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 ABXA20261019473Engine · vibrationIN THE CLIMB OUT RIGHT ENGINE VIB INCREASE TO 3.8 AT LEVEL OFF AT FL380 DECREASED BACK TO .6 A/ RETURNED TO FIELD (ATB) AND LANDED MTX GROUNDED A/C AND PERFORMED GENERAL VISUAL INSPECTION ON FAN BLADES, EXAHUST NO EVIDENCE OF DAMAGED. FOUND RIGHT CORE COWL ROSDR DALA2026100605524Case · damagedATB DUE TO RIGHT ENGINE OVERHEAT MESSAGE. CREW REDUCED THROTTLE TO EXTINGUISH MESSAGE AND DECLARED EMERGENCY. FOUND DAMAGE ON COMPRESSOR CASE. REPLACED ENGINE. OPS CHECK NORMAL. (9031446)(AIRCRAFT GROUNDED)SDR DALA2026092805376Engine · making metalATB DUE TO RIGHT ENGINE HIGH VIBRATION ON TAKE OFF AND CLIMB. ON ARRIVAL FOUND METAL IN THE TAIL. REPLACED RIGHT ENGINE.(9523648)(AIRCRAFT GROUNDED)SDR ABXA20260731342Anti-Ice Valve · malfunctionedLEFT ENG ANTI-ICE VALVE ON TAXI. C/W NNC 3.3 CANNOT TAKEOFF REQUIRES HIGH THRUST CYCLED ENG ANTI ICE AND EICAS/ VALVE LIGHT DISAPPEARED CALLED DISPATCH & MAINTENANCE THEY SAID RTB A/C RETURNED TO GATE AND MTX GROUNDED A/C. MTX REMOVED AND REPLACED LEFT ENGINE SDR CALA2026071717847Spinner · missingPDA 1 PDA 1 ON ARRIVAL FOR #2 ENG SPINNER CONE DEPARTED PIECE IS TRAPEZOIDAL MEASURING 13 INCHES ON THE TRAILING EDGE 8 INCHES ON THE LEADING EDGE AND 11 INCHES ON THE SIDES SEE PICTURE REF LOG PAGE 9567803 FOR ENGINE VIBE SOURCE OF DIVERSION/ ENGINE REPLACEMSDR CALA2026071617812Engine · vibrationRIGHT ENGINE MODERATE VIBRATION. FAN VIB AT 5+ ACRID SMELL IN CO CKPIT FL340.SDR CALA2026051116162Engine · vibrationFAN VIBRATION 4.1 AT CLB THRST TO FL270. AT CRUISE VIB IS 1.0. NO AIR FRM VIB FELT. OIL TEMP AND PRESS PER CREW DEBRIEF: ALL OTHER ENGINE INDICATIONS WERE NORMAL DUE TO PILOT REPORT OF VIBRATION NOT FELT IN FLIGHT DECK, PERFORMED FIM 77-31 FAULT TREE 808. SWISDR CALA2026050415931Sleeve · damagedDURING WALKAROUND FOUND #2 ENG INB THRUST REVERSER SLEEVE LINER DAMAGED 11 O CLOCK POSITION.AREA OF TRIM OUT 1FT X 2FT AT 11 O'CLOCK POSITON. ACCOMPLISHED INTERIM REPAIR PART 1 OF ECRA 7831-01423 REV D. REINSPECTED #2 ENG INB THRUST REVERSER SLEEVE LINER 11 SDR IPXA2026050222041Ring · crackedFOUND ENG-1 RT THRUST REVERSER CASCADE SUPPORT RING CRACK AT 9 O'CLOCK. REFERENCED TASK T3F18E008RMGN INSTALLED THE T/R, FAN COWL AND ACCOMPLISHED THE INSTALLATION TEST.SDR CALA2026041715440Sensor · faultedRIGHT ENG ANALOG N2 STATUS MSG DISPLAYED DEBRIEFED CREW. CREW STATED AFTER TAKE OFF INTO CRUISE THEY NOTICED RIGHT ENG BLEED LIGHT OFF LIGHT ILLUMINATED. QRH WAS PERFORMED WITH NO HELP. SHORTLY AFTER RIGHT CTR FUEL PUMP LIGHT ILLUMINATED WITH NO OTHER ALERTS. SDR DALA2026020500834Fuel Filter · contaminatedFLIGHT RETURNED TO JFK DUE TO RIGHT ENGINE FUEL FILTER MESSAGE. FOUND RIGHT ENGINE FUEL FILTER CONTAMINATED. REPLACED FUEL FILTER AFTER HIGH POWER RUN, CHECKED NORMAL. OK FOR SERVICE.