GE CF6-80 series

Service difficulty reports · 1,092

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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 = 'CF680'
  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 FDEA201012054583Skin · crackedLT WING, RIB 9, LOWER T/E SKIN HAS APPR 0.80" INCH CRACK FROM FASTENER HOLE TO T/E OF SKIN. REPAIRED IAW DWG R57340199 AND EA 6-5730-145507 INSTRUCTIONS.Dec 5, 2010 · N660FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201012054584Skin · crackedRT WING, RIB 9 LWR T/E SKIN PANEL HAS A CRACK APPROX 0.080", NDT VERIFIED CRACK TO BE APPROX .5" INCH LONG. REPAIRED RT WING SKIN IAW WITH DWG NR R57340199 AND EA 6-5730-145507 INSTUCTIONS.Dec 5, 2010 · N660FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201012054585Crossbeam · crackedMDC FLOORBEAM AT FRAME 60 HAS 1250" CRACK ON AFT FACE OF VERTICLE ANGLE, BETWEEN SEAT TRACK 4R AND 5R. BLENDED OUT CRACK DAMAGE AND REPAIRED FLOOR BEAM AT FR 60 BETWEEN SEAT TRACKS 4R AND 5R IAW SRM 53-10-15, PB 201, FIG 211.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201012054586Seat Track · corrodedMDCC SEAT TRACK 6L BETWEEN FR22 TO FR 4 HAS APPR 2" SQ INCHES OF EXFOLIATION CORROSION. REPAIRED SEAT TRACK 6L BETWEEN FR22 AND FR24 IAW 300/600 SRM 53-10-16, FIG 101.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054587Seat Track · corrodedMDCC, SEAT TRACK 6R HAS CORROSION BETWEEN FR30 AND FR32, SEAT TRACK 6R AT FR32 HAS A DOUBLE DRILL HOLE. CUT OUT SEAT TRACK FROM FR29 TO FR33, REPAIRED SEAT TRACK IAW SRM 53-10- 16 FIG 208.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054588Seat Track · corrodedMDCC SEAT TRACK 5L ALONG FR27 HAS CORROSION APPR .25" INCH ON OTBD FLANGE. REMOVED DAMAGED SEAT TRACK 5L SECTION BETWEEN FR26.5 AND FR 31.5 AND REPAIRED SEAT TRACK 5L IAW FREIGHTER SRM 53-10-16, PB 204, 205, 208, FIG 201.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054589Seat Track · corrodedMDCC, SEAT TRACK FLANGE 3R AT FR45 HAS APPROX 12" OF CORROSION. R & R SEAT TRACK 3R BETWEEN FR44 AND FR50 IAW SRM 53-10-16, FIG 203, PG 211/212.Dec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012054590Seat Track · wornAFT CARGO FR54 TO 54.2 DUMMY TRACK RT NR2 EXCEEDS MINIMUM GAP VALUE (0.0350) IAW EO6-5310-7- 3322B, PT1, PG5, STEP11I. REMOVED DUMMY TRACK 2R FROM AFT CARGO FR54 TO 54.2 IAW SRM 51-40-21, PAR 7. REMOVED 12EA BRACKETS FROM THE OLD DUMMY TRACK 2R AND INSTALLEDec 5, 2010 · N660FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR UIEA2010120300184Torque Tube · shearedDURING WALKAROUND INSP, MX FOUND THE MED L1 - UPPER TORQUE TUBE ASSY SHEARED. