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 U2RA201206160005Grommet · brokenCOCKPIT EMERGENCY DECENT DEVICE BLUE GROMMET FOUND BROKEN.SDR U2RA201206260002Bracket · crackedRIGHT WING LANDING GEAR STRUT DOOR LOWWER SECTION FIXED FAIRING MID BRACKET FOUND CRACKED. CRACK LENGTH 1".SDR IPXA2B73984Oil System · warning message'ENG 1 OIL FILTER' EICAS FOLLOWED QRH PROCEDURES, NOTED OIL TEMP 121 & PRESSURE 87. OPEN.SDR IPXA12B73984Engine · contaminatedIFSD - 'ENG 1 OIL FILT' EICAS FOLLOWED QRH PROCEDURES, NOTED OIL TEMP 121 & PRESS 87. MCD INSPECTION, FOUND LARGE AMOUNT OF DEBRIS. R & R NR 1 ENGINE IAW TC 71- 000-00-01 AND OPS CHECKED.SDR U2RA201206200001Retainer · crackedLEFT WING STRUT DOOR LOWER SECTION FIXED FAIRING RETAINER FOUND CRACKED. CRACK LENGTH 1".SDR U2RA201206200003Bracket · crackedRT WING T/E CAVITY AT WING BS 280 BRACKET FOUND CRACKED, CRACK LENGTH .5".SDR U2RA201206200004Support Angle · crackedRT WING NR 7, MOVEABLE FLAP FAIRING OTBD FORWARD ANGLE FOUND CRACKED IN 2 PLACES.SDR U2RA201206150002Skin · crackedNLG WHEEL WELL BS 400 LT AFT CORNER SKIN PANEL FOUND CRACKED. REF AD 2010-26-07, SB 747-53A2305. CRACK LENGTH 2.5" LONG FASTENER HOLE CRACK .030"SDR U2RA201206150004Tension Tie · crackedUPPERDECK BS 1180 RT SIDE TENSION TIE FORWARD CHANNEL CRACKED. CRACK LENGHT .035".SDR U2RA201206190002Cargo Track · crackedFORWARD CARGO COMPARTMENT STA 570 RT OF BUTT LINE 50" CARGO TRACK FOUND CRACKED. CRACK LENGTH IS 2".SDR U2RA201206190003Seal Depressor · crackedFORWARD LOWER CARGO DOOR SEAL DEPRESSOR FOUND CRACKED. CRACK LENGTH 2".SDR U2RA201206190004Roller Tray · crackedAFT LOWER CARGO COMPARTMENT AT STA 1580, RT OF BUTT LINE 58 ROLLER TRAY FOUND CRACKED, CRACK LENGTH 1".SDR U2RA201206190005Plate · crackedENGINE FUEL NOZZLE SPLASH PLATE FOUND RADIAL CRACK, CRACK LENGTH .516".SDR U2RA2010206200002Guide · crackedFORWARD LOWER CARGO COMPARTMENT STA 580-600 LT SIDE GUIDE FOUND CRACKED. CRACK LENGTH 1".SDR U2RA201206210001Beam · crackedNR 2 PYLON OTBD SKIRT FAIRING BEAM L/E CRACKED. 4 CRACKS EXTEND FROM FASTENER HOLE. CRACK LENGTHS .8"SDR U2RA201206270001Web · crackedFORWARD CARGO BS 570, RBL 45-50 WEB FOUND CRACKED. CRACK LENGTH .5".SDR U2RA201206150001Structure · crackedBS 2598, FOUND CRACKED.SDR U2RA201206150003Tension Tie · crackedUPPERDECK BS 1180 LT TENSION TIE FORWARD CHANNEL FOUND 1 EA CRACK. REF AD 2007-23-18, SB 747-53A2507. CRACK LENGTH .035"SDR U2RA201206150005Tension Tie · crackedUPPERDECK BS 1140 TENSION TIE AT FRAME WEB FOUND 1 EACH HOLE CRACK AND 2ND HOLE CRACK AT FAILSAFE.SDR U2RA201206160001Tension Tie · crackedUPPERDECK STA 