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 IPXA12674811Fairing · delaminatedINSPECTION TYPE:9C, LT WING OTBD FLAP INBD L/E FAIRING DELAMINATED 28.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PARA 5A (1) FIG. 5, REV 52.SDR IPXA12674812Fairing · delaminatedINSPECTION TYPE: 9C, LT WING OTBD FLAP MID L/E FAIRING DELAMINATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PARA 5A(1), FIG 5, REV 52.SDR IPXA12674813Fairing · delaminatedINSPECTION TYPE: 9C, LT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT 119.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM51-70-05, PARA 5A(1), FIG 5, REV 52.SDR IPXA12674814Fairing · delaminatedINSPECTION TYPE:9C, LT WING OTBD FLAP MID L/E FAIRING DELAMINATED AT 119.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PARA 5A(1), FIG 5, REV 52.SDR IPXA12674815Fairing · delaminatedINSPECTION TYPE:9C LT WING OTBD FLAP INBD L/E FAIRING DELAMINATED AT 55.5" FROM INBD EDGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PARA 5A(1), FIG 5, REV 52.SDR UIEA2012073100337Shutoff Valve · inoperativeRIGHT ENGINE BLEED PRESSURE INOPERATIVE WITH ENGINE PRESSURE. REMOVED RIGHT ENGINE PRSOV, OPS CHECKED NORMAL.SDR IPXA2674640Skin · damagedRUDDER T/E SKIN DAMAGED ON UPPER RT SIDE 12" UP FROM BOTTOM EDGE. REPAIRED IAW EO B767-5540-47177-B.SDR IPXA2M74647Bleed Valve · inoperativeWITH LEVEL II, AIR SYS 2 PRESSURE LOW ON DESCENT LEVEL II, AIR SYSTEM 1, PRESSURE LOW ILLUMINATED. EMERGENCY DECLARED. SHORTLY AFTER LEVEL II, AIR SYS 3, PRESSURE LOW (NO CABIN PRESSURE). ACCOMPLISHED EMERGENCY DESCENT. R & R APU LOAD BLEED VALVE IAW AMM 36-SDR IPXA12674816Floorboard · puncturedINSPECTION TYPE:9C, MAIN CARGO 4L, BS 540-654+22, L33 TO L55, HAS PUNCTURED FLOORBOARD. FLOORBOARD FABRICATED IAW EO B767-5320-9693H AND INSTALLED IAW AMM 53-01-06.SDR IPXA2674638Transceiver · inoperativeWEATHER RADAR FAIL DISPLAYED ON BOTH LOWER CRT AND WX S/R. DISPLAYED ON STATUS MESSAGE ON CLIMB OUT AND CRUISE. RADAR ON WX MODE, AND RANGE MODE MORE THAN 40 WOULD GIVE WXR FAIL. REMOVED RADAR TRANSCEIVER AND REPLACED WITH KNOWN GOOD UNIT FROM AC 302UP (SESDR UIEA2012073000335Plug · crackedFOUND .8750" CRACK AT 6 O'CLOCK POSITION ON THE NR 1 ENGINE TAIL PIPE EXHAUST PLUG, ACCOMPLISHED PART I OF EO 6778A012, WHICH CONSISTED OF STOP DRILLING THE CRACK WITH A 0.125" DRILL BIT AND INSPECTING FOR FURTHER DAMAGE.SDR IPXA2674637Control Panel · inoperativeWEATHER RADAR FAIL TRWS FORECAST ENROUTE. WEATHER RADAR FAILED ON HSI OK IN TEST. R & R WEATHER RADAR CONTROL PANEL IAW AMM 34-43-00-501.SDR CA120727015Idg · failed(CAN) ACFT WAS IN-FLIGHT FOR ALMOST 3 HRS, WHEN THEY HAD A LT GENERATOR FAILURE. APU