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS; SCHEDULE REPEAT INSPECTIONS AT EVERY 5 FC (FLIGHT CYCLES) AND PERMANENT REPAIR PRIORDec 3, 2010 · N493MC · Boeing 74747UF · Passenger/Crew DoorsSDR FDEA201012034563Floor Support · corrodedFLOOR SUPPORT STRUCTURE, Y 450, HAS CORROSION FROM 6" INCHES AFT OF FR 14 TO 8" INCHES FWD OF FR 14 ON THE TOPSIDE. R & R FLOOR SUPPORT STRUCTURE Y450, FROM FR 11TO FR 15A IAW SRM 51-72-10, PAGES 1-3.Dec 3, 2010 · N443FE · Airbus A310 · Fuselage Miscellaneous StructureSDR FDEA201012034564Crossbeam · crackedCROSSBEAM BETWEEN Y 953 AND Y 450 AND FR 14 AND FR 15A HAS A 1" INCH CRACK ON TOPSIDE. R & R CROSSBEAM BETWEEN Y953 AND Y450 AND FR14 AND FR15A IAW SRM 51-72-10 PAGE 1-3.Dec 3, 2010 · N443FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201012034565Crossbeam · corrodedFWD CROSSBEAM IN REAR FUSELAGE AT FR 85 AND STRINGER 13R HAS 1" INCH OF CORROSION ON TOPSIDE. R & R CROSSBEAM AT FR 85 AND STR 13R IAW SRM 51-40-21, PAR.7.Dec 3, 2010 · N443FE · Airbus A310203 · Fuselage Main, StructureSDR FDEA201012034566Floorbeam · corrodedAFT CARGO FLOORBEAM TOP CHORD FR 60 RT SIDE HAS CORROSION ON BOTTOM, ABOUT 58" FROM CENTERLINE,AND ABOUT 1" LONG X .5" WIDE. R & R ANGLE IN AFT CARGO COMPARTMENT AT FR 60, RT SIDE IAW SRM 51-40-21, PAR 6.Dec 3, 2010 · N443FE · Airbus A310203 · Fuselage Main, Floor BeamSDR FDEA201012034567Skin · crackedTAILCONE HAS A CREASE WITH A DEPTH OF .010", AND A LENGTH OF 0.375", LOCATED BETWEEN FR 96 AND FR 97, BETWEEN STR 2R AND STR 3R. NDT CHECK COMPLIED WITH AND FOUND A CRACK (.375") IAW NTM 51-10-08. CUT OUT DAMAGED SECTION OF TAILCONE AND REPAIRED TAILCONE SKIDec 3, 2010 · N443FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201012034568Skin · cracked.5" INCH CRACK ON TAILCONE SKIN, BETWEEN FR 96 AND FR 97 AND BETWEEN STR 4R AND STR 5R. CUT OUT DAMAGED AREA WEB AND SKIN AREA BETWEEN FR 96 AND FR 97 AND BETWEEN STR 4R AND STR 5R, REPAIRED TAILCONE SKIN IAW SRM 53-19-12, FIG 202, USING WEB FILLER AND WEBDec 3, 2010 · N443FE · Airbus A310203 · Fuselage Main, Plate/SkinSDR FDEA201012034569Beam · corrodedL-2 DOOR, AT BEAM 1 SEGMENT AT FR 74, HAS 2" SQUARE CORROSION ON AFT SIDE. REPAIRED L-2 DOOR SEGMENT AT BEAM 1 IAW DWG NR A52175214 AMD SRM 51-40-21, PAR 6.Dec 3, 2010 · N443FE · Airbus A310203 · Passenger/Crew DoorsSDR FDEA201012034570Seat Track · corrodedMAIN CARGO DECK, RT SEAT TRACK 5R, FROM FR 14 TO FR 18 HAS EXFOLIATED CORROSION. R & R SEAT TRACK 5R, Y-1959, FROM FR 14 TO FR 18 IAW SRM 51-72-10, PAGE 1-3.Dec 3, 2010 · N443FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012034555Light · inoperativeR-1 EMERGENCY LIGHT INOP. INSTALLED LWR PORTION ON RT DOOR ARTICULATING SLIDING CEILING PANEL AND EMERGENCY EXIT LIGHT REF EA 1-5210-146019 AND MM 25-23-23-4. LIGHT OPS CHECKED NORMAL. REF WRI 52-10-6451 FOR REPLACEMENT OF UPPER PORTION OF PANEL AND WRI 52-1Dec 3, 2010 · N614FE · Doug MD11F · Emergency LightingSDR FDEA201012024545Stringer · corrodedCORROSION ON STR 44L ABOUT 10 IN AFT OF FR58 , 1 IN IN DIAMETER, REMOVED CORROSION FROM STR 44L IAW SRM 51-74-10 , CHECKED LIMITS IAW SRM 53-10-14, PAGE 202. FOUND TO BE OUT OFF LIMIT, REPAIRED STR 44L IAW SRM 53-10-14, FIG 201.Dec 2, 2010 · N443FE · Airbus A310203 · Fuselage Main, Longeron/StringerSDR FDEA201012024546Seat Track · corrodedAFT MDCC SEAT TRACK NR3 (-Y953) HAS CORROSION AT 7.5 INCH FWD OF FRAME FR 55/58 TO 10.5 INCH AFT OF FR 55/58 ABOUT 72 SQ IN. REMOVED CORROSION FROM SEAT TRACK SEC 55/58 IAW SRM 51-74-10, PAGE 210. CHECKED LIMITS. