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 UIEA2019111905933Wire · damagedLEFT ENGINE OIL PRESSURE NOT SHOWING ON EICAS.(<P>TEMPORARILY REPAIRED WIRE W5322-301R-18 IAW SWPM 20-10-13. LEFT ENGINE OIL PRESSURE INDICATION OPS CHK GOOD IAW AMM 79-32-00.<BR /></P>)SDR P5CA2019111420215Warning Message · false activationSTATUS MESSAGE: L OIL FILTER.(<P>PERFORMED IDLE ENGINE RUN OF L/H ENG IAW AMM 71-00-00. MESSAGE IS CLEARED WITH NO DEFECTS NOTED AT THIS TIME. </P><P>LP 1089201 - M5: PER MCC REQUEST, REMOVED AND REPLACED #1 ENG SCAVENGE OIL FILTER ELEMENT IAW B767 AMM 79-21SDR UIEA2019111525894Case · damagedON WALK AROUND PILOT FOUND MISSING ABRADABLE MATERIAL ON #2 ENGINE FAN CASE @ 8 O'CLOCK POSITION. APPROXIMATELY 1 SQUARE INCH IN DAMAGE.(<P>DAMAGE WITHIN LIMITS IAW 72-00-00-206-167-H00 AND 72-32-00-601, REPAIR NEEDS TO BE ACCOMPLISHED @ 18931 FLIGHT HOURS. CUSDR UIEA2019110505857Structure · unknownFAA FINDING ON LH ENG FAN COWLING FAIRINGS.(<P>INSPECTED + MEASURED LH ENG FAN COWL IAW AMM 71-11-00-822-001. FOUND WITHIN ACCEPTABLE LIMITS AT THIS TIME. NO OTHER DEFECTS NOTED.<BR /></P>)SDR UIEA2019102805800Fuel Filter · warning messageR ENGINE FUEL FILTER EICAS ON DEPARTURE.(<P>REMOVED AND REPLACED FUEL FILTER PER B767 AMM 73-11-02-004-001-H00 & 73-11-02-404-008-H00, NO LEAKS NOTED.</P>)SDR UIEA2019102205775Warning Message · false activationL ENGINE CONTROL EICAS AFTER ENGINE START.(<P>C/W FIM 73-21 FT 878 (PIMU BITE), NO MESSAGES PRESENT ON PIMU. RAN LEFT ENGINE WITH NO ISSUES NOTED. COULD NOT DUPLICATE IAW AMM 71-00-00. </P>)SDR UIEA2019102205780Engine · vibrationINFO ONLY: RIGHT ENGINE VIBRATION READS 2.9 ON INITIAL CLIMB TO CRUISE POWER SETTING. NO OTHER ABNORMAL INDICATIONS NOTED. (<P>NOTED BY MAINTENANCE, WITHIN LIMITS IAW AMM 71-00-00-862-020. </P>)SDR IPXA2019102194860Thrust Reverser · inoperativeINSPECTION TYPE:ETOPUPON LANDING RIGHT THRUST REVERSER FAILED TO DEPLOY. AMBER REV ILLUMINATED.ACCOMPLISHED OPS TEST OF RH THRUST REVERSER IAW AMM 78-31-00 PB 201 REV 128.06. FOUND SATIS WITHOUT FAULTS. SYSTEM OK TO CONTINUE. ROTHE CGN3738.SDR UIEA2019101905754Circuit Card · malfunctionedL ENG HPSOV EICAS MESSAGE, QRH COMPLETED. (<P>TRANSFERRED TO MDDR #119359 IAW AMM 36-11-02-02, CAT C, DUE DATE: 29-OCT-19. MCC NOTIFIED AND PLACARD INSTALLED.</P><P>LP 1210888 - M4: REMOVED AND REPLACED L/H BLEED AIR CONTROL CARD IAW AMM TASK 36-11-12-404-026.SDR UIEA2019101805747Blade · damaged#5 FAN BLADE ON #1 ENG HAS SMALL DAMAGE.(<P>REPAIRED #5 FAN BLADE IAW AMM 72-31-02-308-045-1100. </P><P>LP 1223620 - M9: FPI REQUIRED FOR L/H ENG, #5 BLADE. PERFORMED FPI OF #5 BLADE TIP BLEND IAW B767 AMM 70-11-06, NO DEFECTS NOTED.