WAS STARTED BUT THEN FAILED. APU STARTED UP AGAIN BUT HAD REDUCED ELECTRICAL OUTPUT. A DIVERSION WAS THEN SET UP. WHILE ENROUTE TO THE CREW THEN HAD A COMPLETE APU AUTO SHSDR UIEA2012072600332Light · inoperativeR4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R4 DOOR EMERGENCY LIGHT IAW AMM 33-51-16.SDR IPXA12674315Wedge · dentedINSPECTION TYPE: 1C, LT WING OTBD T/E FLAP, T/E WEDGE UPPER SURFACE DENTED. COMPOSITE PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 9, REV 52.SDR CA120704007Coffeemaker · odor(CAN) AT TOP OF CLIMB IN-CHARGE REPORTED AN ACRID SMELL IN THE AFT GALLEY. ELECTRICAL POWER TO THE GALLEY WAS SHUTOFF AS WERE THE RECIRCULATING FANS. THE ODOR DISSIPATED AND THE FLT CONTINUED. AS THE IN-FLIGHT CREW WAS PREPARING THE CABIN FOR DESCENT THEY TUSDR UIEA2012070200293Sensor · malfunctionedLEFT PACK INOPERATIVE IN AUTO, FOLLOWED QRH, WORKS OK IN STANDBY. R & R COMPRESSOR OVERHEAT SENSOR OUTLET IAW AMM 21-56-06. OPS CHECKED GOOD.SDR UIEA2012061600267Fuel Filter · failedSTATUS MESSAGE "RT ENG FUEL FILTER". R & R RT ENGINE FUEL FILTER IAW AMM 73-11-02. LEAK CHECKED GOOD.SDR CA120604013Fuel Tank · leaking(CAN) WHILE ON THE GATE, ACFT BEGAN TO LEAK FUEL FROM THE RT WING AT THE SUMP AREA. APPROXIMATELY 2 SQUARE METERS IN SIZE. TIGHTEN THE SCREWS OF PRESS RELIEF PANEL IN RT SURGE TANK. NO HELP TRANSFERED THE FUEL FROM RT TANK TO CENTER TANK. NO HELP. DRAIN TSDR UIEA2012060100256Starter · failedAPU WILL NOT START. REMOVED & REPLACED APU STARTER PER AMM 49-41-01, SYSTEM OPS CHECKED GOOD.SDR CA120522018Radar · failed(CAN) DUAL WEATHER RADAR FAILURE APPROXIMATELY 20 MINUTES AFTER DEPARTURE. OPERATING CREW ELECTED TO RETURN. ACFT LANDING OVER MAXIMUM LANDING WEIGHT. WEATHER RADAR SYSTEM RESET, OPS TEST CUT OUT IAW AMM 34-43-00.501. TEST PASSED, SYSTEM SERVICEABLE.SDR CA120514002Seal · departed(CAN) ON APPROACH , FLAP, AILERON SEAL CAME OFF IN FLIGHT. MOC ADVISED. LANDED WITHOUT INCIDENT. ON RT WING, T/E BETWEEN INBD AND NEXT FLAP, RUBBER SEAL FLAPPING IN THE WIND IN FLIGHT, FELL OFF ON APPROACH. FOUND ON RT INBD AILERON UPPER SEAL MISSING, DEPARSDR UIEA2012050400187Line · dentedNR 2 ENGINE OIL FILTER BYPASS LINE DENTED. REPAIRED OIL FILTER BYPASS LINE IAW 71-00-00.SDR UIEA2012050400186Line · dentedNR 2 ENGINE SCAVENGE FILTER RETURN LINE DENTED. REPAIRED SCAVENGE FILTER IAW AMM 71-00-00.SDR UIEA2012042500163Seal · brokenNR 5 FUEL NOZZLE SEAL BROKEN. NR 2 ENG OTBD FUEL RAIL NR 5 NOZZLE. R & R NR 5 FUEL NOZZLE SEAL AT NR2 ENG O/B FUEL RAIL IAW BAMM 767 73-11-05 THRU STEP 5D(5). PERFORMED OPS AND LEAK CK IAW AMM 73-11-05, CHECKS GOOD.SDR UIEA2012042500161Indicator · no testSTANDBY