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, Dec 2, 2010 · N423FE · Airbus A310203 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201012014530Pressure Switch · failedDUE TO ENG NR 3 FUEL FILTER AND MASTER CAUTION LIGHT . SPEED 50 KTS. NO MAX BREAKING RECEIVED. R & R FUEL FILTER PRESSURE SWITCH.Dec 1, 2010 · N610FE · Doug MD11F · Engine Fuel DistributionSDR HALA2010120100580Skin · corrodedLEVEL 2 CORROSION AT FUSE, RT SIDE SECTION 45, SKIN AROUND WINDOW FRAMES, AT THE FOLLOWING LOCATIONS CORRODED. WINDOW 5R, 6R, 8R, 9R, 10R, 12R, 14R, AND 15R. CORROSION REMOVED, AREA ALODINED AND PAINT PROTECTED, IAW SRM 51-20-01.3, REV 84 AND AMM 51-25-10, REDec 1, 2010 · N596HA · Boeing 767332 · Fuselage Main, Plate/SkinSDR DALA1034481504Wire · brokenEMERGENCY LIGHTS ROW 20FG THROUGH 28FG ARE INOPERATIVE. MX REPLACED THE BATTERY PACK, CHARGER, AND REPAIRED A BROKEN WIRE AT SET 20FG. SYS OPS IS NORMAL.Nov 30, 2010 · N154DL · Boeing 7673P6 · Light System WiringSDR DALA1034451701Skin · damagedUPPER SKIN DAMAGE LT WING AFT MAIN FLAP 8 " FROM INBD SIDE. REPAIRED IAW SRM 57-53- 01 REPAIR 1 AND SRM 51-70-10.Nov 29, 2010 · N171DZ · Boeing 767332 · Trailing Edge FlapsSDR FDEA201011294506Seat Track · corrodedMAIN DECK CARGO - UPON REMOVAL OF FLOOR PANELS FOR CORRODED FERRULES. REPLACEMENT FOUND SEAT TRACK X=75 FROM STA 1861 TO 1871 INBD AND OTBD FLANGES CORRODED. REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STATION 1751 TO STATION 1887 X= 75 AS PER SRM Nov 29, 2010 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR HALA2010112900579Skin · corrodedLEVEL 2 CORROSION, FUSE STATION 390, RT SKIN AROUND WINDOW FRAMES AT THE FOLLOWING LOCATIONS CORRODED, AT WINDOWS 16R, 17R, 18R, 19R, 20R, 21R, 24R, & 28R. CORROSION REMOVED, AREA IODINED AND PAINT PROTECTED, IAW SRM 51-20-01, REV 54, AND AMM 51-21-10 REV102.Nov 29, 2010 · N596HA · Boeing 767332 · Fuselage Main, Plate/SkinSDR FDEA201011274499Seat Track · corrodedMAIN DECK CARGO - UPON REMOVAL OF FLOOR PANEL FOR SLANT PANEL INSPECTION ACCESS FOUND SEAT TRACK STATION 1531 TO STATION 5-33, X= -8 INBOARD FLANGE WITH MULTIPLE SURFACE CORROSION. MAIN DECK CARGO - CORRODED SEAT TRACK AT STATION 1531 TO STATION 5-33 X= -8Nov 27, 2010 · N602FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011274500Skin · damagedMAIN DECK CARGO DOOR LOWER MID CUT OUT AT STA 695 TO STA 700, LONGERON 27 LT FOUND CHIPPED. MAIN DECK CARGO DOOR LOWER MID CUT OUT AT STATION 695 TO STATION 700 LONGERON 27LT, CHIPPED AREA REPAIRED AS PER E.A. 1-5310-143493. REPAIR CLASSIFIED AS MINOR AS PENov 27, 2010 · N602FE · Doug MD11F · Fuselage Main, Plate/SkinSDR FDEA201011254487Smoke Detector · dirtyAIR TURN BACK FOR "AVIONICS SMOKE" ECAM. NO EMERGENCY DECLARED. FOUND WATER IN AVIONICS SMOKE DETECTOR. R & R AVIONICS SMOKE DETECTOR AS REQUIRED. OPS CHECK GOOD REF MM 26-15-12-04-0. PREMATURE