1180, RT TENSION TIE AT FRAME WEB FOUND 1 EA HOLE CRACKED. REF AD 2007-23-18 SB 747-53A2507. CRACK HOLE CRACK LENGTH .035"SDR U2RA201206160002Pressure Panel · crackedLT LANDING GEAR WHEEL WELL CANTED PRESSURE DECK CLOSEOUT PANEL FOUND CRACKED. REF AD 2003-01 SB 747-51A2057. CRACK LENGTH 1".SDR IPXA12B73833Oil System · leakingLOSS OF ENGINE OIL PRESSURE AND QTY, CREW SHUTDOWN ENGINE, ENGINE WINDMILLED FOR 1:05 HOURS. INSPECTION FOUND OIL QTY IN TANK EMPTY, MCD HAVE PARTICLE TOO MUCH AND PMA INTERNAL DAMAGED SO OIL INSPECTION NOT FOUND EVIDENCE LEAKAGE AROUND ENGINE COMPARTMENT BISDR SAJF201206141017Engine · failed(B-18721) DURING CLIMB, EICAS MESSAGE "ENG 4 OIL PRESS" WITH OIL PRESSURE INDICATING 4 PSI, FOLLOWED QRH, ENGINE 4 SET TO IDLE, SHORTLY NOISE AND VIBRATION, THEN N1,N2 DROP, EICAS MESSAGE "ENG 4 FAIL", FOLLOW QRH ENG SHUTDOWN. GROUND CHECK FOUND METAL CHIPS SDR UIEA2012052100248Access Panel · damagedDURING MX WALKAROUND OF ACFT AT PVG REVEALED NR 3 ENGINE THRUST REVERSER ACCESS DOOR WAS FOUND OPEN AND DAMAGED. ACCOMPLISHED A TIME LIMITED REPAIR.SDR TRBA20120519001Wire · brokenFLIGHT 4839, CREW REPORTED LOWER EMERGENGY EXIT SIGN MAIN CABIN DOOR LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. REPAIRED WIRE ON LOWER EMERGENCY EXIT SIGN IAW JIC 33-50-00. ACFT RETURNED TO SERVICE.SDR UIEA2012042000156Rotor · damagedAFTER TAKEOFF, EXPERIENCED COMPRESSOR STALL ON NR 1 ENGINE, FOLLOWED BY 2 MORE COMPRESSOR STALLS. INSPECTION OF ENGINE ACCOMPLISHED IAW AMM 72-00-00. DAMAGE TO STAGE 5 VSV WITH 1 BROKEN, LEVER FOUND. DURING BORESCOPE DAMAGE TO 6TH, 7TH AND 8TH; STAGE COMPRSDR IPXA2B72577Blades · damagedON GEAR RETRACTION AFTER TAKE OFF, MULTIPLE ENGINE REPORTS LOUD AND ASSOCIATED VIBRATIONS ON ENG NR 1. SHUTDOWN NR 1 ENGINE IAW QRH. DUMPED FUEL RETURNED TO DEPARTURE. NO WING CAUTION MESSAGES OR ALERTS. AFT INSPECTION, FOUND 26 FAN BLADES DAMAGED. R &SDR SAJF201203051010Oil System · contaminated(B-18708) SHORT AFT REACHING TOC, OIL QTY DROPPED TO 1, OIL TEMP RISING VERY SLOW, OIL PRESS DROPPED SLOWLY. BOTH STABILIZED BEFORE REACHING LIMIT, THR LEVER WAS RESTARED, NO MESSAGE APPEARED. GROUND CHECK FOUND OIL LUB & SCAV PUMP TGB & AGB INLET SCREEN WERSDR UIEA2012042000151Skin · damagedNR 1 CORE COWL SCRATCH. REPAIRED IAW SRM 54-45-01-2R-1, REPAIR 1.)SDR SAJF2012022601007Fire Warning · false activation(B18710) AIR TURN BACK, DUE TO MAIN DECK FIRE WARNING. NO FIRE EVIDENCE WAS FOUND AFTER ACFT TURNED BACK. CHECKED ELECTRONIC COMPARTMENT FOR ANY LEAKS AND THE CONDITION OF THE SEALANT OF THE FLOOR PANELS. THE RESULT IS NORMAL. WATER RESIDUAL AND