</P><P>LP 1223621 - M11: OPSDR UIEA2019101805746Blade · damagedFOUND LH ENG BLADES (FAN) #10 & 11 LEADING EDGE TIP CURL.(<P>LP 1223619 - M5: REF LP 1223618 - M3. REMOVED FAN BLADES #9, 10, 11, 4, 5, AND 6 IAW AMM 72-31-02. RE-INSTALLED BLADES #4, 6, AND 9 ON L/H ENG IAW AMM 72-31-02.</P><P>LP 1223618 - M3: REMOVED AND REPSDR UIEA2019101505720Seal · dislodgedORANGE SEAL APPEARS EXTRUDED OR DISLODGED ON SENSOR PROBES IN ENGINE INLET ON # 2 ENGINE.(<P>CORRECTED SEAL IAW AMM 72-32-00, NO FURTHER DEFECTS NOTED AT THIS TIME. </P>)SDR UIEA2019100905683Igniter · failedRIGHT ENGINE DID NOT LIGHT OFF ON FIRST ATTEMPT, SECOND ATTEMPT SUCCESSFUL. STATUS MSG R ENG IGNITER 1. REMOVED AND REPLACED RIGHT ENGINE IGNITER NR 1 PER AMM 74-21-02. PERFORMED RIGHT ENGINE AUDIBLE CHECK PER AMM 74-00-00-730-803-H03. OPS CHECK GOOD AT THIS SDR UIEA2019100765664Warning Message · false activationRT ENG IGNITION STATUS MESSAGE. RH ENG NO IGNITION WITH SINGLE IGN SELECTED ON FIRST START ATTEMPT. START SUCCESSFUL IN BOTH. PERFORMED RT ENGINE START AT THE GATE. ALL INDICATIONS NORMAL IN SINGLE SOURCE IGNITION START IAW AMM 71-00-00.SDR IPXA2019100447543Blade · nickedLEFT ENGINE, 1 X FAN BLADE LEADING EDGE NICK DAMAGE AT 564 MM FROM ROOT. BLEND REPAIR C/O IAW AMM 72-31-02. C/W INSPECTION OF THE LT ENGINE ONE FAN BLADE IAW AMM 72-31-02. NO CRACK NOTED. OK FOR CONTINUED SERVICE.SDR UIEA2019100315619Engine · not reportedNR 2 ENG DISC RECORD COMPLIANCE ISSUE. REMOVED AND REPLACED THE NR 2 ENGINE IAW AMM 71-00-02.SDR UIEA2019091905543Blade · nicked#2 ENGINE, #10 FAN BLADE NICKED ON LEADING EDGE AREA "D". BLENDED #2, ENG #10 FAN BLADE LEADING EDGE IAW AMM 72-31-02. INSPECTED BLADE, NO CRACKS NOTED. REQUIRES DYE PENETRANT INSPECTION TO NON MEL 117872. LP 1111411 - M4: COMPLETED THE FLUORESCENT PENETRANT ISDR CNMA2019100901Connector · defectiveINFLIGHT LOST EGT INDICATION ON RIGHT ENGINE ON BOTH UPPER EICAS AND STBY INDICATION. ACCOMPLISHED FIM 77-21. FAULT TREE 806. REMOVED & REPLACED JUNCTION BOX PER AMM 77-21. OPS CHECK NORMAL.SDR UIEA2019081505174Connector · not seatedNR 1 ENGINE, DURING START, N2 RISING UP TO 20% ONLY AND PRESSURE MANIFOLD FLUCTUATES AROUND 15-20 PSI. SEATED THE CONNECTOR PLUGS ON NR 1 HP CONTROLLER AND PERFORMED SATISFACTORY NR 1 ENGINE START WITH NO FLUCTUATING IN MANIFOLD PRESSURE IAW AMM 71-00-00.SDR UIEA2019081505175Blade · damaged#2 ENG LE FAN BLADE DENT MARKED WITH DOT.(<P>UPON FURTHER EVALUATION, FOUND DAMAGE TO BE NICK IN AREA "D" OF BLADE WITH ALLOWABLE DAMAGE TO 0.060". MEASURED 0.040". ASSET # 0017552 WITHIN ALLOWABLE LIMITS IAW AMM 72-31-02. NO ACTION REQUIRED.</P>)SDR UIEA2019081505180Tube · cracked#1 ENGINE TURBINE COOLING AIR TUBE CRACKED AT 8:30 POSITION.