REMOVAL/INSTALLATION. NOTE: PREV WRITE UP AT GATE - WATER CLNov 25, 2010 · N673FE · Airbus A300F4605R · Fire DetectionSDR UIEA2010112500183Web · crackedDURING WALK AROUND INSP, DAMAGE TO THE LOWER AFT CARGO COMPARTMENT - BS1850, LBL45.5 FLOOR WEB - CRACK/DAMAGE WAS FOUND MEASURING 2.0 IN. X 4.450 IN. (REF FIGURE 1). (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONov 25, 2010 · N408MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR FDEA201011254489Skin · crackedHFEC OPEN HOLE INSPECTION CARRIED OUT ON RT WING ON PSE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. FOUND 15 EA HOLES WITH CRACK INDICATIONS. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MNov 25, 2010 · N602FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201011254490Access Panel · crackedHFEC OPEN HOLE INSP CARRIED OUT ON LT WING ON PSE LOWER SKIN PANEL OUTER WING ACCESS DOOR CUTOUT AT BETWEEN STA XORS= 683.4 AND XORS= 713.6. FOUND 05 EA HOLES WITH CRACK INDICATION. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR INov 25, 2010 · N602FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201011244484Battery Pack · inoperativeLEVEL 1 'EMER LT BAT 6 LO' ALERT DISPLAYED DURING EMERGENCY LIGHT TEST. R & R AFT EMERGENCY LIGHT BATTERY PACK (U1-2070) REF AMM 33-51-01-4-0. OPS CHECKS NORMAL.Nov 24, 2010 · N587FE · Doug MD11F · Emergency LightingSDR FDEA201011224464Power Supply · failedDURING MAINT"A"CHECK, EMERGENCY LIGHT TEST FAILED WITH "EMER LT BAT LO" ALERT ON DISPLAY. MX R & R EMERGENCY BATTERY POWER SUPPLY IAW AMM 33-51-01-4 TEST PASSED AMM 33-51-01-5.Nov 22, 2010 · N592FE · Doug MD11F · Emergency LightingSDR DALA1034151503Wire Harness · damagedEMERGENCY LIGHT AT 35B IS INOPERATIVE. MX RE-PINNED THE HARNESS. SYS OPERATION IS NORMAL.Nov 22, 2010 · N153DL · Boeing 7673P6 · Light System WiringSDR DALA1034161503Wire Harness · damagedEMERGENCY LIGHTS AT SEAT 14B WERE INOPERATIVE. MX RE-PINNED THE HARNESS. SYS OPS IS NORMAL.Nov 22, 2010 · N153DL · Boeing 7673P6 · Light System WiringSDR DALA1034141611Connector · dirtyON FINAL APPROACH F/A REPORTED ELECTRIC ODOR IN FORWARD GALLEY. UTILITY BUSES TURNED OF AND GALLEY CIRCUIT BREAKER PULLED. ODOR DISAPPEARED. IN CONSULT WITH MCC OVENS SN DL626 AND DL259 WERE REMOVED AND ELECTRIC CONNECTORS CLEANED. SYS OPS IS NORMAL.Nov 20, 2010 · N1611B · Boeing 767332 · Electrical Power System WiringSDR FDEA201011194427Valve · failedREJECTED TAKEOFF AT 60 KNOTS DUE TO ECAM MESSAGE- NR2 REVERSER PRESSURIZED. R & R NR 2 ENG PRESS REGULATING AND SHUTOFF VALVE REF MM 78-31-05-04.DUE TO REJECTED TAKEOFF. C/W HIGH PWR ENG RUN REF JRH CH 7 CKS GOOD.Nov 19, 2010 · N650FE · Airbus A300F4605R · Engine Thrust ReverserSDR IPXA0M63640Battery Pack · inoperativeEMERGENCY LIGHT TEST FAIL BAT 1 LO MSG, ITEM TRANSFERRED TO M439552 IAW MEL 33-50-4. R & R EMER BATTERY PACK IAW AMM 33-51-01. OPS CK NORMAL. THIS CLEARS M439552.Nov 18, 2010 · N256UP · Doug MD11F · Emergency LightingSDR HALA2010111600542Unknown · unknownETOPS SIGNIFICANT SYS - APU