(7846648)SDR ABXA20260115012Controller · defectiveDURING TAXIT OUT, EICAS MSG LT ENG CONTROL APPEARED AFTER TWO ENGINE STARTS. AIRCRAFT RETURNED TO BLOCKS. (BTB). REMOVED AND REPLACED LEFT ENG EEC IAW B767 AMM 73-21-15. A/C REMAINS NO ETOPS. AIRCRAFT RETURNED TO SERVICE.SDR CALA2025101009905Pressure Switch · faultedR ENG FUEL FILT MSG AFTER LEVEL OFF... ALL OTHER ENG INDICATION NORMAL REF FIM 73-11 FAULT TREE 803 T/SHOOTING, R/H FUEL FILTER REPLACED AS PER AMM 73-11-02 NIL FINDINGS , REPLACEMENT OF FUEL FILTER DIFFERENTIAL TRANSMITTER REQUIRED. FUEL PX SWITCH R & R IAWSDR CALA2025082208056Control Unit · faultedRTO DUE TO LEFT ENG SURGE AND STALLDEBRIEF FROM CREW PUSHING THROTTLES UP TO 70% N1 LH ENG SLOW TO ACCELERATE. ENGAGED AUTO THROTTLE AND ENGINE SPOOLED UP AND THENN1 ROLLED BACK TWICE TO 90% N1. F/O MAY HAVE SEEN EXCEEDANCE BUT NO RED BOX SHOWING. CREW HAD NO SDR DALA2025081306041Engine · fireATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. REPLACED LEFT ENGINE.SDR DALA2025072305534Engine · fireSHIP 1812 - ATB- -IFSD- LEFT ENGINE FIRE ON TAKEOFF, PERFORMED ENGINE IFSD. CORRECTIVE ACTION: FOUND SEVERE DAMAGE TO THRUST REVERES AND CORE COWLS. ENGINE CHANGE AND REPAIRS IN PROGRESS.SDR IPXA202507074238Link · wornWORN OUT SUPPORT LINK, NO.2 ENG R/H HPT CASE COOLING FWD DUCT UPPER SIDE, NEAR FUEL SUPPLY LINE. (REPLACE) OK TO WORKSDR IPXA2025070762480Manifold · brokenBROKEN - MANIFOLD, NO.2 ENG LPT CASE COOLING, NEAR 11:00 AREA. I.A.W. AMM 75-24-03-004-050-H00 AND 75-24-03-404-037-H00, REV.145, REPLACED THE LPT COOLING MANIFOLD OF NO.2 ENGINE. JOB COMPLETED AND CONDITION CHECK NORMAL.SDR DALA2025070805172Hpc · damagedSHIP 1806- DIV - DIVERTED TO AMS DUE TO LEFT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: PERFORMED BORESCOPE, FOUND MULTIPLE 1ST STAGE HPC BLADES CURLED AND SHINGLED. ENGINE CHANGE REPLACED.SDR CALA2025062305790Pressure Switch · faultedR ENG FUEL FILTER CAUTIO N AND STATUS MESSAGE INSPECTED FUEL FILTER WITH NO DEBRIS FOUND, REPLACED ENG 2 FUEL FILTER AND FUEL PRESS SWITCH REF AMM 73-11-02-404-008-H00 AND 73-34-01-424-008-H00. PERFORMED ENG 2 IDLE RUN REF AMM 71-00-00 WITH NO LEAKS NOTED ANDSDR