(<P>REMOVED AND REPLACED #1 ENG TURBINE COOLING AIR MANIFOLD @ 8:30 POSITION IAW AMM 75-24-03. AS# 0018938, AS# 0013164, AS# 0019069.</P>)SDR UIEA2019081505181Lead · damaged#2 ENGINE INBD LOWER IGNITION LEAD HAS ARC DAMAGE.(<P>REMOVED & REPLACED #2 ENG #1 SYSTEM IGNITOR LEAD IAW AMM 74-21-01. ASSET # 0019077, 0019114, 0018917 OPS CHECK ACCOMPLISHED ON TASK # T2031.</P>)SDR UIEA2019081505186Monitor · malfunctionedWHILE PERFORMING ENGINE RUNS, ENGINE VIBE BITE MSG SHOWS ON EICAS.(<P>REMOVED AND REPLACED ENG AVM IAW AMM 77-31-03. PERFORMED SATISFACTORY ENG AMM OPS CHK IAW AMM 77-31-00.</P>)SDR UIEA2019081505189Isolation Valve · malfunctionedN1 ENGINE FAILS TO SPOOL ABOVE 20% N2. REMOVED AND REPLACE RT ISOLATION VALVE IAW AMM 36-11-04. ACCOMPLISHED SATISFACTORY OPERATIONAL AND LEAK TEST IAW AMM 71-00-00, 36-11-04. NR 1 ENGINE SPOOL UP WAS 26% N2 IAW AMM 71-00-00. NO DEFECTS NOTED.SDR UIEA2019081635053Packing · leakingFOUND ENG SN: 707422 LPT D-SUMP COVER OIL SEEPING EXIST.(<P>REPLACED D-SUMP COVER PACKING WITH NEW PART IAW 71-00-00-795-034. PERFORMED ENG IDLE LEAK CHECK. RESULT CONDITION CHECK NORMAL AND NO LEAK FOUND IAW AMM <SPAN>72-53-02-004-001 & AMM 72-53-02-404-004</SDR UIEA2019081635046Packing · leakingFOUND ENG SN:707422 NO. 1 BEARING MANIFOLD OIL LEAK.(<P>REPLACED NO. 1 BEARING MANIFOLD PACKING. PERFORMED ENG IDLE RUN LEAK CHECK. RESULT CONDITION CHECK NORMAL AND NO LEAK FOUND IAW 72-31-03-004-001 & 72-31-03-404-005.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>PSDR UIEA2019081214999Igniter · malfunctionedR ENG IGNITER ON EICAS - #2 ENG WOULD NOT START SINGLE SETTING. NORMAL START ON BOTH. R & R NR 1 AND 2 IGNITER AND SWAP IGINITION BOXES ON NR 1 AND 2 TO ORIGINAL POSITION IAW AMM 74-21-02-74-11-01, OPS CHECKS OKSDR UIEA2019080984970Warning Message · false activationRIGHT ENGINE NR 1 IGNITER STATUS MESSAGE. PERFORMED FIM 74-00 FT P11 FOR THE NR 1 IGNITER. MESSAGE CLEARED, NO FAULTS NOTED AT THIS TIME.SDR UIEA2019080524936Warning Light · no indicationRT "ENG VALVE" LIGHT DID NOT ILLUMINATE ON SHUTDOWN. ENGINE SHUTS DOWN IMMEDIATELY ON SELECTION OF "CUT OFF".(<P>REPLACED RELAY K1252 PER FIM 76-11 FT 808, NO HELP. CYCLED INDICATOR LIGHT AND LIGHT TEST NORMAL. OPERATED SWITCH WITH ENG OFF, LIGHT OPS NORMAL. SSDR CA190729008O-Ring · leaking(CAN) INFLIGHT SLOW LEAK OF L SYSTEM HYDRAULIC ISSUES. SYSTEM TURNED OFF IN FLIGHT AND TURNED BACK ON BEFORE LANDING. FLIGHT LANDED SAFELY AND TAXIED TO GATE UNDER OWN POWER. RESOLUTION LH OUTBOARD SPOILER ACTUATOR FILTER COVER REMOVED IAW AMM 27-61-02-024-00SDR CA190718003Indicator · failed(CAN) REJECTED TAKEOFF DUE AIRSPEED INDICATOR NOT CROSS CHECKING BETWEEN CAPTAIN AND FIRST OFFICER. SPEED CROSS CHECK AT 80 