FAULT. PERFORMED FIM 49-11-00, FIG 103. BITE CHECKED APU ECU NO FAULTS NOTED. NO MINI FLAGS. STARTED APU 1ST ATTEMPTED SUCCESSFUL NO DEFECTS NOTED. OK FOR SERVICE.Nov 16, 2010 · N597HA · Boeing 767332 · Airborne Auxiliary Power Unit (APU) SystemSDR IPXA0663603Skin · dentedNR5 SLAT (LT WING) HAS L/E DENTS. SKIN CUTOUT MEASURES 8.3 X 7.2 REF D -437285. REPAIRED IAW EO B767-5750-40211-B.Nov 15, 2010 · N313UP · Boeing 76734AF · Trailing Edge FlapsSDR UIEA2010111300179Skin · crackedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE FUSELAGE SKIN AT BS 2600 BELOW STRINGER 42R, CONSISTING IN A CRACK, MEASURING 0.250 IN. LONG. THE DAMAGE IS BEYOND THE ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-01, FIG 101 (ALLOWABLE DAMAGE 1). (DISPOSITION WAS MADNov 13, 2010 · N493MC · Boeing 74747UF · Fuselage Main, Plate/SkinSDR IPXA0M63608Cover · misinstalledL1 DOOR SLIDE COVER DOES NOT PROPERLY STOW. RE-INSTALLED DOOR COVER AND CHECKED CONDITION - SATISFACTORY.Nov 12, 2010 · N255UP · Doug MD11F · Escape SlideSDR FDEA201011104295Flange · crackedENG 1 RT T/R COWL FWD RING FLANGE GOT CRACK AT UPPER EDGE. ACCOMPLISHED WORK IAW DWG NR:SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 10, 2010 · N665FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201011104297Rib · crackedLT WING T/E AREA, 1EA RIB CRACKED POSITION UNDER NR5 SPOILER INBD SIDE. FABRICATE NEW PART IAW DWG A-57240194. REPLACE NEW PART IAW SRM 51-72-10 AND 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 10, 2010 · N665FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201011104299Frame · damagedDURING REMOVING FRAME, FOUND FRAME FOOT 1 EA ENLARGE HOLE LOCATED POSITION B. ENLARGED HOLE AREA, TRIM OUT IAW EO 6-5310-7-5006, PT1, FIG 8.Nov 10, 2010 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201011104300Frame · crackedLT SIDE FR44 BETWEEN STGR 25 AND STGR 26 HOLE B WAS FOUND CRACK INDICATION OV ER 100 PERCENT FSH. DEPTH OF CRACK INDICATION IS 3MM AT FRAME LAYER. REPLACED WITH NEW FRAME SECTION (PN A5381231020001) IAW AB6F SRM 51-72-10, 51-40-20.Nov 10, 2010 · N665FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201011104301Skin · crackedRT WING SPOILER SHROUD SUPPORT SKIN GOT CRACK ABOUT .2500" BELOW NR 5 SPOILER INBD EDGE. FABRICATE NEW PART IAW DWG A-57240194. REPLACE NEW PART IAW SRM 51-72-10, 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.Nov 10, 2010 · N665FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201011104296Shim · migratedRT WING NR6 FLAP TRACK FRONT CARRIAGE UPPER BRIDGE INBD SHIM MIGRATED IAW EA6-2750-141649, REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Nov 10, 2010 · N665FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201011104298Shim · migratedRT WING T/E NR4 FLAP FRONT CARRIAGE UPPER BRIDGE BOTH SIDE SHIM EXTRUDED IAW EA6-2750-141649, REPAIR ACCOMPLISHED IAW GMM 6-2-100. REPAIR CLASSIFIED AS MINOR.Nov 10, 2010 · N665FE · Airbus A300F4605R · Leading Edge Devices
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