IXXA2025061301Door · eroded#2 ENG IB TR INSIDE LIP ON THE IDG DOOR HAS CHAFFING WEAR ON LANDINGSDR CALA2025060205177Pressure Switch · faultedINTERMITTENT RIGHT ENGINE FUEL FILTER BYPASS. REMOVED, INSPECTED AND REPLACED RIGHT ENGINE FUEL FILTER REF AMM 73-11-02. INSPECTION OF FILTER SHOWED CLEAN NO DEBRIS NOTED. REMOVED AND REPLACED FUEL FILTER DIFFERENTIAL PRESSURE SWITCH REF AMM 73-34-01. LEAK CHESDR CALA2025050204417Bleed Valve · faultedL ENG OVERHEAT ON CLIMBOUT WITH ASSOCIATED BLEED OFF AND PACK OF F. COULD NOT RECOVER PERFORMED FIM 26-11 FAULT TREE 807. SEE L/P 4678470 FOR REPLACEMENT OF # 1 ENGINE FAN AIR VALVE (DUE TO HIGH PRECOOLER OUT DUCT TEMPERATURE) AS PER MM-36-11-16/401. RAN # 1 ESDR CALA2025043004350Pressure Switch · faultedDEBRIEFED CREW, NO OVWT LANDING, 32K FEET, FUEL FILTER BYPASS R MSG, ENG APPEARED AND SHOWED NORMAL, ALL INDICATIONS NORMAL. 2 HRS OUT. ADVISORY TO STATUS. 304-283-6970. PILOT. REMOVED AND REPLACE #2 ENGINE FUEL FILTER REF AMM 73-11-02-404-008-H00, LEAK CHECK SDR CALA2025042504220Bleed Valve · failedR ENG BLEED FAIL AT 75 KTS ON TAKEOFF... CHECKLIST RAN AND RESET WITH NO DEMAND HPSOV REPLACED AS PER AMM TASK 36-11-07-424-014-003 REV 144, SATIS.SDR UIEA2025012100100Frame · corrodedENG 1, FAN FRAME, BTWN 4-8 O'CLOCK SURFACE WITH SEVERAL POINTS OF CORROSION.(<P>ENG 1, FLOWPATH EXTENSION BETWEEN 4 TO 8 O'CLOCK WERE REPLACED IAW AMM 72-33-00-308-104-H00 REV 144. NO FURTHER DEFECTS NOTED</P>)SDR CALA2025011701944Wire Harness · brokenENG 2 EGT FLUX DRAMATICA LLY JUST AFTER TO POWER SET. NO OVERTE MP INDICAT ED. OTHER ENG PARAM S DEBRIEFED FLIGHT CREW ALL OTHER INDICATIONS WERE NORMAL EGT WAS INTERMITTENT HAVING FLUCUATIONS. INTERROGATED MAINTENANCE MESSAGES CH. 71 AND FOUND AUTO AND MANUASDR ABXA2025011207Warning Message · false activationDURING TAXI RH BLEED OFF AFTER START . AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC . MTX RAN RH ENGINE AND RESET RT BLEED AIR IAW AMM 71-00-00 OPS CHECK GOOD AC REMAINS NO ETOPS 180 . MTX RETURNED AC TO SERVICE .SDR ABXA20241223270Shutoff Valve · malfunctionedDURING TAXI OUT , RH ENGINE BLEED VALVE OFF REGARDLESS OF THE POSITION AFTER STARTING ENGINE. AC RETURNED TO GATE(BTB) AND MTX GROUNDED AC , TROUBLE SHOT AND REPLACED RH PRSOV IAW AMM 36-11-09 OPS CK AND LEAK CK GOOD. INSPECTED HPSOV, PRC AND PRV LINES AND FITSDR IPXA2024121872254Inlet · cracked*SUPPLEMENTAL SDR* R/H ENGINE INLET, INNER LIP, AT APPROXIMATE 12 O€™CLOCK POSITION, HAS 6 INCH CRACK SPANNING SEVERAL FASTENERS. REMOVED