Douglas DC-10-30F

Service difficulty reports · 1,152

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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 aircraft_model_key = 'DC1030F'
  ORDER BY difficulty_date DESC"

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SDR G60A200800009Support · corrodedFOUND CORROSION NOSE WHEEL WELL JAM SUPPORT AT STATION 541 AND 547.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Miscellaneous StructureSDR G60A200800007Skin · corrodedFOUND CORROSION ON FUSELAGE SKIN FS 1942-2163.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Main, Plate/SkinSDR G60A200800003Floor Support · corrodedFOUND CORROSION AFT CARGO FLOOR ANGLE.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Miscellaneous StructureSDR G60A200800010Door Frame · corrodedFOUND CORROSION NOSE WHEEL WELL DOOR JAM STRUCTURE, SHELF.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Main, StructureSDR G60A200800006Pulley Bracket · corrodedFOUND CORROSION CENTER FUEL TANK AFT SIDE FUEL VALVE PULLEY BRACKET.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Miscellaneous StructureSDR G60A200800005Floor Support · corrodedFOUND CORROSION ON BULK CARGO FLOOR SUPPORT RAIL.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Miscellaneous StructureSDR G60A200800004Frame · corrodedFOUND CORROSION ON FRAME.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Main, FrameSDR G60A200800002Seat Track · corrodedFOUND CORROSION ON SEAT TRACK IN FRONT OF AFT CARGO DOOR.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR G60A200800001Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM LBL 5 STATION 1781.Feb 7, 2008 · N606GC · Doug DC1030F · Fuselage Main, Floor BeamSDR FDEA200802050350Skin · crackedLT WING INBOARD FLAP ON UPPER SKIN FOUND CRACK. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I.Feb 5, 2008 · N306FE · Doug DC1030F · Trailing Edge FlapsSDR 08FDEA00356Fitting · crackedACCOMPLISHED AN INITIAL BHEC INSPECTION OF THE NR 6 MCD SPOOL BRACKET BOLT BORES IAW NTSPM 06-10-01.003 AND EA 8-5230-117632, STEP C. BORE HOLES B, C, AND D HAVE CRACK/CORROSION INDICATIONS. REAMED 4 EA. BOLT BORES, ACCOMPLISHED BHEC, FABERICATED AND INSTALLFeb 5, 2008 · N315FE · Doug DC1030F · Cargo/Baggage DoorsSDR 08FDEA00360Door Frame · corrodedMCD DOOR JAMB, WEB CORRODED UNDER CENTERING GUIDE. REPAIRED AREA IAW EA 8-5710-116952.Feb 5, 2008 · N315FE · Doug DC1030F · Fuselage Main, StructureSDR 08FDEA00350Skin · crackedLT WING INBOARD FLAP ON UPPER SKIN FOUND SCRATCH.Feb 5, 2008 · N306FE · Doug DC1030F · Trailing Edge FlapsSDR ARWA20080202Connector · dirtyUPON ADVANCING, THE POWER LEVERS FOR TAKEOFF, NR 3 START VALVE LIGHT ILLUMINATED, LIGHT EXTINGUISHED WHEN POWER LEVERS WERE RETARDED TO IDLE. CLEANED AND SECURED CONNECTOR AT NR 3 ENGINE STARTED VALVE, OPERATIONAL CHECK AT BLAST FENCE TAKEOFF POWER IAW MM 71-Feb 3, 2008 · N478CT · Doug DC1030F · Engine Starting System WiringSDR 08FDEA00331Beam · crackedCTR CARGO COMPT ON BEAM FOUND CRACK 0.70" LONG. REPAIRED BEAM IAW SRM 53-00-01 VOL I FIG 4 SHT 2.Jan 30, 2008 · N306FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA00323Fitting · corrodedACCOMPLISHED AN INITIAL BHEC INSPECTION OF THE NR 2 MCD SPOOL BRACKET BOLT BORES IAW NTSPM 06-10-01.003 AND EA 8-5230-117632, STEP C. ALL FOUR BORE HOLES (A, B, C AND D) HAVE CRACK/CORROSION INDICATIONS. REAMED BOLT BORES IAW SRM 53-50-00 VOL I FIG 17 PG 81Jan 29, 2008 · N315FE · Doug DC1030F · Cargo/Baggage DoorsSDR 08FDEA00297Seat Track · corrodedMAIN CABIN SEAT TRACK HAS AREAS OF CORROSION STA 1481 TO 1531 LBL9. REMOVED, FABRICATED AND INSTALLED SEAT TRACK ATTACH LOBE AND SUPPORT STRUCTURE REPAIR IAW MD/DC10 -30 SRM 53-70-00 FIG 5 SHT 1 VOL 1,51-38-01 VOL II, 51-21-01 VOLII, 51-21-02 VOLII AND 51-40-Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00296Bracket · crackedMCD SPOOL BRACKET NR 7 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REPAIRED IAW EA 8-5310-113030.Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage Main, Attach FittingsSDR 08FDEA00295Bracket · crackedMCD SPOOL BRACKET NR 5 HAS CRACK INDICATION ON HOLES B, C, AND D. REPAIRED IAW EA 8-5310-113030. MAJOR REPAIR.Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 08FDEA00294Bracket · crackedMCD SPOOL BRACKET NR 4 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REPAIRED IAW EA 8-5310-113030.Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage Main, Attach FittingsSDR 08FDEA00293Bracket · crackedMCD SPOOL BRACKET NR 3 HAS CRACK INDICATION ON HOLES A AND B. REPAIRED IAW EA 8-5310-113030.Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage Main, Attach FittingsSDR 08FDEA00288Bracket · crackedMCD SPOOL BRACKET NR 1 HAS CRACK INDICATION ON HOLES A, B, C, AND D. REAMED ALL HOLES TO DIMENSIONS SHOWN IN TABLE 1 OF EA 8-5310-113030. PERFORMED HFEC OF ALL HOLES, NO DEFECTS NOTED. IAW NDT SPM 06-10-01-003. REPAIRED LOWER JAMB BEAMS IAW EA 8-5310-113030Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage Main, Attach FittingsSDR 08FDEA00287Seat Track · corrodedMAIN CABIN SEAT TRACK BETWEEN STA 1019 TO 1039 AT APPROX RBL - 48 IS CORRODED AND CRACKED. REMOVED AND REPLACED SEAT TRACK FROM STA 949 TO STA 1049 RBL48 IAW MD/DC10 -10 SRM 51-40-02 VOL II.Jan 26, 2008 · N315FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00278Shear Tie · crackedAFT CARGO COMPT AT FS 1952 BETWEEN L47-48R SHEAR TIE IS CORRODED. REMOVED, FABERICATED AND INSTALLED SHEAR TIE IAW SRM 51-33-01, PG-1, VOL II & DWA AGA7133 REV.H. & SRM 51-35-01 VOL II.Jan 25, 2008 · N315FE · Doug DC1030F · Fuselage Internal Mounting StructureSDR 08FDEA00264Skin · dentedRIGHT WING TRAILING EDGE LOWER SKIN SURFACE DENTED INBD OF OUTBD MAIN FLAP INBD END. REMOVED PANELS TO FOM IAW MD/DC10 SRM 51-31-01 VOL II, CUTOUT DAMAGE AREA IAW MS/DC10 SRM 57-00-01 VOL I. MATERIAL ID FOR DOUBLER REPAIR 2024 T-3, .090 PO NR 575582.1, IJan 24, 2008 · N315FE · Doug DC1030F · Wing, Plate/SkinSDR WRLA2008013Indicator · malfunctionedKDOV/EDDP TAS/SAT INSTRUMENT OFF FLAGS APPEARED, 10 MINS LATER SMOKE EMINATED BRIEFLY FROM INSTRUMENT, TAS/SAT C/B PULLED CONDITION WENT AWAY, MX CONTROL ADVISED. REMOVED