COWL INNER SIDE NR 2 FRAME FROM FWD END IS GOUGED. REPAIRED NR 2 ENGINE INBOARD CORE COWL NR 2 FRAME, IAW B767 SRM 54-45-01-2R REPAIR 3.SDR UIEA2020110902367None · noneINFO ONLY: RT ENGINE NO START FIRST ATTEMPT ON SINGLE IGNITOR. START OK ON BOTH. PERFORMED RT ENGINE IGNITION SYSTEM AUDIBLE TEST, IAW AMM 74-00-00. OPERATIONS CHECK GOOD, IGNITORS OPERATE NORMAL.SDR DALA2020110903638Hmu · power lossETOPS EVENT SLC-JFK. PERFORMED A REJECTED TAKE OFF AT 100 KTS DUE TO LEFT ENGINE LACK OF ACCELERATION. ENGINE WOULD NOT GO HIGHER THAN 87%. CORRECTIVE ACTION: MAINTENANCE REPLACED THE FUEL FILTER AND INSTALLED HMU. SYSTEM OPERATION IS NORMAL.SDR P5CA2020110300370Module · failedLEFT ENGINE FUEL VALVE LIGHT INOPERABLE. TRANSFERRED TO MDDR 137160, IAW MEL 73-21-03-01, CAT: C EXP: 13NOV20 MX PROCEDURE COMPLIED WITH. MZ AT 1424 05NOV20. REMOVED AND REPLACED ANNUNCIATOR LIGHT MODULE, PER AMM 33-16-02. CHECKS OK. THIS CLEARS MDDR 1371SDR MK1Y20201029010Exhaust Cone · dentedENG NR 1 EXHAUST OUTBOARD SIDE BETWEEN NAC STA 317.94-349.236 DENT HAS BEEN CAUSED DURING INSTALLATION OF PRIMARY EXHAUST P/N 015U1547-271, S/N: 0475A, LOCATION OF DENT: B/T 8-9 O`CLOCK. DIMENSIONS: L=11.5" W=1.53" Y=0.07" A/Y=21.
THE DENT IS NOT WITHIN ALLSDR 2LCF2020102901Wheel · meltedDURING THE N532LA TRANSIT SERVICE CHECK ON OCTOBER 29TH IN THE STATION OF QUITO (UIO), LOSS OF PRESSURE OCCURS IN THE WHEEL NR 1, AT THE MOMENT OF CHANGING IT, THE CORRESPONDING BEARING AND BRAKE WERE FOUND WITH DAMAGE. FOLLOWING THE PROCEDURE BY THE AMM, THESDR UIEA2020102902335Warning Light · false activationAFTER SHUTDOWN LT ENGINE VALVE REMAIN ILLUMINATED. LT ENGINE VALVE LIGHT EXTINGUISHED ON ITS OWN. PERFORMED DRY MOTOR AND IDLE RUN, IAW AMM 71-00-00. COULD NOT DUPLICATE FAULT. ENGINE PARAMETERS READ NORMAL. NO FAULTS NOTED AT THIS TIME.SDR UIEA2020102602304Feedback Unit · malfunctionedBTB DUE TO RT ENGINE WOULD NOT SPOOL PAST 60% N1 FOR TAKEOFF. REPLACED RT ENGINE RT T/R CDU FEED BACK ASSEMBLY, IAW AMM 78-31-21. RAN ENGINE TO VERIFY TAKE OFF THRUST ON L/P 1362873/1.SDR UIEA2020102802328Carbon Seal · leakingNR 1 ENGINE OIL LINES CAPPED FOR 10 FLT CYCLES (HIGH OIL CONSUMPTION), REF NON-MEL 136533. UNCAPPED NR 1 ENGINE OIL LINES, PER 71-71-00 RECONNECTED HMV AND FUEL PUMP DRAIN LINES, PER 71-71-00. FOUND IDG WITH 2 OZ OIL AND STARTER EDP WITH 1/8TH OZ OIL. NMEL SDR UIEA2020102502303Igniter · malfunctionedSTATUS MESSAGE: LT ENGINE IGNITOR 1. NO LIGHT OFF OF FIRST ATTEMPT, LEFT ENGINE NORMAL START 2ND ATTEMPT W/ENGINE START BOTH. PERFORMED AUDIBLE TEST OF LT ENGINE IGNITER 1. NO FAULTS NOTED, STATUS MESSAGE CLEARED, NO FAULTS NOTED AT THIS TIME. PERFORMED AUSDR UIEA2020101902276Connector · contaminatedLT START VALVE LIGHT DID NOT ILLUMINATE DURING START, TESTED NORMAL WITH LIGHT TEST, STARTER OPERATES NORMAL. FOUND CONTAMINATION & LOOSE CANNON PLUG D10970 ON LT STARTER VALVE. RESECURED, PER WDM 80-11-11 AND CLEANED PLUG, PER AMM 20-60-00. OPERATIONS CHECSDR FDEA202010152519Skin · gougedNR 2 ENGINE CORE COWLING LT LOWER SURFACE IS GOUGED. ACCOMPLISHED REPAIR OF NR 2 ENGINE CORE COWLING LT, IAW ROHR SRM 54-40-00 REPAIR 2.SDR FDEA202010152521Latch · chafedNR 1 INBOARD FWD T/R LATCH PANEL, FWD LIP WORN AND CHAFED 2 PLACES. REPAIRED NR 1 FWD LATCH PANEL, IAW STEA CMM 78-32-09 REPAIR 5.SDR FDEA202010152522Latch · chafedNR 2 ENGINE T/R HINGE LATCH PANEL FWD EDGE GOUGED AND HAS BARE METAL. REPAIRED NR 2 FWD LATCH PANEL, IAW STEA CMM 78-32-09 REPAIR 5.SDR UIEA2020101602266Unknown · unknownUPON