KNOTS, CAPTAIN INDICATOR READ 0 WITH A FLAG, REJECTED AND TAXIED OFF RUNWAY WITHOUT INCIDENT. RESOLUTION LEFT MACH ASI REPLACED AND TESDR 2LCF20190716002Eec · failedAFTER TAKEOFF ON THE MIA - MVD ROUTE, A MESSAGE FROM THE LEFT ENGINE CONTROL WAS PRESENTED TO THE CREW. IN COMMUNICATION WITH THE MOC, THE CONVENIENCE OF RETURNING TO MIA WAS DETERMINED BECAUSE MVD DID NOT HAVE THE NECESSARY RESOURCES TO CORRECT THE FAIL. UPONSDR CA190722008Shutoff Valve · failed(CAN) IN CLIMB CREW NOTICED A FUEL IMBALANCE. ONCE IN CRUISE USED FUEL CONFIG CHECKLIST AND TRIED TO BALANCE FUEL. EVENTUALLY WERE ABLE TO NOTICE THAT FUEL WAS FLOWING FROM L MAIN TANK TO CENTRE TANK AT APPROX 2.6T/HR. AFTER TROUBLESHOOT WITH MOC AND NO SOLUTISDR P5CA2019071400152Cover · cutDURING #1 ENG. CHANGE, DISCOVERED 2 INCH CUT IN CONTAINMENT RING OUTER COVER, 5 O'CLOCK POSITION.(<P>PERFORMED REPAIR OF CONTAINMENT RING OUTER COVER IAW AMM 72-32-00, CURE TIME IS 8 HOURS. REF LP 1049527 ITEM M34 FOR REMOVAL OF FILM. </P><P>LP 1049527 - M34: SDR UIEA2019071204741Unknown · vibrationHIGH ENGINE VIBRATIONS NOTED ON TAKEOFF / CIMB OUT / HIGH THRUST SETTINGS ON LEFT ENGINE. EVENT RECORD SNAPSHOT. TAKEN 0440Z ON CLIMB OUT. LEFT VIB 3.2 FAN, RIGHT VIB 0.7 FAN.(<P><SPAN>FOLLOWED FIM 71-05 TREE 853 PERFORMED INCET EXAUST INSPECTION FOUND OK ALL SDR CA190711017Bolt · sheared(CAN) UPON ARRIVAL INSPECTION, FOUND THE R/H MLG SHOCK STRUT GEAR DOOR MOUNT BOLT SHEARED. THE DOOR WAS REMOVED UNDER CDL THE AIRCRAFT WAS RETURNED TO SERVICE. SB 320194R2 HAS NOT BEEN CARRIED OUT ON THIS DOOR MOUNT HARDWARE. (TC# 20190711017)SDR UIEA2019070804709Engine · malfunctionedVERIFICATION FLIGHT FAILED. N1 + N2 SURGE AT FLT IDLE DESCENDING THRU 2500'. N1 SURGE 12% N2 8%. EVENT RECORD SELECTED @ 2055Z(<P>REF W/O 53664. W/O C/W IAW W/O INSTRUCTIONS. #1 ENG CHANGE<BR /></P>)SDR P5CA2019070400140Engine · vibrationLEFT ENGINE NIB (N2) REACHED 5.0 AFTER THRUST REDUCED TO IDLE AT TOP OF DESCENT.(<P>C/W FIM TASK 71-05 F/T 852. DEFERRED LEFT ENGINE VIB INDICATION PER DDG 77-31-01 CAT C DMI 114191.</P><P>LP 1049522 - M19: LEFT ENGINE BORESCOPE NOT SUFFICIENT, ENGINE CHANGE CSDR CA190628013Actuator · failed(CAN) AFTER TAKE-OFF LEFT MAIN GEAR FAILED TO RETRACT. EICAS MSG `GEAR DISAGREE` AND `GEAR DOORS` WITH ASSOCIATED ANNUNCIATION LIGHTS. QRH PROCEDURE FOLLOWED WITH A NORMAL GEAR EXTENSION AND RETURNED TO LAND. UPON TROUBLESHOOTING FOUND THE LMLG SIDE STRUT ACTUSDR UIEA2019062874607Sensor · malfunctionedON DESCENT BEGINING @ FL310, LH ENGINE SPOOLS UP/DOWN 10% N1 & N2, AND AIRCRAFT YAWS WITH EACH SPOOL UP & DN.