ENGINE INDICATOR FAILED TEST. REPLACED INDICATOR, BITE TESTED GOOD IAW AMM 77-41-01.SDR UIEA2012041800126Guide Vane · erodedNR 1 ENGINE HAS 7 FAN EXIT GUIDE VANES WITH ERODED SPEED TAPE. REPAIRED IAW AMM 77-33-00.SDR UIEA2012041800127Guide Vane · erodedNR 2 ENGINE HAS FIVE FAN EXIT GUIDE VANES WITH ERODED SPEED TAPE. REPAIRED IAW AMM 72-33-00.SDR UIEA2012040400115Filter · unknownDIFFERENTIAL PRESSURE INDICATION ON NR 2 ENGINE & IDG. R & R NR 2 ENGINE SCAVENGE OIL FILTER, INSPECTION CHECK TASK 24 11-02-212-002. NO METAL FOUND.SDR CA120404010Unknown · odor(CAN) AS A RESULT OF A VERY STRONG ODOR IN ROWS 25-27 SEATS D, E AND F. THE CREW ELECTED TO RETURN WHERE AN OVERWEIGHT LANDING OCCURRED. ENGINE RUN ACCOMPLISHED OF EACH ENGINE FOR 30 MIN WITH NO ODOR OF MUSKY SOCKS. SEAT CARPET REPLACED AND AREA DEODORIZED SDR CA120412001Slide · failed(CAN) DURING THE ACOMPLISHMENT OF SB 767-25A0260, THE LT OFF WING SLIDE UNLATCH ACTUATOR FAILED TO FULLY UNLATCH UNDER 175 IN/LBS IAW SB REQUIREMENT. ON FURTHER INVESTIGATION IT WAS DISCOVERED THAT THE MOST FWD LATCH DID NOT OPEN FULLY AND THIS CAUSED THE JAMSDR UIEA2012032000098Warning Message · illuminatedLEFT ENGINE EEC C1 STATUS MESSAGE WITH ASSOCIATED MAINT MESSAGES- L PIMU, LT ENG EEC C2, LT ENG EEC C1. OPENSDR CA120312014Duct · ruptured(CAN) AFTER ARRIVING AT THE GATE AND DURING WALK-AROUND, FOUND NR 4 SLAT, LT WING, INBD BLOW OUT PANEL BLOWN WITH NO ANTI-ICING DUCT VISIBLE FROM THE OPENING. FURTHER INSPECTION REVEALED THE DUCTS TO BE DISINTEGRATED AND FRAYED WITH STRANDS OF TUBE MATERIAL BSDR UIEA2012022900073Connector · looseDURING TROUBLESHOOTING, FOUND CONNECTOR D4224P ON NR 1 ENGINE EEC LOOSE. REMOVED, INSPECTED AND REINSTALLED CONNECTOR D422P IAW AMM 20-60-06 AND 20-10-06. NO DEFECTS NOTED.SDR UIEA2012022700064Warning Light · illuminatedLEFT ENGINE EEC MODE ON ROLLOUT.SDR UIEA2012022700063Warning Message · illuminatedLEFT IGNITER 1 STATUS MESSAGE. PREFORMED FIM 74-00-00, FIG 108 HAD CODE ON PIMU 351-25B LT ADC CHANNEL FAIL.SDR CA120214002Wire · broken(CAN) AIRBORNE RETURN AFTER HPSOV FAILURE. EMERGENCY DECLARED, NORMAL APPROACH & LANDING CONDUCTED. FOUND CONNECTOR ON LT HPSOV CONTROLLER LOOSE. CONNECTOR SECURED AND BLEED TEST CARRIED OUT. CHECKED SERVICE DETAILS AND FOUND NO CONTINUITY BETWEEN TERMINALSDR CA120124005Engine · shutdown(CAN) DURING PUSHBACK BOTH ENGINES STARTED NORMALLY, NR 1 ENGINE SHUTDOWN WITHOUT WARNING.SDR UIEA2012012100021Guide Vane · damagedLT ENGINE HAS 2 INLET GUIDE VANES DELAMINATED. NO DELAMINATION, FOUND MISSING METAL JACKET ON L/E & NBSP; APPLIED SPEED TAPE IAW AMM 72-33-00 PAGE 816 "F".SDR CA120110002Wire · damaged(CAN) AFTER