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 IPXA11B63958Skin · gougedGOUGE ON FUSELAGE SKIN AT LAP SEAM, STA 685, STR 34R TRIMOUT OF 1.250W X X 2.80H. DOUBLER FILLER REPAIR IAW EO B747-5330-40895-A.SDR UIEA2010121900195Sleeve · crackedDURING MX WALKAROUND OF N408MC MX FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR3 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 16" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LSDR UIEA2010121900196Skin · damagedDURING DEICING ON 19DEC2010, THE R STABILIZER FIXED T/E PANEL WAS STRUCK AT STABILIZER BL 418. THE DAMAGE MEASURES APPROX 1.375 INCH DEEP BY 1.500 INCH WIDE AS SHOWN IN FIG 1. (THE REPAIR IAW PART 1, THE REPETITIVE INSP IAW PART 2 ARE APPROVED BY DER ON THE 8SDR UIEA2010121600194Sleeve · crackedDURING MX WALKAROUND, FOUND A CRACK ON THE EXHAUST NOZZLE OUTER SLEEVE, STARTING AT APPROX THE 12 O'CLOCK POSITION ON THE NR2 ENGINE. THE CIRCUMFERENTIAL CRACK IS APPROX 12" LONG AND IS APPROX 13" FROM THE T/E OF THE NOZZLE. IAW SRM 54-41-30 THE LENGTH OF THE SDR IPXA0B63860Lamp · inoperativeLT UPPER DECK EMERGENCY EXIT GND MODE LIGHT NOT OPERATIVE. RELAMPED GND MODE LIGHT. INDICATION NORMAL.SDR UIEA2010121300190Structure · damagedDURING ROUTINE A-CHECK OF ACFT , THE NR 2 AND NR 4 LT THRUST REVERSER CORE COWL L/E WERE FOUND WITH LOOSE FASTENERS AND BROKEN BONDING MATERIAL. THE NR2 AND NR4 RT T/R CORE COWL L/E'S WERE FOUND WITH BROKEN BONDING MATERIAL. (DISPOSITION IS TO REPAIR ALL THESDR UIEA2010120600187Skin · delaminatedDURING WALKAROUND INSP, MX FOUND THE RT WING LANDING GEAR DOOR - LOWER EDGE DELAMINATION, MEASURING 2.2 IN. X 0.800 IN. (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, SCHEDULE REPEAT INSPECTIONS ASDR UIEA2010120500186Winglet · damagedDURING TAXI, ENROUTE FOR TAKEOFF. ACFT CAME IN CONTACT WITH ANOTHER ACFT ON THE TAXI WAY. THE WINGLET WAS DAMAGED. (REMOVED WINGLET AND DISPATCHED IAW CDL 57-28-1).SDR IPXA0B63693Structure · damagedRT INBD MID FLAP HAS .3750 HOLE LOCATED 11.3750 FROM T/E AND 19.2500 FROM INBD EDGE. REMOVED DAMAGE AND REPAIRED IAW B747-5750-40625-A.SDR IPXA0B63694Structure · damagedRT OTBD FORE FLAP DAMAGED. REPAIRED IAW EO B747-5750-40626-A.SDR IPXA0B63695Skin · puncturedRT INBD MID FLAP LOWER SKIN HAS 2 PUNCTURES. FIRST PUNCTURE IS .2500" DIA AND 2.2500" FROM T/E, 69.5" FROM INBD EDGE. SECOND PUNCTURE IS .2500" DIA 4.2500" FROM T/E AND 69.5" FROM INBD EDGE. REMOVED DAMAGE AND REPAIRED IAW EO B747-5750-40625-A.SDR UIEA2010112300180Skin · dentedDURING WALKAROUND INSP, MX FOUND THE LWR LOBE - LWR AFT CARGO DOOR AT BS1817, LWR FWD CORNER AREA WITH A DENT/DAMAGE, MEASURING 12.5 IN. LONG X 0.150 IN. (REF FIG 1). THE DENT EXCEEDS THE SRM 52-30-01, FIG 101, DETAIL XI ALLOWABLE LIMITS. (DISPOSITION WAS MADSDR UIEA2010112000182Floorboard · gougedDURING WALK AROUND INSP, MX FOUND GOUGES/DAMAGE TO THE MAIN DECK - FLOORBOARDS (2 EA) BS1520 - BS1580, LBL68.0 (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS, INITIATE REPETITIVE DVIS AT EVERY 1000SDR UIEA2010111000178Probe · brokenDURING ROUTINE MX "A" CHECK IN PVG, MX WAS ACCOMPLISHING EO 4477A003 AND BROKE OFF AN EGT PROBE ON NR 3, ESN 706125 AT THE 11:30 (PROBE NR 6) POSITION LEAVING THE REMAINDER OF THE PROBE IN THE LPT BOSS INACCESSABLE FOR REMOVAL. AS IAW AMM TASK 77-21-00-216-00SDR UIEA2010110900175Skin · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING REPLACEMENT OF THE HMU ON THE NR3 ENGINE, MX FOUND THE NR3 RT T/R CORE COWL WITH DAMAGE TO THE INSULATION AND THE INNER SKIN OF THE CORE COWL.SDR IPXA10B63555Circuit Card · malfunctionedAIR TURN BACK DUE TO WHEEL WELL FIRE WARNING MESSAGE