AND REPLACED R/H INLET COWL REF 767 M/M CHAP 71-11-01-404-005-H00.SDR ABXA20241126235Anti-Ice Valve · faultedDURING TAXI WITH BOTH ENGINES RUNNING AND ENGINE ANTI-ICE SELECTED ON WE OBSERVED THE RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED AND A RIGHT ENGINE ANTI-ICE AMBER MESSAGE AC RETURNED TO GATE( BTB) AND MTX GROUND AC . TROUBLESHOT AND FOUND MX PROCEDURES FSDR DALA2024112211156Hpc · leakingSHIP 1819 -ATB- AIR TURN BACK TO JFK DUE TO DIRTY SOCK SMELL IN CABIN. RAN ENGINE AND FOUND ODOR TO BE COMING FROM RIGHT ENGINE. PERFORMED BORESCOPE INSPECTION AND NOTED OIL WETTING IN HPC STAGE 2. CORRECTIVE ACTION: NEED ENGINE REPLACEMENT. (0670372)SDR IPXA2024101886334Fan · vibration**ATB**DURING CLIMB LFT ENG FAN VIB IND 4.1 AIRFRAME VIB ALSO NOTED ACCOMPLISHED INSPECTION OF L/H ENG IAW 77.00.00.206.001.H00 NO DAMAGED FOUND. ACCOMPLISHED FIM 71.5 FAULT 856 AND AMM 77.31.00/501. ACCOMPLISHED AVM FAN TRIM BALANE. ACCOMPLISHED HIGH POWER RSDR CALA2024102102692Bleed Valve · faultedL ENG BLEED OFF EICAS W/ ASSOC L ENG BLEED LIGHT OCCURED MULTIP LE TIMES IN FLT. THEY NOTICED THIS FLUCTUATION AT LEAST 6 TIMES. UPON DEBRIEFING FLT CREW MAINT WAS NOTIFIED THAT THE LEFT BLEED ALSO THE LEFT PACK WOULD INDICATE OFF DUE TO NOT HAVING ENOUGH INDISDR DALA2024100909868Shim · damagedSHIP 1817 -DIV- CREW REPORTED #2-ENGINE HIGH N1 VIBES IN FLIGHT. CORRECTIVE ACTION: FOUND #32 FAN BLADE SHIM DAMAGED. REPLACED SHIM AND LUBED FAN BLADES. ALL CHECK NORMAL. (6629804)SDR IPXA2024093054655Engine · leakingON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROMED BOROSCOPE INSPECTION IAW B767 AMM 72-00-00-211-801. ON THE #1 ENG .FOUND OIL POOLED AT THE 6 O`CLOSDR IPXA2024100454655Engine · leakingON DEPARTURE , AT HIGH POWER SETTING, STRONG SMELL OF DIRTY SOCKS? ON FLIGHT DECK. DISSIPATED AFTER POWER REDUCTION T/S PER B767 FIM79-21FAULT TREE 807,PERFROMED BOROSCOPE INSPECTION IAW B767 AMM 72-00-00-211-801. ON THE #1 ENG .FOUND OIL POOLED AT THE 6 O`CLOSDR DALA2024082608451Blades · out of limitsDIV - ON CLIMB OUT NOTED HIGH N1 VIBES ON RIGHT ENGINE DIVERSION TO CDG. ENGINE HAD PREVIOUS BIRD STRIKE IN NCE WHICH RESULTED IN SPINNER AND FAN BLADE DAMAGE. REPLACED SAME. HAD A 1 CYCLE BORESCOPE DEFERRAL PLACED AFTER BIRD STRIKE. UNABLE TO GET 1 CYCLE DEFESDR DALA2024072007303Engine · bird ingestionSHIP 1811 - ATB/IFSD - AIR TURNBACK DUE TO LEFT ENGINE BIRD STRIKE THAT CAUSED AN ENGINE FAILURE. CORRECTIVE ACTION: REPLACED ENGINE. REPLACED RIGHT MAIN GEAR UPLOCK FITTING, LEFT