(<P>TROUBLESHOOT ENG FAULT IAW WDM 71-51-51 AND 71-51-53. VERIFIED VBV, VSV AND T12 WIRING FROM THE EEC TO THE RESPECTIVE COMPONENTS NO FAULTS NOTED. VSDR CA190626010Shaft · damaged(CAN) DURING AIRCRAFT SERVICE CHECK NOTED THE LEFT ENGINE INBOARD THRUST REVERSER HALF WAS NOT FULLY STOWED NEAR THE UPPER ACTUATOR. UPON FURTHER INSPECTION NOTED THE THE FLEXIBLE SHAFT ASSY BETWEEN CENTER DRIVE UNIT AND UPPER ACTUATOR WAS DAMAGED. THE LEFT ENSDR DALA2019062103722Actuator · malfunctionedFLIGHT 99 DIVERTED, DURING CLIMB OUT PASSING 18000 FT THE RIGHT ENGINE COMPRESSOR STALLED. A YAWING MOVEMENT AND LOUD BANG WAS HEARD. FIRST OFFICER DECLARED EMERGENCY. PARAMETERS REMAINED NORMAL FOR DURATION OF FLIGHT, NORMAL LANDING. REPLACED VSV ACTUATOR ASDR UIEA2019061984525Eec · failedLEFT ENGINE CONTROL EICAS MESSAGE AFTER START. PERFORMED BITE OF LH EEC WITH PIMU FAULTED CHAN A & B FOR LT EEC , REMOVED AND REPLACED THE LT EEC IAW AMM 73-21-15. OPS CHECKED GOOD.SDR UIEA2019061704505Warning Message · false activationAFTER LEFT ENGINE START RECEIVER EICAS MESSAGE L ENG CONTROL STATUS MESSAGE L ENG CONTROL(<P>PERFORMED FIM 73-21 FT 894 NO DEFECTS NOTED PIMU BITE TEST SHOW NO FAULTS EICAS MSG L ENG CONTROL GOOD </P>)SDR UIEA2019061804522Warning Message · false activationAFTER LEFT ENGINE START, RECEIVED EICAS MESSAGE L ENG CONTROL STATUS MESSAGE L ENG CONTROL. PERFORMED FIM 73-21 FLT 894 - NO DEFECTS NOTED. PIMU BITE SHOWS NO FAULTS.</P>)SDR UIEA2019061874510Exciter · malfunctioned# 2 ENGINE DID NOT START WITH SINGLE IGNITER , SWITCHED TO BOTH FOR BOTH ENGINE STARTS. PERFORMED NO.2 SYS IGNITION AUDIBLE TEST. CONFIRMED ONLY ONE IGNITER IS OPERATING WITH SWITCH SET TO 'BOTH'. A/C DOWNGRADED TO ER 60. PLACARDS INSTALLED. REMOVED AND REPLASDR 2LCF20190719001Heat Exchanger · failedON JUNE 15, THE AIRCRAFT FLEW ON THE MIA - ANF ROUTE, A REPORT BY LT BLEED DUCT LEAK IS PRESENTED, WHICH RETURNS THE AIRCRAFT TO THE MIA STATION; LT PRSOV WAS REPLACED. AFTER THIS EVENT ON JUNE 16, THE AIRCRAFT MADE THE MIA - ANF -SCL FLIGHT, PRESENTING IN THISDR UIEA2019061744494Igniter · inoperativeDURING LEFT ENGINE START, NO LIGHT OFF. PERFORMED CORRECTIVE PROCEDURE AND SNGINE START WAS SUCCESSFUL ON SECOND ATTEMPT,(<P>PERFORMED AUDIBLE IGNITION TEST ON LEFT ENGINE, COULD NOT HEAR #2 SYSTEM (TOP) IGNITER. REMOVED AND REPLACED #2 IGNITOR WITH NEW. OPS CSDR UIEA2019061304483Engine · unknownLEFT ENGINE N1 & N2 VARIES UP AND DOWN +/- 5% -6% RESPECTIVELY DURING DESCENT AT IDLE THRUST. FL 200 @ -10 C SAT. PERFORMED ENGINE IDLE RUN IAW AMM 71-00-00, NO FLUCTUATION NOTED AT THIS TIME.SDR UIEA2019061324469Status Message · false activationSTATUS MESSAGE, LEFT ENGINE SPEED CARD. PERFORMED OPS CHECK IAW PER B767 AMM 77-12-00. OPS CHECKED GOOD, NO STATUS MESSAGE DISPLAYED.
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