PAPER TOWSDR SAJF201202041011Screw · dislodged(B18717) EXPERIENCED TWO CAN’T SHUTDOWN ENGINE EVENTS ON NR 3 ENGINE; FIRST ON JAN 27,2012 & SECOND ON FEB 4,2012). DURING TROUBLESHOOTING, GROUND CONFIRMED THAT THE HMU FUEL SHUTOFF VALVE STUCK IN OPEN POSITION & NR 2 HMUS WERE REPLACED. SHOP REPORT REVEALSDR QOCF2012F00034Engine · flamed out(B-16462) NR 2 ENGINE FLAMEOUT DURING LANDING AT SPEED 50 KNOTS WITH FULL REVERSER IN ANC.SDR UIEA2011103100633Insulation · delaminatedDURING WALKAROUND, MX FOUND THE NR 4 RT T/R INSULATION DAMAGE AS FOLLOWS (REF FIG 1) DELAMINATIONS AND PUNCTURE OF INSULATION FROM HONEYCOMB STRUCTURE IS AS FOLLOWS: DELAMINATED AREA IS 19.0" FROM FRAME TO FRAME AND 35.0" TOP TO BOTTOM. THE PUNCTURE IN THE MSDR P5CA2011091200466Fuel Filter · dirtyON DESCENT INTO PVG NR 1 ENGINE HAD FLAME-OUT AND AUTO RESTART WITH STATUS MESSAGES & NBSP;"IDLE DISAGREE" AND "ENGINE NR 1 CONTROL" (ACCOMPLISH FUEL SUMP OF NR 1 MAIN TANK AS PER AMM 12-11-10 WITH "O" WATER FOUND. REMOVED AND REPLACED ENGINE NR 1 FUEL FILTERSDR UIEA2011082700474Skin · puncturedDURING WALKAROUND, MX FOUND THE NR 4 RT THRUST REVERSER CORE COWL HAS 2 PUNCTURES IN THE SKIN LOCATED ABOVE THE ACCESS PANEL AND BLOWOUT DOOR. DAMAGE TO THE ACCESS PANEL AND BLOWOUT DOOR HINGES, LATCHES AND LANYARDS. REPAIRED.SDR UIEA2011082300458Fire Warning · false indicationPRIOR TO LANDING, HAD A FALSE MAIN DECK FIRE WARNING INDICATION. WARNING TERMINATED AFTER 30 SECONDS. PERFORMED FIRE DETECTION SYS TEST IAW MM 26-14-00. PASSED WITH NO DEFECTS FOUND.SDR UIEA2011080700432Skin · damagedDURING MX WALKAROUND, MX FOUND DAMAGE TO THE NR 2 ENG RT THRUST REVERSER TRANSLATING COWL EXTERNAL SKIN OUTER FINISH DAMAGE. THE DAMAGE IS LOCATED IN NEAR THE REVERSER COWL SKIN T/E (REF FIG 1-3): PERFORMED A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK ISDR SAJF201107010023Blades · failed(B-18711) AIRCRAFT ENROUTE, AFTER T/O AT FL015, NR 4 ENG HAD "BANG" SOUND AND SPOOL DOWN AND EGT OVER LIMIT. CREW FOLLOWED QRH TO SHUTDOWN ENGINE, DUMP FUEL AND AIR TURNED BACK. GROUND CHECK FOUND MANY METAL CHIPS IN TAILPIPE AND N1 ROTOR SEIZED. PRELIMINARYSDR UIEA2011061500314Engine · vibrationON TAKE-OFF ROLL, ENGINE VIBE 4 SHOWED 5.2. FELT A VIBRATION WHEN SELECTING MAX THRUST (VISUALLY INSPECTED INLET/EXHAUST OF ENGINE, MAG CHIP DETECTOR AND & NBSP; ENGINE LPT AREA COMPONENTS AMD VIBRATION PICKUP CONNECTOR & NBSP; ALL IAW FIM 71-00. PERFORMED BSDR SAJF20110609021Engine · failed(B-18712) ACFT ENROUTE, DURING CLIMB AT 1000 FT FLT CREW HEARD A NOISE, AT 5000 FT RETARDED NR 3 THRUST LEVER THEN NOISE GONE. CLIMB 7000 TO 