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 FDEA200912224497Doubler · crackedLT WING L/E FOUND CRACK ON INTERNAL DOUBLER. REPAIRED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1Dec 22, 2009 · N320FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA200912224496Intercostal · crackedLT WING L/E FOUND CRACK ON INTERNAL INTERCOSTAL. REPAIRED INTERCOSTAL IAW SRM 57-00-01 FIG.10 SH.1 VOL.1Dec 22, 2009 · N320FE · Doug DC1030F · Wing Miscellaneous StructureSDR FDEA200912224495Channel · corrodedLWR CTR CARGO COMPT, SEVERE CORROSION ON CHANNEL.Dec 22, 2009 · N320FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200912224494Frame · wornMAIN CABIN DEFORMATION AND WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00, FIG 4, VOL I.Dec 22, 2009 · N315FE · Doug DC1030F · Fuselage Main, FrameSDR 22AA200900032Control Box · failedANTI-SKID TESTED NORMAL ON BEFORE LANDING CHECKLIST UPON NORMAL LANDING (NO EMERGENCY DECLARED) AND AFTER EXITING RUNWAY TOWER REPORTED OBSERVING SPARKS FROM RT WING LANDING GEAR, EMERGENCY VEHICLES WERE OUT TO INSPECT, FOUND NO FIRE OR DAMAGE, CLEARED TO TAXIDec 19, 2009 · N478CT · Doug DC1030F · Brake Anti-Skid SectionSDR FDEA200912044355Frame · crackedLT AIR CONDITIONING COMPT FOUND CRACK ON FRAME. REPAIRED FRAME IAW SRM 53-30-00, FIG 4, VOL I.Dec 4, 2009 · N315FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200912034338Membrane · crackedCOCKPIT FLOOR STRUCTURE HAVE BEEN FOUND CRACK ON MEMBRANE AND ON STIFFENERS. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Dec 3, 2009 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200911264201Skin · crackedLT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.Nov 26, 2009 · N320FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200911264200Skin · crackedLT WING OTBD FLAP FOUND CRACK ON UPPER SKIN. REPAIRED SKIN IAW SRM 57-00-01 FIG 4, SHT 2, VOL I.Nov 26, 2009 · N320FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200911264199Skin · dentedLT WING OTBD FLAP LWR SKIN FOUND MANY DEEP NICKS. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, VOL I.Nov 26, 2009 · N320FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200911234121Channel · corrodedFWD CARGO COMPT DURING MOD, REMOVED PART FOUND 6 EA MODERATELY CORRODED CHANNELS UNDER SHOE BRAKES. REPAIRED AREA IAW SRM 53-70-00 FIG 7, SHT 5, VOL I.Nov 23, 2009 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200911234120Channel · corrodedFWD CARGO COMPT DURING MOD REMOVED ACTION FOUND MODERATE CORROSION UNDER THE SHOE BRAKE CHANNEL. REPAIRED AREA IAW SRM 53-70-00, FIG 7, SHT 5, VOL I.Nov 23, 2009 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200911234119Frame · crackedMAIN CABIN FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.Nov 23, 2009 · N321FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200911234118Frame · crackedMAIN CABIN FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 5 VOL I.Nov 23, 2009 · N321FE · Doug DC1030F · Fuselage Main, FrameSDR 22AA200900031Elt · malfunctionedON PRE-FLIGHT FOUND ELT LIGHT BLINKING. ENTERED