AT LEVEL OFF FL340, WHEEL WELL FIRE WARNING REPEATED ITSELF. PERFORMED VISUAL INSP AT BOTH WHEEL OVERHEAT DETECTOR, FOUND NO DEFECTS AND NO MESSAGE NOTED. PERFORMED POWER ENGINE RUN, AND CHECKED DUCT LEAK SDR IPXA10B63543Fairing · chafedINSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING OTBD AREA HOLE CHAFED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5D, FIG 6, REV 57 121, CELSIUS DEGREE.SDR IPXA10B63270Fairing · delaminatedINSPECTION TYPE:C2, LT WING OTBD FORE FLAP OTBD L/E FAIRING DELAMINATION COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5.A, FIG 5, REV 57.SDR IPXA10B63008Floor Support · damagedINSPECTION TYPE:C, DMI D433753 - FWD LWR CARGO COMPT BALL MAT SUPPORT BEAM AND TRACK REPAIR AT BS 570. TIE DOWN TRACK REPAIRED IAW SRM53-00-52 REPAIR 10, REV 16 & EO B747- 5320-39438-A JUST AT RBL 45.5" BETWEEN STA570 & 591, BROKEN DAMAGE 3" ,CUT OFF LENGTH SDR UIEA2010092900172Thrust Reverser · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING ROUTINE INSPECTION A-CHECK, MX FOUND THE NR 3 RT THRUST REVERSER CORE COWL WITH A 4.0 INCH CRACK LOCATED APPROX AT THE 1 O'CLOCK POSITION (REF FIG1). OBTAIN ACCESS TO THE NR 3 RT THRUST REVERSER CSDR UIEA201000197Line · leakingENGINE 4, OIL QUANTITY DROPPED TO ZERO BEFORE OIL PRESSURE, REQUIRED ENGINE SHUTDOWN. FOUND OIL D-SUMP LINE AT 4 O'CLOCK POSITION CRACKED. R & R OIL LINE IAW MM 72-53-04 AND 79-21-02. PERFORMED HIGH POWER ENGINE RUN UP. (NR4) IAW MM 71-00-00 AND ALL INDICATIONSDR UIEA201000198Start Valve · faultyREJECTED TAKEOFF. LOW SPEED EICAS MESSAGE "STARTER CUTOUT 3". START VALVE FOUND FAULTY, ITEM DEFERRED IAW DDG IAW 80-11-01.SDR IPXA10B62525Wedge · damagedLEFT INBD T/E FLAP, T/E WEDGE HAS HOLE. REPAIRED IAW SRM 51-70-07 AND EO B747-5750-39166-B.SDR UIEA201000199Skin · damagedDURING D2C3 CHECK INSP BEING PERFORMED; DAMAGE WAS FOUND TO THE RT WING OTBD AILERON AT THE FOLLOWING LOCATIONS: WBL 925.960 & WBL 995 - AFT SIDE LOWER SURFACE - DISBOND. WBL 849.982 - AFT SIDE UPPER SURFACE - EROSION. PERMANENT REPAIRS ACCOMPLISHED IAW THSDR IPXA10B62679Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MID FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5 REV 57.SDR IPXA10B62722Wedge · delaminatedINSPECTION TYPE:C RH WING INBD FORE FLAP T/E WEDGE UPPER SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B63040Skin · damagedINSPECTION TYPE:C, EO B747-2320-37798-A FUSELAGE AT BS 2120-2140 & STR 1L-1R PERFORMED SKIN REPAIR AFTER ELT DOUBLER WAS REMOVED FROM ACFT. FUSELAGE AT BETWEEN BS 2120 TO BS 2140 AND STR 1L-1R AREA DOUBLER INSTALLED IAW EO B747-5330-39508-C (REF DWG DG215-220SDR UIEA2010083100149Rod · brokenDURING WALKAROUND INSP AT STN, DAMAGE WAS DISCOVERED AT RT WBL238.30. FIXED T/E UPPER RIB INSTALLATION CONSISTING IN BROKEN TIE ROD AND CLEVIS. (THE BROKEN ROD WAS REMOVED AND A DETAIL VISUAL INSP WAS PERFORMED TO ASSURE DAMAGE-FREE CONDITION TO THE SURROUNDSDR IPXA10B62360Floorbeam · crackedFLOOR SUPPORT BEAM DAMAGES AT FWD LWR CARGO STA 570. REPLACED BEAM IAW EO B747-5320-39489-A.SDR IPXA10B62800Fairing · dentedINSPECTION TYPE:C, LT WING - NR 6 VC FLAP BULLNOSE FAIRING DENTED 4" X 6" AT MID SECTION. LT WING NR 6 VC FLAP BULLNOSE FAIRING BTN ILES1060 & ILES1082.5 AREA SKIN REPAIRED IAW HX RS R57-44-36823 & EO B747-5750-39749. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIRSDR IPXA10B63093Skin · dentedINSPECTION TYPE:C, DMI D433270 - LT WING OTBD AFT FLAP DENT OTBD OF INBD CANOE FAIRING. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 2, FIG 203, REV 16.SDR IPXA10B62723Wedge · damagedINSPECTION TYPE:C, RT WING INBD AFT FLAP T/E WEDGE LWR SURFACE HOLED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 57.SDR IPXA10B62652Wedge · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR (REDO) NON-STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B62657Wedge · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR (REDO) NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR. 5C FIG 2, REV 57.SDR IPXA10B62658Fairing · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP L/E FAIRING EXISTING REPAIR (REDO) NON STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR. 5A(1) FIG 5, REV 57.SDR IPXA10B62670Wedge · misrepairedINSPECTION TYPE:C, LT WING INBD AFT FLAP T/E WEDGE LWR SURFACE EXISTING REPAIR (REDO) NON-STANDARD REPAIR. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C, FIG 2, REV 57.SDR IPXA10B62543Wedge · delaminatedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV. 57.SDR UIEA2010082300145Seat Track · damagedTHE PURPOSE OF THIS EO IS TO DOCUMENT A MAJOR REPAIR. DURING WALK AROUND INSP, DAMAGE TO THE MAIN DECK BS1820, LBL 98.58. SEAT TRACK DAMAGE WAS FOUND, CRACK MEASURING 14.0 INCH LONG (REF, FIG 1). DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRSDR IPXA10B62553Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1), FIG 5, REV 57.SDR IPXA10B62626Fairing · crackedINSPECTION TYPE:C, RT WING OTBD MID FLAP L/E FAIRING CRACKED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5G, FIG 9, REV 57.SDR IPXA10B62720Fairing · delaminatedINSPECTION TYPE:C, RT WING INBD MID FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A(1), FIG 5, REV 57.SDR IPXA10B62937Rib · crackedINSPECTION TYPE:C, RT WING L/E CAVITY RIB AT ILE 756 FOUND CRACK AT MID AREA. RT WING L/E CAVITY RIB AT ILE STA 756.95. REPAIRED IAW HXRS R57-41-36809 REV A AND EO B747-5740-39903-A. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR. ORG MAT'L IS FORGING 7075T73SDR UIEA2010081700143Skin · delaminatedDURING WALK AROUND INSP AT MX, REPORTED RT NR 14 L/E KRUEGER FLAP EXTERNAL SKIN (EDGEBAND) - DELAMINATION MEASURING 0.4 INCH WIDTH AND 10 PERCENT OF EDGEBAND LENGTH (REF FIG 1). DISPOSITION WAS MADE TO PERFORM TIME LIMITED REPAIR IAW SRM 51-70-02-1A FIG 101 SSDR IPXA10B62605Wedge · delaminatedINSPECTION TYPE:C, LT WING INBD FORE FLAP T/E WEDGE LWR SURFACE FOUND DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B62607Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD FORE FLAP L/E FAIRING FOUND DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR IAW SRM 51-70-07 PAR 5A(1) FIG 5, REV 57.SDR IPXA10B62667Panel · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP UPPER SURFACE EXISTING REPAIR (REDO) NON-STANDARD REPAIR. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, REV 57.SDR IPXA10B62668Panel · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP UPPER PANEL EXISTING REPAIR NON STANDARD REPAIR. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 2, REV 57.SDR IPXA10B62678Panel · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP LOWER SURFACE MID AREA EXISTING REPAIR NON STANDARD REPAIR. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 2, REV 57.SDR IPXA10B62733Panel · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP LOWER SURFACE OTBD AREA EXISTING REPAIR (REDO) NON STANDARD REPAIR. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR 4, FIG 202, SHEET 2, REV 57.SDR IPXA10B63007Skin · misrepairedINSPECTION TYPE:C, SURVEY SEQUENCE NO 580-F1-15 FUSELAGE AT BETWEEN BS2650 TO BS2661 & STR 11R - 13R AREA EXISTING REPAIR DOES NOT CORRELATE TO SRM. SURVEY SEQ 580-F1-15 FUSELAGE AT BETWEEN BS2650-BS2661 & STR 11R-13R AREA SKIN REPAIRED IAW HXRS R53-81-36813
Back to GE CF6-80C2B1F