AND REPLACED TAS/SAT GAUGE, OPS NORMAL MM 34-15-00. DMI'S CLOSED.Jan 22, 2008 · N303WL · Doug DC1030F · Airspeed/Mach IndicatorSDR 08FDEA00187Skin · wornRT WING LWR SIDE EXT ZONE FOUND DEEP WEAR ON SKIN. REPAIRED AREA IAW SRM 57-10-00 FIG 36 AND 39 VOL I.Jan 17, 2008 · N306FE · Doug DC1030F · Wing Main, Frame StructureSDR 08FDEA00189Squat Switch · inactiveAFTER T/O RAISED GEAR AND NOSE GEAR REMAINED UNSAFE, BOTH PRIMARY AND SECONDARY INDICATIONS. RAN QRH CHECKLIST, CYCLED GEAR AND GOT GOOD UP AND LOCKED INDICATIONS, SO CONTINUED ON FLIGHT. WHILE GEAR WAS UNSAFE ALSO GOT PITOT AND TAT PROBE HEAT OFF INDICATIJan 15, 2008 · N301FE · Doug DC1030F · Landing Gear Position and WarningSDR ARWA20080101Mechanism · damagedSLAT DISAGREE LIGHT ILLUMINATED WHEN SLATS SELECTED IN POST FLIGHT; INSPECTION FOUND LT INBOARD SLAT DEPLOYED. REMOVED AND REPLACED ASSEMBLY RUN NR 53A, NR 54A, NR 55A, AND NR 56A; NR 55C AND TWO (2) PULLEYS ASSEMBLY ON LT NR 7 AND NR 2 SLAT IN ACCORDANCE WITJan 12, 2008 · N450ML · Doug DC1030F · Leading Edge Slat Control SystemSDR 08FDEA00081Frame · crackedAFT FUSE WASTE TANK COMPT ON FRAME FOUND CRACK. REPAIRED FRAME IAW SRM 53-30-00 FIG 4 VOL I.Jan 10, 2008 · N306FE · Doug DC1030F · Fuselage Main, FrameSDR 08FDEA00079Frame · crackedUPPER FUSELAGE ENTRY WAY CRACK ON FITTING SUPPORT (P/N AWE8001-503 ). REPAIRED FRAME IAW SRM 53-30-00 FIG 5 SHT 1 VOL I.Jan 9, 2008 · N308FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200801070056Skin · dentedRT INBD ELEVATOR LWR SURFACE FOUND DENT ON SKIN. REPAIRED AREA IAW SRM 51-10-00 FIG 8 VOL I.Jan 7, 2008 · N306FE · Doug DC1030F · Elevator, Plate/SkinSDR ARWA20071206O-Ring · leakingLOST HYDRAULIC QUANTITY BELOW 6 GALLONS SYSTEM 3; HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT "ON". REMOVED AND REPLACED "O" RING AT LOWER FITTING OF REVERSIBLE MOTOR PUMP SHUTOFF VALVE NR 1-3 IN ACCORDANCE WITH M/M 29-22-01; OPERATIONAL CHECK AND LEAK CHECKED IN ADec 29, 2007 · N450ML · Doug DC1030F · Hydraulic System, MainSDR FDEA200712205107Skin · dentedEXT FUSELAGE LWR SKIN FOUND 2 DEEP DENT, 1) 6 INCH BY 2 INCH THE WIDTH OF THE DENT IS APPROX .09 INCH, 2) 7 INCH BY 2 INCH THE WIDTH OF THE DENT IS APPROX .09 INCH. REPAIRED AREA IAW SRM 53-20-00 FIG 13 SHT 2A VOL I.Dec 20, 2007 · N306FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 07FDEA05113Switch · failedPDIS: LEVEL AT FL330, 45 MINUTES INTO FLIGHT, GOT NR 3 MANF LIGHT, FOLLOWED BY A LEVEL 3 "MANIFOLD NR 3 FAIL" ALERT. COMPLIED WITH RED TABS AND LANDED AT NEAREST SUITABLE AIRFIELD (KLAS). MAN LIGHT EXTINGUISHED SOMEWHERE BETWEEN 8000' AND 5000' IN THE DESCENDec 20, 2007 · N304FE · Doug DC1030F · Pneumatic Indicating SystemSDR ARWA20071204Wire · damagedDURING INITIAL TAKEOFF ROLL SPOOLING UP NR 1 ENGINE REVERSER PRESSURE LIGHT CAME ON. TRANSFERRED TO DMI NR 21307, MEL 78-1 CAT "C", INSTALLED PLACED AND DEACTIVATED FAN REVERSER IAW DDG. REPAIRED WIRES AT THRUST REVERSER LOCK SWITCH CAM ASSEMBLY THROTTLE MODec 16, 2007 · N450ML · Doug DC1030F · Engine Exhaust System WiringSDR 07FDEA05062Valve · failedNEAR