ON DMI NR 23233 IAW MEL 25-40-2 CAT "A" C/B COLLARED VERIFIED NO AUDIO TRANSMIT ON VHF FREQ, PLACARD INSTALLED DMI NR 23233.Nov 17, 2009 · N450ML · Doug DC1030F · Emergency Locator BeaconSDR FDEA200911173995Skin · dentedEXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN 1"X 1" DEEP 0.060". PERFORMED HFEC INSPECTION IAW NDTSPM 06, NO CRACK FOUND. INSTALLED FINGER DOUBLER IAW SRM 53-20-00 FIG.13 SH.2 & SH.5 VOL.1.Nov 17, 2009 · N320FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR FDEA200911143954Spar Cap · crackedLT HORIZ STABILIZER L/E, FOUND 1EA CRACK 1,5" LONG ON UPPER FRONT SPAR CAP AT XE 115 REPAIRED IAW SRM 55-20-00 VOL 1, FIG9.Nov 14, 2009 · N314FE · Doug DC1030F · Horizontal Stabilizer, Spar/RibSDR FDEA200911043841Skin · crackedDURING INSP OF HORIZ STABILIZER, FOUND SKIN PANEL PLANKS CRACKED. IAW EO NR 8-5510-7-2307 PT1, SECT. C, STEP 1 AND 2 VERIFY APPLICABILITY OF EO NR 8-5510-7-4308 PT 2. REPAIRED AREA IAW EA 8-5510-133464 & EA 8-5510-133465.Nov 4, 2009 · N315FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR FDEA200911033801Support · corrodedAFT CARGO COMPT, SEVERE CORROSION WITH EXFOLIATION ON SUPPORT. REPAIRED AREA IAW SRM 53-70-00 FIG 13 SHT 1 VOL I.Nov 3, 2009 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200911033800Support · corrodedAFT CARGO COMPT, SEVERE CORROSION WITH EXFOLIATION ON SUPPORT. REPAIRED AREA IAW SRM 53-70-00 FIG 13 SHT 1 VOL I.Nov 3, 2009 · N315FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200910303739Skin · dentedDURING INSPECTION EXT FUSELAGE LWR SURFACE FOUND DENT 2.50" X 1.50" DEEP 0.066" ON SKIN. REPAIRED AREA IAW SRM 53-20-00, FIG 13, SHT 5 VOL I.Oct 30, 2009 · N315FE · Doug DC1030F · Fuselage Main, Plate/SkinSDR CLCA10202009.2Access Door · missingON POST FLIGHT INSPECTION AT (SVMI) FOUND CENTER COMPARTMENT ACCESS DOOR MISSING. INSTALLED CENTER COMPARTMENT ACCESS DOOR IAW MM 52-32-00. AIRCRAFT RETURNED TO SERVICE.Oct 22, 2009 · N47888 · Doug DC1030F · DoorsSDR FDEA200910213623Skin · crackedRT WING OTBD FLAP UPPER SURFACE FOUND CRACKED ON SKIN. REPAIRED SKIN IAW SRM 57-10-00, FIG 85, SHT 3, VOL I.Oct 21, 2009 · N315FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200910143574Door Frame · crackedMAIN CABIN FOUND CRACK ON WEB JAMB DOOR. REPAIRED AREA IAW SRM 53-50-00 FIG 19 VOL I.Oct 14, 2009 · N321FE · Doug DC1030F · Fuselage Main, StructureSDR FDEA200910063482Skin · dentedDURING INSP EXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN OF CTR CARGO DOOR 4"X2" DEEP .120". REPAIRED DENT IAW SRM 52-10-00, FIG 6, VOL I.Oct 6, 2009 · N314FE · Doug DC1030F · Cargo/Baggage DoorsSDR FDEA200910023460Channel · corrodedFWD CARGO COMPT, STA 866 X= 58, FOUND EXFOLIATION CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I.Oct 2, 2009 · N321FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200910023459Floorbeam · crackedCTR CARGO COMPT, STA 1701 X= 34, Z=-100, FLOORBEAM LWR FLANGE WITH 1EA CRACK 3" LONG AND 1EA CRACK 1" LONG. REPAIRED AREA IAW SRM 53-60-01 FIG 3 VOL I.Oct 2, 2009 · N321FE · Doug DC1030F · Fuselage