DEPARTURE, THE IN-CHARGE F/A NOTICED A SMOKE ODOR IN THE GALLEY. THE SMOKE WAS CONFIRMED BY THE CREW AND THE FLIGHT RETURNED AFTER DECLARING A "PAN PAN" WITH ATC. DAMAGED WIRES TO NR 2 FWD GALLEY OVEN REPAIRED AND NR 2 OVEN C/B REPLACED IAW ENGINESDR UIEA2012010800004Warning Message · false activationRT ENGINE CONTROL MESSAGE. PEFORMED "PIMU" RESET PROCEDURES IAW FIM 73-21-00. NO FAULTS NOTED. MESSAGE CLEARED.SDR UIEA2011123100743Oil System · leakingDURING INSPECTION IAW AMM 71-71-00, LEFT ENGINE LEAKING OIL IN TAIL PIPE. 71-71-00, FOUND TO BE SERVICEABLESDR CA111026011Idg · failed(CAN) ACFT DISCONNECTED THE LT IDG APPROX 3 HR IN FLIGHT DUE TO THE DRIVE LIGHT AND ECAM MESSAGE ILLUMINATING. SCL FOUND THE 2 ADJUSMENT BOLT HEADS MISSING AND OIL IN THE COWL. THE IDG REQUIRED APPROX 3 LITRES OF OIL TO SERVICE. IMAGES 1 SHOWS THE BOLT HEADSDR CA110831004Coffeemaker · failed(CAN) ELECTRICAL POP IN FORWARD GALLEY, SIMULTANEOUS WITH GALLEY COOLER START, F/A SUSPECTED THE GALLEY COOLER AND TURNED THE COOLER OFF. NO EVIDENCE OF ELECTRICAL ARCING OR ELECTRICAL ODOR. REPORTED TO MX ON ARRIVAL, MX INVESTIGATION FOLLOWED. CHILLER AIR SDR CA110815011Indicator · failed(CAN) AT THE 80 KNT A/T CHECK ON TAKE-OFF FO`S A/T READ ZERO. REJECTED TAKEOFF AIR SPEED INDICATOR REPLACED MPN: 4039891-903,SDR CA110809003Terminal · damagedWHILE IN CRUISE, EICAS MESSAGE SHOWED AIR CONDITIONING PACK INOP. FLIGHT DIVERTED FOR REPAIRS. HPSOV EICAS ILLUMINATED MULTIBLE TIMES AFTER LEVEL OFF AT FL320. CHECKLIST QRH COMPLETED MULTIPLE TIMES. MEL 36-11-02 APPLIED, HPSOV WAS SECURED CLOSED. FOUND LUGSDR DALA1145031602Engine · failedATB, SHIP 1602 FLT 56 EWR-AMS RETURNED TO EWR DUE TO LEFT ENGINE FAILURE ON CLIMB. ENGINE REPLACEMENT. ETOPS CATEGORY 'A': ANY IN-FLIGHT SHUTDOWN.SDR IPXA11667902Blade · damagedINSPECTION TYPE:E TOP, ATB - BIRD STRIKE ON TAKEOFF, LT FAN VIBRATION 5.0. ALL OTHER ENG INDICATIONS NORMAL. REPLACED 5 EA DAMAGED BLADES IAW EO80C2-7230-43438-A & AMM 72-31-02-4 VIB SURVEY W/I LIMITS IAW AMM 71-00-00-5.SDR CA110708016Brake · fireLSA ACS ON ARRIVAL NOTICED LT MAIN GEAR BRAKES ON FIRE, VISIBLE FIRE ACS LSA CALLED STOC AND GTAA EMS DX, ACS LSA PLACE FIRE EXT ON STAND BY, MTCE AND FIRE CHIEF INSPECTED ACFT. CONDITIONAL INSP NR 6 BRAKE/WHEEL/AXLE IAW AMM05-51-14-212-094 CARRIED/ON. FOUNSDR CA110708009Sensor · failedAFTER DEPARTURE, IN A RT TURN THROUGHT 5000FT TO 7000FT, A L/E ASYMMETRY ICAS MESSAGE WAS RECEIVED WHEN THE FLAPS WERE BEING MOVED TO THE UP POSITION. ATC WAS ADVISED AND THE FLIGHT LEVELED OFF AT 7000 FT AND SPEED REDUCED. THE QRH PROCEDURE WAS FOLLOWED BUT T
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