AND RIGHT GEAR UPLOCK FITTING SHEAR PINS. REPLACED NBR 1 - 8 MAIN TIRE ASSEMBLIESDR DALA2024070706832Blades · damagedSHIP 1812 - ATO - ABORTED TAKEOFF AT 150KTS DUE TO AN AIRCRAFT YAW AND SUDDEN ENGINE EGT EXCEEDANCE. LEFT ENGINE FOUND TO HAVE DAMAGE TO TURBINE BLADES. CORRECTIVE ACTION: ENGINE CHANGED. (6089112)SDR IPXA2024032667475Unknown · leakingFUEL LEAKING FROM LEFT ENGINE ACCOMPLISHED LEFT ENGINE RUN AT IDLE (CREW RAN IT) AS PER B767 71-00-00 TEST NO.3 IDLE LEAK CHECK AND CHECKED DRAINS PER B767 AMM 71-71-00. NO LEAKS NOTEDSDR DALA2024032603758Carbon Seal · leakingSHIP 1813 -DIV- DUE TO RIGHT ENGINE OIL QUANTITY LOSS, ALL OTHER ENGINE INDICATIONS NORMAL. CREW AND DISPATCH CHOSE TO DIVERT TO DTW. CORRECTIVE ACTION: FOUND THE STARTER, IDG, AND HYDRAULIC PUMP CARBON SEALS LEAKING. CAPPED THE DRAINS PER AMM AND DEFERRED FORSDR UIEA2022102201169None · noneTHREE DENTS ON ENGINE #2 PRIMARY EXHAUST OUTER SKIN BETWEEN 6/8 O´CLOCK AND BETWEEN NAC STA 323.42/344.67(<P>WELD FILL REPAIR IAW BOEING MSG: CMA-TLS-22-0022-02B</P>)SDR UIEA2022070700739None · none#2 ENG EXHAUST CASE ( CORE COWL ) RUB PADS HAS SEVERAL LOOSE/WORN PADS(<P><SPAN>REMOVED AND REPLACED LOOSE OR WORN OUT RUB PADS AT # 2 ENG. EXHAUST CORE COWL PER B767-300 SRM 51-40-02-0G-0.</SPAN></P>)SDR UIEA2022070700735Tape · noneMAIN DECK CARGO DOOR FORWARD AND AFT DOOR FRAME HAS LOOSE AND WORN TAPE.(<P><SPAN>REMOVED AND REPLACED LOOSE AND WORN TAPE AT MAIN DECK BY CARGO DOOR CUT OUT FWD & AFT PER B767-300 AMM 25-52-10-308-159</SPAN></P>)SDR KCSA2022042308Engine · stalledRIGHT ENGINE COMPRESSOR STALL, FOLLOWED BY EXHAUST GAS TEMPERATURE INCREASE, RIGHT ENGINE UNRESPONSIVE. RIGHT ENGINE LEFT AT IDLE FOR REMAINDER OF FLIGHT, EMERGENCY DECLARED.SDR KCSA2022041505None · noneDECLARED EMERGENCY FOR LEFT ENGINE FUEL FILTER ENGINE INDICATING AND CREW ALERTING SYSTEM MESSAGESDR UIEA2022041000282Fire Loop · damagedENG #1 WIRING OF FIRE LOOP LOWER DAMAGED LOCATED AT 6 O'CLOCK FWD OF PRESSURE SWITCH REPAIRED #1 ENG FIRE LOOP WIRED DETECTOR TS683 PER W/D 26-11-11 ; SWPM 20-10-14 OPS CHECK OK AMM 26-11-00SDR P5CA2022012400017Lead · noneENGINE #2 LOWER IGNITION LEAD IS DAMAGED(<P>REMOVED & REPLACED ENG #2 LOWER IGNITION LEAD PER AMM 74-21-00. OPS CHECK GOOD</P>)SDR P5CA2022012400011None · noneRIGHT ENGINE THRUST REVERSER INOP REF. MDDR # 159690.(<P>REACTIVATED RH ENGINE T/R PER AMM 78-31-01. OPS CHECK GOOD. NO DEFECTS NOTED. THIS ITEM CLEARS MDDR # 159690.</P>)
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