Main, Floor BeamSDR FDEA200910023458Floorbeam · crackedCTR CARGO COMP STA 1701, X=-34, Z=-100, LWR FLOORBEAM FLANGE WITH 1EA CRACK 7,5 " LONG REPAIRED AREA IAW SRM 53-60-01 FIG 3, VOL I.Oct 2, 2009 · N321FE · Doug DC1030F · Fuselage Main, Floor BeamSDR FDEA200909233370Skin · dentedRT WING INBD FLAP UPPER SKIN FOUND DEEP DENT AND OIL CANING 2.50 INCH X 1.50 INCH DEEP .055 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1-4 VOL I.Sep 23, 2009 · N314FE · Doug DC1030F · Trailing Edge FlapsSDR FDEA200909163308Sensor · malfunctionedDURING T-OFF, WHILE SETTING POWER TARGET 114.4 WHEN N1 REACHED APPROX 98-99 PERCENT (70KTS) N2 EXCEEDENCE ON NR 01 ENGINE, RESET T-OFF AT 70KTS AMBER ENG 1 EXCEDENCE DISPLAYING, AMBER 109,9 N2 DISPLAYED VCP R NO RESTRICTION REF: 72-00-00-6 1, NR 1 ENGINE,Sep 16, 2009 · N318FE · Doug DC1030F · Turbine GovernorSDR FDEA200909123289Beam · crackedCTR CARGO COMPT SUMP AREA FOUND BEAM CRACKED AND BROKEN. REPAIRED AREA IAW SRM 53-60-00 VOL I, FIG 3.Sep 12, 2009 · N313FE · Doug DC1030F · Fuselage Main, StructureSDR FDEA200909093277Seat Track · corrodedMAIN CABIN ENTRY WAY SEVERE INTERGRANULAR CORROSION ON SEAT TRACK. REPAIRED AREA IAW SRM 53-70-00 FIG 1 VOL I.Sep 9, 2009 · N321FE · Doug DC1030F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200909083267Longeron · corrodedLT AIR CONDITIONING COMPT FOUND SEVERE CORROSION WITH EXFOLIATION ON LONGERON. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & SRM 53-40-00 FIG 15 VOL I.Sep 8, 2009 · N321FE · Doug DC1030F · Fuselage Main, Longeron/StringerSDR FDEA200909083266Frame · crackedLT MLG WW FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-00-01 FIG 8 SHT 2 VOL I.Sep 8, 2009 · N321FE · Doug DC1030F · Fuselage Main, FrameSDR FDEA200909053260Transcowl · departedTOWER INFORMED US WE DROPPED SOMETHING ON ROLLOUT. SMOOTH LANDING, REVERSERS STOWED BY 65-70KTS. A LARGE PIECE OF NR 2 REVERSER CAME OFF AT END OF LANDING, ROLL INITIALLY GOT ALL 3 ENGINES SHOWING REV STOWED THEN NR 2 U/L LIGHT CAME ON. SHUTDOWN NR 2 AND TSep 5, 2009 · N306FE · Doug DC1030F · Engine Thrust ReverserSDR FDEA200908313170Door Frame · corrodedINSPECTED UPPER CARGO DOOR JAMB STRUCTURE CORROSION ON UPPER DOOR JAMB. ACCOMPLISHED EA NR 8-5310-129649.Aug 31, 2009 · N314FE · Doug DC1030F · Fuselage Main, StructureSDR FDEA200908263096Intercostal · crackedCOCKPIT, CRACK 2 INCHES LONG ON HORIZ WEB AT STA 276, X=-47, Z=-4 REPAIR IAW SRM 53-00-01, FIG 8, SHEET 2 AND FIG 10, SHEET 1, VOL 1.Aug 26, 2009 · N321FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200908263095Bulkhead · crackedCOCKPIT, FOUND 1EA CRACK 2 INCHES LONG ON HORIZ WEB AT STA 305, X=-14 REPAIR MEMBRANE IAW SRM 53-00-01 FIG 4, SHT 2, VOL 1.Aug 26, 2009 · N321FE · Doug DC1030F · Fuselage Main, BulkheadSDR FDEA200908263094Bulkhead · crackedCOCKPIT, 1EA CRACK 2 INCHES LONG ON HORIZ WEB AT STA 305, X= 14 REPAIR MEMBRANE IAW SRM 53-00-01 FIG 4, SHEET 2 VOL 1.Aug 26, 2009 · N321FE · Doug DC1030F · Fuselage Main, BulkheadSDR FDEA200908263093Skin · wornLT WING SLAT FOUND 1EA DEEP WEAR ON EXTERNAL SKIN