GE CF6-80C2B6F

Service difficulty reports · 1,456

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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.

SDR IPXA10663050Intercostal · crackedINSPECTION TYPE:C, M/DECK STA 1043 LBL 11 TO RBL 11 INTERCOSTAL FOUND CRACKED. MAIN DECK STA 1043 LBL 11 TO RBL 11 FLOOR INTERCOSTAL REPLACED AFTER FABRICATED IAW HX RS R53-00-36841 AND EO B767-5320-40037, ORG MATL BAC1518-790-7075T6511. FABRICATE NEW INTERCOSep 21, 2010 · N305UP · Boeing 76734AF · Fuselage Miscellaneous StructureSDR CA100922008Motor · seizedBOTH WEATHER RADAR SYS FAILED AFTER TAKEOFF, ENROUTE. FLIGHT DIVERTED AND DURING TROUBLESHOOTING IT WAS IDENTIFIED THAT THE WEATHER ANTENNA SWEEP MOTOR, COMMON TO BOTH SYS, WAS SEIZED. THE ANTENNA WAS REPLACED AND BOTH SYSTEMS WERE GROUND FUNCTIONED SERVICEASep 21, 2010 · Boeing 767375 · Weather Radar SystemSDR DALA1022601704Charger · inoperativeEMERGENCY ESCAPE PATH LIGHTS AT 33B ARE INOPERATIVE. MX REPLACED BATTERY CHARGER AND REPAIRED WIRES. SYS OPS IS NORMAL.Sep 11, 2010 · N174DZ · Boeing 767332 · Emergency LightingSDR IPXA10662475Eadi · inoperativeBOTH CAPT AND F/O EADI BLANKED AFTER T/O. EADI S/G CB RESET, E/E COOLING TEST, EFIS TEST AND CHECKED DISPLAY UNIT COOLING SCREEN, ALL COND NORMAL.Sep 10, 2010 · N316UP · Boeing 76734AF · Navigation SystemSDR IPXA10662594Floor Panel · damagedINSPECTION TYPE:C, MCD STA 540 TO 654+22 RBL 55" TO RBL 77" FLOOR PANEL FOUND 1 DAMAGE & 10 DENT MARKS, FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662595Floor Panel · damagedINSPECTION TYPE:C, MCD STA 412 TO 540 LBL 11" TO RBL 11" FLOOR PANEL FOUND 1 DAMAGE & 9 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662596Floor Panel · damagedINSPECTION TYPE:C, MCD STA 412 TO 550 LBL 77" TO LBL 89" FLOOR PANEL FOUND 3 DAMAGES & 15 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662597Floor Panel · damagedINSPECTION TYPE:C, MCD STA 412 TO 540 RBL 33" TO RBL 55" FLOOR PANEL FOUND 1 DAMAGES & 7 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662598Floor Panel · damagedINSPECTION TYPE:C, MCD STA 1331 TO 1480 LBL 77" TO LBL 89" FLOOR PANL FOUND 1 DAMAGE & 10 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10662599Floor Panel · damagedINSPECTION TYPE:C, MCD STA 1480 TO 1599 RBL 33" TO RBL 55" FLOOR PANEL FOUND 1 DAMAGE & 8 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.Sep 7, 2010 · N331UP · Boeing 76734AF · Fuselage Floor PanelSDR DALA1021831704Fuse · inoperativeEMERGENCY LIGHTS AT SEATS 32AB THROUGH 39AB ARE INOPERATIVE. MX REPLACED FUSE M9010. SYS OPS IS NORMAL.Sep 4, 2010 · N174DZ · Boeing 767332 · Emergency LightingSDR CA100907003Relay · failedJUST OVER 6 HRS AFTER DEPARTURE, CREW REPORTED THERE WERE NO SERVICABLE LAVS AND THERE WAS A STRONG ELECTRICAL BURNING ODOR FROM ONE OF WASHROOMS. CREW DECLARED AN EMERGENCY AND DIVERTED. VISUAL INSP CARRIED OUT BEHIND ALL LAV PANELS. NO INDICATION OF ANY DSep 4, 2010 · Boeing 767333 · AC Power Distribution SystemSDR CNMA20100029Structure · damagedON POST FLIGHT WALKAROUND INSP, FOUND RT STRUT GEAR DOOR DETATCHED FROM MOUNTS AND DAMAGED ALSO CAUSING DAMAGE TO TRUNNION DOOR. SHOCK STRUT DOOR & TRUNNION DOOR REPLACED REF SAL MX ORDER 152030292C4-0010 FOR WORK PERFORMED AND CERTIFICATION FOR RTS IAW LOG.Aug 29, 2010 · N342AX · Boeing 767328 · Landing