GE CF6-80C2B1F
Service difficulty reports · 768
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 = 'CF680C2B1F' 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 = 'CF680C2B1F' 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 UIEA200900062Structure · damagedLT WING INBD MID FLAP L/E FOUND DAMAGED AT MOST INBD AREA. PERMANENT REPAIR PERFORMED IN ACFT WITH THE SRM 41-70-07 AND SRM 57-53-01 FIG 201, TABLE 1.SDR UIEA201000178Conduit · damagedFLEXIBLE ELECTRICAL CONDUIT AT THE LT WING GEAR DAMAGED. "PERFORMED A TIME LIMITED REPAIR IAW THE SWPM 20-10-91".SDR UIEA201000176ASeat Track · crackedMAIN CARGO SIDE DOOR AREA - SEAT TRACK LUG CRACKED AT FS 1806.95 LBL 99 NEXT TO ROLLOUT STOP ASSY. NR 1 POSITION."PERMANENT REPAIR PERFORMED IAW THE SRM 53-00-52-2R-6, REPAIR 6."SDR UIEA201000176Fairing · crackedENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.SDR UIEA201000177Fairing · crackedENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.SDR UIEA201000181Door · damagedGROUND DAMAGE FOUND ON THE BS 1112.1 - 1170 AIR CONDITIONING ACCESS DOOR 192HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL (REF FIG 1.) "TIME LIMITED REPAIR IAW PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATION OF 5 CYCLES IN ACC WISDR UIEA2010080500137Door · damagedEO 4453A264: GROUND DAMAGE FOUND ON THE BS 1112.1-1170 AIR CONDITIONING ACCESS DOOR 192 HR. THE DAMAGE PENETRATED THROUGH THE HONEYCOMB MATERIAL. (PERFORMED A TIME LIMITED REPAIR AS DESCIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE PART 2 PRIOR TO THE ACCUMULATISDR UIEA201000169Support Angle · crackedDURING OFF LOADING DAMAGE TO THE MDSCD BS 1920 SUPPORT ANGLE FOUND TO BE CRACKED (REF. FIGURE 1). "DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS AT EVERY 10FC AND PERMANENT REPAIR ATSDR UIEA201000179Skin · damagedLT T/E INBD MID FLAP INBD L/E SKIN PANEL WBL 137.55 WITH A GOUGE HOLE/DAMAGE (ONE FACE SKIN AND HONEYCOMB DAMAGE WITHOUT INTERNAL SKIN DAMAGE MEASURING 1.0 IN X 10.0 IN. "TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS OF EO 4457A195. SCHEDULE REPSDR UIEA201000123Skin · dentedEO 4453A074 RECORDED A DENT TO THE FUSELAGE SKIN AFT OF FWD CARGO DOOR BETWEEN S38 - S39 (24APR2006) WITH AN INITIAL HFEC INSP AND REPEAT INSPECTIONS AT 1,500 FC. DURING C-CHECK BEING PERFORMED ON 01 - 06 JUNE, 2009; INTERIM REPAIR WAS ACCOMPLISHED TO THE FUSSDR UIEA201000129Duct · crackedEO NR 4478A087: DURING ROUTINE INSP OF ACFT N498MC AT HKG "C" CHECK, THE NR 3 LT THRUST REVERSER PRECOOLER DUCT WAS FOUND CRACKED. THE CRACK IS APPROX 8 INCHES IN LENGTH. THE CMM 78-32-02 REPAIR 018 PROVIDES INSTRUCTIONS FOR THE REPAIR OF CRACKS IN WELD JOINTSSDR UIEA201000174Floor Panel · damagedMAIN DECK FLOOR AT STA 1700L FOUND "2 X 1" PUNCTURE. "1. REMOVE THE RELATED FLOOR PANEL FROM STA 1660 TO 1720 REF AMM 25-50-00. REF EO 4453A243 REPAIRED THE DAMAGE WITH BMS5-28 TYPE 19 AND BMS 9-3 TYPE L FABRIC AND EPO CAST 50A19816 RESIN CSRM 53-00-50 REPAIR SDR UIEA201000120Skin · delaminatedEO 4457A189 WINGS - LT INBD & OTBD FORE FLAP AND OTBD AFT FLAPS. NUMEROUS AREAS OF DAMAGE/DELAMINATION. ACCOMPLISH REPAIR TO THE LT OTBD FORE FLAP, L/E MID SECTION DELAMINATION (3 AREAS) IAW THE SR 57-53-01 FIG 201, RPR 1 TABLE 1 AND SRM 51-70-07 ( REF FIG 1SDR UIEA201000116Skin · delaminatedACCOMPLISH REPAIR TO THE LT INBD AFT FLAP, LOWER SURFACE INBD FWD AREA OF DELAMINATION IAW SRM 57-53-01 FIG 201,SRM 51-70-07 (REF FIG 1). ACCOMPLISH REPAIR TO THE RT INBD FORE FLAP, INBD T/E LOWER SURFACE DAMAGE IAW SRM 57-53-01, FIG 201, RPR 1 TABLE I AND THESDR UIEA201000180Floorboard · damagedRT MAIN DECK BS 1500 FLOORBOARD DAMAGED. "TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS OF EO 4453A238, INITIATE INSPECTIONS AT EVERY 5 FLIGHT CYCLES. SCHEDULE PERMANENT REPAIR AT THE NEXT A CHECK AFTER PART 1 IN ACC WITH THE SRM 53-00-50 FIG 20SDR UIEA201000175Linkage · damagedRT OTBD MID TO AFT FLAP SUPPORT LINKAGE STRUCTURE PN 65B39149-19/21 WAS FOUND DAMAGED, WITH A GOUGE/DENT. "AFTER BLEND OUT THE REWORKED AREA MEASURED 0.500 IN WITH A 0.013 IN DEPTH. IN ADDITION, INSPECTION OF THE DAMAGE WAS PERFORMED AS DESCRIVED IN THE PART 1SDR UIEA201000109Flap Track · damagedEO DOCUMENTS A MAJOR REPAIR. DURING D-CHECK, DAMAGE WAS FOUND TO 1 FASTENER COUNTERSUNK TO A DEEPER PROFILE (0.730"/100 DEGREE) BEYOND OHM REQUIREMENTS OF THE ORIGINAL DESIGN DIMENSION ( 0.645-0.675" /100 DEGREE REF FIG 1) OF NR 8 FLAP TRACK (PN:65B17061-116, SDR UIEA201000170Floor Support · corrodedCORROSION AT UPPER DECK GALLEY FLOOR FWD. OTBD SUPPORT FITTING WITH CORROSOIN DAMAGE. DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY A-CHECK AND PERMANENT REPAIR AT THE NEXT C
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