TOP OF CLIMB, NR 3 AIR SYS OFF LIGHT ILLUMINATED. NR 3 DUCT DISPLAYED RED MOMENTARILY UNTIL AUTO SHUTDOWN. DIVERTED DUE TO INABILITY TO USE WING ANTI-ICE VALVE - INOP CLOSED. DO NOT USE NR 3 PNEUMATIC SUPPLY SYSTEM." DECAY CHECK C/W PER M/M 36-00-01Dec 15, 2007 · N301FE · Doug DC1030F · Pneumatic Distribution SystemSDR 07FDEA05050Seat Track · crackedAFTER REMOVAL CEILING PANELS WITH J/C "2552C120-2JR" FWD CARGO COMPT BELOW SEAT TRACK FOUND CRACK. REPAIRED SEAT TRACK IAW SRM 53-70-01 FIG 1 VOL I.Dec 13, 2007 · N308FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA05049Floor Support · corrodedAFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-70-00 VOL I FIG 13.Dec 13, 2007 · N308FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 07FDEA05048Support · corrodedAFTER REMOVAL CEILING PANELS WITH J/C "2552C180-3JR" AFT CARGO COMPT BELOW CHANNEL SUPPORT FLOOR FOUND SEVERE EXFOLIATION CORROSION. REPAIRED AREA IAW SRM 53-70-00 FIG 13 VOL I.Dec 13, 2007 · N308FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR 07FDEA05047Web · crackedLOWER AFT FUSELAGE COMPT CRACK ON WEB, UPPER TORQUE BOX PLANE. REPAIRED WEB IAW SRM 51-40-00 FIG 41 VOL I.Dec 13, 2007 · N308FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200712034979Seat Track · corrodedCTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.Dec 3, 2007 · N306FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04980Seat Track · corrodedCTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK. REPAIRED SEAT TRACK IAW SRM 53-70-00 FIG 1 SHT 1-2 VOL I.Dec 3, 2007 · N306FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04979Seat Track · corrodedCTR CARGO COMPT DURING PERFORMED J/C MD10-2552-C180 FOUND SEVERE EXFOLIATION CORROSION ON SEAT TRACK.Dec 3, 2007 · N306FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR 07FDEA04978Skin · dentedLOWER EXT FUS FOUND DENT .50" BY .50" DEPTH .04" ON SKIN. REPAIRED AREA IAW SRM 53-20-00 FIG 13 VOL I.Dec 3, 2007 · N308FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 07FDEA04883Skin · dentedFUSELAGE SKIN AFT OF CENTER PIT DOOR HAS 3 EACH DENTS REPAIRED AREA AS REQUIRED IAW SRM 53-20-00 FIG 13.Nov 20, 2007 · N317FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR 07FDEA04882Torque Box · crackedR-3 DOOR FWD JAMB TORQUE BOX WEB CRACKED AT FLOOR LINE REPAIRED WEB IAW SRM 53-50-00 FIG 19 SHEET 1.Nov 20, 2007 · N317FE · Doug DC1030F · Fuselage Main, StructureSDR 07FDEA04881Web · crackedR-3 DOOR AFT JAMB TORQUE BOX WEB CRACKED AT FLOOR LINE REPAIRED WEB IAW SRM 53-50-00 FIG 19 SHEET 2.Nov 20, 2007 · N317FE · Doug DC1030F · Fuselage Main, StructureSDR 07FDEA04847Skin · crackedLT INBD ELEVATOR OUTER RIB WITH 1/4" CRACK ON RIB AND LOWER SKIN.Nov 19, 2007 · N306FE · Doug DC1030F · Elevator, Plate/SkinSDR FDEA200711124772Stiffener · wornAIR CONDITIONING COMPT LT SIDE ON VERTICAL BHD ON NR 2 VERT STIFFENER FOUND DEEP WEAR. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 8 AND 9.Nov 12, 2007 · N306FE · Doug DC1030F · Fuselage Miscellaneous Structure
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