9000 FT T/L ADVANCED BANG SOUND COME OUT AGAIN, THOUGH ALL ENGINE PARAMETERS ARE WITHIN LIMIT. FLT CREW CONFIRMED THE SDR UIEA2011060700287Fairing · crackedDURING A-CHECK, ON NR2 ENGINE RT T/R TRANSCOWL, AFT FAIRING WAS FOUND WITH A CRACK APPROX 2.45 INCHES IN LENGTH. (DISPOSITION WAS MADE TO PERFORM REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. PERMANENT REPAIR AS DECRIBED IN PART 2 WILL BE PERFORMED AT 15,0SDR UIEA2011060600292Stiffener · deformedDURING A C3-CHECK INSP, THE MLG W/W TOP PRESSURE DECK STIFFENERS AT BS 1393.5 & NBSP; LOWER FLANGE WERE FOUND DEFORMED AT RBL 46 AND RBL 45.5 RESPECTIVELY AS SHOWN ON FIG 1. AT BS1393.5 THE DEFORMATION IS APPROX BETWEEN RBL 44 AND RBL 48. THE WEB IS ALSO DEFSDR IPXA1B66281Floor Panel · damagedFLOOR PANEL DAMAGE AT STA 550 LBL 59. REPAIRED IAW EO B747-5320-42129-A.SDR KCSA11021Engine · leakingSMOKE IN FLT DECK & CABIN DURING CRUISE. DECLARED EMERGENCY AND DIVERTED TO EDDF. PERFORMED FIM TASK 21-00 TASK 810 & 71-03 TASK 854. FOUND OIL (ENG) IN TAIL PIPE. REMOVED & REPLACED THE NR 4 ENG IAW B747-400 MM 71-00-02, PERFORMED ENG TEST NR 7 IAW B747-4SDR IPXA1B65770Fire Loop · inoperativeEICAS MSG DET FIRE/OHT 3. REPLACED UPPER AFT LOOP ASSY (TS681), LOWER AFT LOOP ASSY (TS682) AND LOWER FWD LOOP ASSY (TS683) REF AMM 26-11-02-4. OPS CHECK GOOD.SDR UIEA2011032500164Skin · debondedDURING D2 CHECK INSP BEING PERFORMED; A DISBOND DAMAGE WAS FOUND TO THE RT WING OTBD T/E AFT FLAP UPPER PANEL INNER SKIN. DELAMINATION AREA WAS BETWEEN WING STATION, WBL 747.678 - 799.20 AND AS SHOWN IN FIGURE 2. (ALL DETAILS OF DAMAGE AND REPAIR DATA WERE RSDR IPXA1B65806Floor Support · corrodedINSPECTION TYPE:D, BULK CGO COMPT STA 1920 TO 2040 RBL 51" FLOOR PANEL SUPPORT FOUND CORROSION. CORROSION REMOVED & REPROTECTED IAW SRM 51-10-02 AND SRM 51-20-01, ORG: 0.050" BLENDED DEPTH: 0.003" WIDTH: 1" LENGTH: 2" WITHIN SRM 53-00-51. ALLOWABLE DAMAGE 1 FSDR IPXA1B65400Skin · misrepairedINSPECTION TYPE:C, RT WING OTBD FORE FLAP OTBD L/E AREA EXISTING REPAIR (NON STANDARD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5C.SDR IPXA1B65399Skin · misrepairedINSPECTION TYPE:C, RT WING OTBD AFT FLAP LOWER SURFACE T/E INBD AREA EXISTING REPAIR (NO REPAIR RECORD) REDO. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A, FIG 5, REV 58.SDR IPXA1B64004Skin · damagedFUSELAGE SKIN DAMAGED 14" AFT OF FWD LOWER CARGO DOOR. OPENED NR 338291 DUE TO MAJOR REPAIR. ALL WORK COMPLETED AND SIGNED FOR ON NR 338291. ITEM PLACED ON DEFERRAL FOR REPETITIVE INSP AS DESCRIBED IN EO B747-5330-40895A.
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