CONNECTING EXTERNAL POWER RIGHT ENGINE SPOOLED TO FLIGHT IDLE FOR FIVE SECONDS BEFORE SPOOLING BACK DOWN TO GROUND IDLE BEFORE SHUTDOWN. PERFORMED ENGINE 2 IDLE RUN. NO DEFECTS NOTED AFTER SHUTDOWN WHEN TRANSFERRING POWER, REF B767 AMM 71-00-00. OPERATSDR UIEA2020101602263Packing · leakingDURING WALK AROUND FOUND NR 1 ENGINE FUEL LEAK. FOUND FUEL OIL COOLER LINE BROKEN. R & R LINE, IAW AMM 24-11-10. LEAK CHECK PENDING. PERFORMED ENGINE WET MOTOR AND ENGINE RUN UP, NO LEAKS NOTED. OPERATIONS CHECK NORMAL, IAW 71-00-00 REF LEAK CHECK ONLY. SDR UIEA2020101002208Gasket · leakingNR 2 ENGINE SHOWS SIGN OF OIL LEAK. REMOVED AND REPLACED FUEL TO/OIL HEAT EXCHANGE TUBE GASKET, IAW B767 AMM 79-21-01.SDR P5CA2020101290355Logic Card · malfunctioned"LT ENGINE SPEED CARD" STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED LT ENGINE N2 SPEED CARD, IAW AMM 73-21-54. STATUS MESSAGE CLEARED. OPERATIONS CHECK GOOD.SDR UIEA2020100752173O-Ring · damaged#2 ENGINE HAS OIL LEAK FROM HORIZONTAL DRIVE SHAFT. OIL LEAK IS WITH IN ALLOWABLE LIMITS. REF AMM TASK: 72-63-02-226-001-H00. ITEM TRANSFERRED TO NON-MEL NR 135433 FOR TRACKING PURPOSES AND PLANNED FURTHER ACTION. CVG STA, 13OCT20 LP 1250999, ITEM M8: SEE NRSDR UIEA2020100522149Warning Message · false activationRT ENGINE ANTI ICE. OPERATIONS TEST OF RT ENGINE TAI CARRIED OUT, IAW AMM 30-21-03. ALL INDICATIONS NORMAL. OK FOR SERVICE.SDR UIEA2020100652171Bushing · failedDURING EO 1972A763 ENGINE HIGH PRESSURE COMPRESSOR (HPC) STAGE 5 VSV'S LEVER ARMS INSPECTION, SEVERAL VSV'S WERE FOUND WITH EVIDENCE OF METAL TO METAL CONTACT WITH HIGH PRESSURE COMPRESSOR CASE. ACCOMPLISHED (CF6-80C2) HIGH PRESSURE COMPRESSURE (HPC) STAGE 5 SDR UIEA2020100622150Blade · distortedENGINE NR 1 BLADE NR 11 HAS DISTORTION. PERFORMED INSPECTION OF THE FAN BLADE, IAW B767 AMM 72-31-02-226-012-H00. DIMENSIONS FOUND TO BE AT 0.15 INCHES AT THIS TIME, WITHIN LIMITS AT THIS TIME. OPENED NON-MEL FOR TRACING: MDDR 135354.SDR UIEA2020093002135Relay · failedRT ENG ANTI-ICE DISCRETE LIGHT DOES NOT ILLUMINATE "VALVE" WHILE IN TRANSIT. "TAI" DOES ILLUMINATE ON EICAS. TRANSFER TO MDDR 135223, CAT C, PER DDG 30-21-02-01A DUE 09OCT20. MX ACTION COMPLIED WITH, PLACARD INSTALLED. 2219Z SP. REMOVED AND REPLACED RELAYSDR UIEA2020092542065Engine · unknownNO LIGHT OFF ON THE NR 1 ENGINE ON FIRST ATTEMPT. DISCONTINUED START AFTER 25 SECONDS, IAW COMPANY POLICY. GROUND CREW REPORTED SEEING SOME SMOKE COMING FROM THE NR 1 ENGINE DESPITE NO INDICATION OF LIGHT OFF OR EGT RISE IN COCKPIT. ATTEMPTED 2ND START WITHSDR UIEA2020092542061Warning Message · illuminatedSTATUS MSG "LT ENG IGNITOR 1". PERFORMED LT PIMO BITE, IAW FIM F/T 810. 2 FAULTS 350-18 A/B TMC & 35120-8 LT IGN 1 FAIL. CLEARED FAULTS, STATUS MSG CLEARS. PERFORMED ENGINE RUN NR 1 IN BOTH SINGLE AND BOTH IGNITORS POSITIONS. ALL PARAMETERS NORMAL, PER 72-SDR UIEA2020092852072Warning Message · false activationRT ENG ANTI ICE EICAS ILLUMINATED W/ASSOCIATED VALVE LIGHT WHEN SELECTING SWITCH TO THE OFF POSITION. OPERATIONAL TEST OF RT ENG TAI CARRIED OUT, IAW AMM 30-21-03. ALL IND NORMAL, OK FOR SERVICE.SDR UIEA2020092212032Engine · not reportedWO 70929 DUE TO NR 2 ENGINE UER. CW WO 70929. REMOVED AND REPLACED NR 2 ENGINE, PER INSTRUCTIONS CONTAINED IN THE W/O.SDR UIEA2020092212033Wire Harness · inoperativeRT START VALVE INOP. REMOVED AND REPLACED RT ENGINE HARNESS, REF AMM 70-50-00. REF START VALVE OPS NORMAL ON ENGINE RUN UP, IAW AMM 71-00-00.
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