Gear DoorsSDR IPXA10662140Skin · gougedRT SIDE FUSELAGE SKIN GOUGED AFT OF FWD LOWER CARGO DOOR AT STA 610R AND BETWEEN STRINGERS S30 & S29 RT. ACCOMPLISHED PERMANENT REPAIR OF SKIN DAMAGE AT STA 612 RT AND BETWEEN STRINGERS S30 AND S29 RT IAW SRM 53-00-15-1A-1, FIG 101, DETAIL II.Aug 25, 2010 · N337UP · Boeing 76734AF · Fuselage Main, Plate/SkinSDR IPXA10661875Sign · damagedINSPECTION TYPE:PS1, EMERGENCY EXIT LIGHT ASSY TABS TO HOLD LIGHT COVER ON WORN. R & R EMERGENCY LIGHT ASSY IAW MM 33-51-01-2.Aug 14, 2010 · N330UP · Boeing 76734AF · Emergency LightingSDR IPXA0661952Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATED FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5, REV 47.Aug 9, 2010 · N332UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA0661953Skin · delaminatedINSPECTION TYPE:C, LT WING NR1 SPOILER PANEL UPPER SURFACE DELAMINATED. GRAPHITE FABRIC WET LAY UP REPAIR CARRIED OUT IAW SRM 51-70-17, PAR 4A (1) FIG 10, REV 47.Aug 9, 2010 · N332UP · Boeing 76734AF · SpoilersSDR IPXA0661954Wedge · misrepairedINSPECTION TYPE:C, NON-STANDARD REPAIR ON LT WING NR1 SLAT UPPER SURFACE INBD T/E WEDGE AREA. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R REPAIR 4, FIG 202, SHEET 1, REV 47.Aug 9, 2010 · N332UP · Boeing 76734AF · Leading Edge DevicesSDR DALA1018611706Connector · damagedEMERGENCY PATH LIGHT AT SEAT 30A IS INOPERATIVE. MX RE-CRIMPED CONNECTOR PLUG. SYS OPS IS NORMAL.Aug 7, 2010 · N176DZ · Boeing 767332 · Light System WiringSDR IPXA10661903Floor Panel · dentedINSPECTION TYPE:C, MCD STA 283 TO 412, RBL 77 TO RBL 89 FLOOR PANEL FOUND 1 GROOVE MARK AND 4 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Aug 7, 2010 · N332UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661904Floor Panel · damagedINSPECTION TYPE:C, STA 654+22 TO 676 LBL 11 TO RBL 11 FLOOR PANEL FOUND 2 DAMAGE AND 13 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.Aug 5, 2010 · N332UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661445Floor Panel · damagedONE INCH HOLE IN MCD FLOOR POS 4R 2ND PANEL FROM EDGE. REPAIRED IAW SRM 50-00-5002R.Aug 2, 2010 · N334UP · Boeing 767300 · Fuselage Floor PanelSDR IPXA10661447Floor Panel · damagedPOS 11L, FLOOR PANEL DAMAGED. REPAIRED IAW SRM 53-00-50-2R.Aug 2, 2010 · N334UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661455Control Panel · inoperativeINSPECTION TYPE:E, TOP ENG ANTI ICE SELECTED AND SWITCH WOULD NOT STAY DEPRESSED. R & R KERRY SWITCH FOR RT ENG A/I, NO HELP. R & R ANTI ICE CONTROL PANEL, ROBBED PANEL REF MM 30 11 01, 4 MFG SWPM 20 84 18.Aug 1, 2010 · N331UP · Boeing 76734AF · Airfoil Anti/De-ice SystemSDR DALA1017791606Connector · disconnectedSEAT MOUNTED EMERGENCY PATH LIGHTS AT 26FG ARE INOPERATIVE. MX FOUND (1) WHITE EMERGENCY PATH LIGHT SIDE WALL PLUG DISCONNECTED. RECONNECTED PLUG, SYS OPS IS NORMAL.Jul 26, 2010 · N16065 · Boeing 767332 · Light System WiringSDR DALA1017811603Wire · looseEMERGENCY LIGHT AT 16G HAS LOOSE WIRE AT WALL CONNECTOR. MX REPLACED CONNECTOR. SYS OPERATION IS NORMAL.Jul 25, 2010 · N1603 · Boeing 767332 · Light System WiringSDR IPXA10661193Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP L/E FOUND DELAMINATION COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05, PAR 5A (1) FIG 5.Jul 14, 2010 · N330UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10661049Lamp · inoperativeLT EXTERIOR EMERGENCY LIGHT FOUND INOP DURING MX INSP PS1 CHECK ITEM. CORRECTED BY REPLACING THE LAMP; OPS CHECKS NORMAL.Jul 10, 2010 · N339UP · Boeing 76734AF · Emergency LightingSDR IPXA10660955Floor Panel · damagedINSPECTION TYPE:C, MCD STA 985 TO 1087, LBL 77 TO LBL 88, FLOOR PANEL FND 1 DAMAGED & 7 DENT MARKS. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G & REINSTALLED IAW AMM 53-01-01.Jun 28, 2010 · N301UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10661040Skin · misrepairedINSPECTION TYPE:C, RT WING INBD AILERON EXISTING REPAIR PATCH NOT IAW SRM 57-60-01-2R1, TABLE 3, NOTE G. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT EXISTING REPAIR PATCH AREA IAW EO B767-5750-38681 AND RS R57-60-36772.Jun 25, 2010 · N301UP · Boeing 76734AF · AileronsSDR CA100701003Engine · failedRIGHT ENGINE SURGE AFTER T/O. ENGINE NOISE, VIBRATION AND N1 INDICATION WAS ALSO SURGING. EGT WAS CONTROLLABLE WITH THRUST LOWER N1. REDUCED ENGINE POWER TO 75 PERCENT N1 AND RETURNED TO THE DEPARTURE AIRPORT. THE ENGINE APPEARS TO HAVE HAD A FAILURE AND LJun 14, 2010 · Boeing 767375 · Engine (Turbine/Turboprop)SDR DALA1012620175Brake Assy · failedNR 7 MAIN BRAKE ASSY SHATTERED ON LANDING. PARTS RECOVERED. ACFT TOWED TO GATE REM/REP NR7 BRAKE ASSY IAW AMM 32-41-08. INSPECTED AXLE NO FURTHER DAMAGE NOTED. (DL76G101457)Jun 10, 2010 · N175DZ · Boeing 767332 · Landing Gear Brake SystemSDR IPXA10660383Hmu · malfunctionedINSPECTION TYPE:E, TOP IFSD - DIVERSION - AT CRUISE NR1 ENG LOST POWER. NO PRIOR INDICATION OR WARNINGS. COMPLETED ALL CHECKLISTS, DECLARED EMERGENCY AND DIVERTED TO RFD. MADE A SINGLE ENG LANDING WITH NO PROBLEMS. T/S PER FIM 71-05-00 FIG 104. OPS TEST OF FUJun 9, 2010 · N339UP · Boeing 76734AF · Fuel Controlling SystemSDR IPXA10660174Rib · crackedINSPECTION TYPE:C, LT WING L/E LES 160 FIXED FAIRING UPPER SUPPORT RIB FRONT SPAR SUPPORT ANGLE FOUND CRACKED CRACK .2500" IN LENGTH. LT WING L/E LES 160 FIXED FAIRING UPPER SUPPORT RIB FRONT SPAR SUPPORT ANGLE REPLACED AND INSTALLED IAW SRM 51-10-02 AND 51-May 25, 2010 · N317UP · Boeing 76734AF · Wing, Rib/BulkheadSDR IPXA10660175Hinge Fitting · crackedINSPECTION TYPE:7C, LT WING INBD MAIN FLAP INBD HINGE FITTING FLANGE FOUND CRACKED. LT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02- 2R1, FIG 201, REV 47. ORG MAT'L IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 1.5" AND OTBD FLANGMay 24, 2010 · N317UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660176Hinge Fitting · crackedINSPECTION TYPE:7C, RT WING INBD MAIN FLAP INBD HINGE FITTING FLANGE FOUND CRACKED. RT WING INBD MAIN FLAP HINGE FTG AT IFS179.75 REPAIRED IAW SRM 57-53-02- 2R1, FIG 201, REV 47. ORG MAT'L IS 7075T73 FORGING, CRACK LENGTH AT INBD FLANGE IS 0.6" AND OTBD FLANMay 24, 2010 · N317UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10660200Skin · crackedINSPECTION TYPE:C, LT WING NR 3 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR3 SLAT INBD AT OSS723.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1375 DAMAGED CUTOUT IS 0.468" DIA THIS IS CMay 24, 2010 · N317UP · Boeing 76734AF · Wing, Plate/SkinSDR IPXA10660201Skin · crackedINSPECTION TYPE:C, LT WING NR3 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 3 SLAT L/E OTBD AT OSS792.5 NOSE SKIN REPAIRED IAW RS R57-00-36739, EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1255", DAMAGED CUTOUT IS 0.468" DIA, THMay 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660204Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E INBD AT OSS572.