SLAT DROOPED AT STA XDLE 309 REPAIR IAW SRM 57-21-01 FIG 4, VOL 3 AND SRM 57-00-01 FIG4, SHEET 2, VOL.1Aug 26, 2009 · N321FE · Doug DC1030F · Leading Edge DevicesSDR FDEA200908263092Skin · wornRT L/E SLAT FOUND 1EA DEEP WEAR ON EXTERNAL SKIN L/E DROOPED AT STA XDLE 309 REPAIR IAW SRM 57-21-01 FIG.4 VOL 3 AND SRM 57-00-01 FIG 4 SHEET 2 VOL 1.Aug 26, 2009 · N321FE · Doug DC1030F · Leading Edge DevicesSDR FDEA200908263091Skin · crackedRT WING, OTBD AILERON UPPER SURFACE FOUND 1EA CRACK 1 INCH LONG ON UPPER SKIN AND DEFORMED ON RIB AT STA XOA 1024 REPAIR IAW SRM 57-10-00 VOL I, FIG.85.Aug 26, 2009 · N321FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA200908263090Skin · crackedRT WING INTERNAL L/E FOUND 1EA CRACK 3 INCHES LONG ON INTERNAL SKIN DOUBLER UPPER AT STA XOS 667. REPAIR BEADED DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.Aug 26, 2009 · N321FE · Doug DC1030F · Wing, Plate/SkinSDR FDEA200908263089Rib · crackedRT WING INTERNAL L/E FOUND CRACK 1 INCH LONG ON INTERNAL RIB AT STA XOS 691 REPAIR FORMER IAW SRM 57-00-01 VOL 1, FIG 10, SHT 1.Aug 26, 2009 · N321FE · Doug DC1030F · Wing, Rib/BulkheadSDR CLCA08152009.1Engine · fodDURING TAKEOFF ROLL (MIA) NR 1 ENGINE VIBRATION OCCURRED FOLLOWED BY LOUD COMPRESSOR STALL. ABORTED TAKEOFF, ENGINE SHUT DOWN AND CAC EMERGENCY PROCEDURES FOLLOWED. RETURNED TO RAMP WITHOUT INCIDENT. INSPECTED NR 1 ENGINE, FOUND SEVERAL PARTICLES OF METAL IAug 15, 2009 · N47888 · Doug DC1030F · Turbine Engine Compressor SectionSDR FDEA200908133004Strap · crackedFWD AVIONICS COMPARTMENT, AFTER NOSE SKIN REMOVAL WITH OAN J/C SP10530242-7002- 4JR, FOUND CRACK ON INTERNAL SPLICE. REPAIRED AREA IAW SRM 53-00-01 FIG 4 SHT 2 VOL I.Aug 13, 2009 · N321FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200908102964Channel · corrodedCTR CARGO COMPT REF EO 8-2550-7-2354 P2 STEP "E1" AFTER REMOVAL PARTS FOUND DEEP CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I.Aug 10, 2009 · N314FE · Doug DC1030F · Fuselage Miscellaneous StructureSDR FDEA200908052908Skin · crackedDURING U/S INSP OF HORIZONTAL STB, CONSTANT SECTION, FOUND PANEL P/N 7226-1 & 7224-1 LOWER INTERIOR SKIN PANELS WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-130928.Aug 5, 2009 · N321FE · Doug DC1030F · Horizontal Stabilizer, Plate/SkinSDR 22AA200900022Slat System · malfunctionedON SHORT FINAL, SLAT DISAGREE LIGHT ILLUMINATED CAUSING STICK SHAKER. PROMPT APPLICATION OF FIREWALL POWER AND INCREASE IN SPEED PUT SLATS BACK IN "LAND" LANDING UNEVENTFUL. APP GW OF 305.000 LBS. 35/EXT REF OF 133+5 KTS. (K)Jul 30, 2009 · N450ML · Doug DC1030F · Leading Edge Slat Control SystemSDR 22AA2009000022Slat System · malfunctionedON SHORT FINAL, SLAT DISAGREE LIGHT ILLUMINATED CAUSING STICK SHAKER PROMPT APPLICATION OF FIREWALL POWER AND INCREASE IN SPEED, PUT SLATS BACK IN LAND; LANDING UNEVENTFUL. APP GW OF 35.000 LBS, 35/EXT. REF. OF 133 + 5 KTS. INSPECTED SLAT SYS CABLES, PULLEYS,Jul 30, 2009 · N450ML · Doug DC1030F · Leading Edge Slat Control System
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