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1845", DAMAGED CUTOUT IS 0.500" DIAMay 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660205Skin · crackedINSPECTION TYPE:C, RT WING NR 9 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 9 SLAT L/E OTBD AT OSS641.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRK LENGTH IS 0.1460", DAMAGED CUTOUT IS 0.500" DIA,May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660206Skin · crackedINSPECTION TYPE:C, RT WING NR 10 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E INBD AT OSS723.9 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1625", DAMAGED CUTOUT IS 0.500" May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10660207Skin · crackedINSPECTION TYPE:C, RT WIING NR 10 SLAT OTBD NOSE SKIN RIVET HOLE FOUND CRACKED. RT WING NR 10 SLAT L/E OTBD AT OSS792.5 NOSE SKIN REPAIRED IAW RS R57-00-36739 AND EO B767-5750-38009, ORG MATL IS 7075T6-0.063", CRACK LENGTH IS 0.1440, DAMAGED CUTOUT IS 0.500" May 24, 2010 · N317UP · Boeing 76734AF · Leading Edge DevicesSDR IPXA10659995Floor Panel · damagedD418763 MCD FLOOR PANEL DAMAGED AT POSITION 10L MFG AND INSTALLED IAW EO B767-4320-9693-G, POS 10L.May 23, 2010 · N320UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659874Floor Panel · puncturedMAIN CARGO POSITION 6L MOST OTBD FLOOR PANEL HAS 2 SMALL PUNCTURES. 2 SMALL PUNCTURES IN ZONE 1 THROUGH FIRST PLY ONLY. FIRST MEASURES .5" BY .1280", SECOND MEASURES .5" BY .2500" AND ARE 4 INCHES APART FROM EACH OTHER. ACCOMPLISHED MAJOR REPAIR IAW EO B76May 15, 2010 · N309UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659748Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT POS 6 L HAS .6250 X .2500 HOLE. REPAIRED IAW SRM 53-00-50-22R.May 10, 2010 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659749Floor Panel · damagedMAIN CARGO DECK FLOOR AT POS 6L HAS 1" HOLE IN IT. REPAIRED IAW SRM 53-00-50-2R.May 10, 2010 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659893Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP MID L/E FAIRING INBD AREA DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5C, FIG 2.May 10, 2010 · N303UP · Boeing 76734AF · Trailing Edge FlapsSDR IPXA10659938Stringer · misrepairedINSPECTION TYPE:C, FUSELAGE STA524 STR25L EXISTING REPAIR MUST BE REMOVED AND REACCOMPLISHED IAW SRM. GIVEN IN VALIDATION EO B767-5100-36544 APPENDIX B ITEM 1 FX AT BTN BS511.5 & 532.5 STR25L STR REPAIRED IAW R53-00-36725 & EO B767-5330-37838, ORG MATL 7075T6 May 10, 2010 · N303UP · Boeing 76734AF · Fuselage Main, Longeron/StringerSDR IPXA10659735Floor Panel · puncturedMAIN CARGO DECK FLOOR PNL AT POS 12L OTBD HAS 1 1/4 X 1 HOLE THUR BOTH SKINS FABRICATED PNL IAW EO B767-5320-9693-G.May 9, 2010 · N317UP · Boeing 76734AF · Fuselage Floor PanelSDR IPXA10659736Floor Panel · damagedINSPECTION TYPE:N/A MAIN CARGO DECK FLOOR PANEL HAS 2 HOLES. HOLES MEASURES 6.7500 X 3.5 AN D 3.5 DIAMETER. REPAIRED IAW SRM 53-00-50.May 9, 2010 · N317UP · Boeing 76734AF · Fuselage Floor Panel
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