Mcdonnell Douglas DC-8-63

Service difficulty reports · 1,601

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 aircraft_model_key = 'DC863'
  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 ABXA010388Skin · corrodedFUSELAGE SKIN BULGING AT FASTENER, AT APPROXIMATELY FS 205, LONGERON 31 LEFT. REMOVED CORROSION. REPLACED FINGER DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0, 51-1-8, 51-1-11, AND REA D853-40861MR.Jun 28, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010355Window · obstructedFIRST OFFICER'S SLIDING WINDOW WOULD NOT OPEN. FOUND AFT LOWER LOCK ON FIRST OFFICER'S WINDOW OBSTRUCTED BY SEALANT. REMOVED SEALANT. WINDOW OPERATED NORMAL.Jun 26, 2001 · N822AX · Doug DC863 · Flight Compartment WindowsSDR ARWA0010606Transformer · malfunctionedTAXI OUT SMOKE CAME OUT OF ELECTRICAL PANEL. AIRCRAFT RETURN TO BLOCKS WITHOUT INCIDENT. LOCATED THE SOURCE, GLARE INSTRUMENT WHITE LIGHTS BALLAST TRANSFORMER. DEACTIVATED GLARESHIELD AND INSTRUMENT WHITE LIGHTS AND ENTERED ON DMI 15265 AS PER MEL 33-1 CAT Jun 22, 2001 · N345JW · Doug DC863 · Flight Compartment LightingSDR ABXA010385Frame · crackedAFT LOWER CARGO FRAME AT STA 1440, LONGERON 35 RIGHT WAS CRACKED ABOVE LONGERON 35 RIGHT. REPLACED REPAIR ANGLE IAW DC-8 SRM 53-2-0, 51-1-21, 51-1-20D, AND 51-1-8.Jun 19, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010337Fitting · crackedAFT LOWER CARGO Z-FITTING CRACKED AT STATION 1180 FROM LONGERON 35 RIGHT TO LONGERON 34 RIGHT. REPLACED Z-FITTING AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, AND 51-1-24.Jun 11, 2001 · N828AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010558Bulkhead · crackedMAIN CABIN AFT PRESSURE BULKHEAD WAS CRACKED APPROXIMATELY 63 INCHES ABOVE THE FLOOR BETWEEN THE LEFT BUTT LINE 28 TO LEFT BUTT LINE 40. REPAIRED AREA IAW DAC DWG SRO 8530007, DC-8 SRM 51-1-8, 51-1-20D, 51-3-0, 51-3-1, AND 53-8-5.Jun 9, 2001 · N818AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA010322Skin · corrodedAFT CARGO AT FUSELAGE 1180 - 1220 AT LONGERON 29 LEFT SKIN WAS CORRODED UNDER AND BESIDE L-ANGLE.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010321Fitting · crackedAFT CARGO AT FUSELAGE 1180 BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING WAS CRACKED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010320Fitting · corrodedAFT CARGO AT FUSELAGE 1160 BETWEEN LONGERON 27 LEFT - 28 LEFT Z-FITTING WAS CORRODED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010319Angle · crackedNR 4 PYLON INTERIOR INBOARD VERTICAL ANGLE STATION YN 298 UNDER UPPER SPAR WEB CRACKED.Jun 8, 2001 · N818AX · Doug DC863 · Nacelle/Pylon, Main FrameSDR ABXA010318Angle · corrodedFS 980 LONGERON 35 LEFT BULKHEAD ATTACH ANGLE WAS CORRODED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010317Skin · corrodedAFT LOWER CARGO SKIN CORRODED AROUND SEVERAL FASTENERS FROM STATION FS 980 TO STATION FS 1040 BETWEEN LONGERON 35 LEFT AND LONGERON 35 RIGHT.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010316Longeron · corrodedAFT LOWER CARGO LONGERON 36 CORRODED AT STATION FUSELAGE 1021.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010315Fitting · corrodedFORWARD LOWER CARGO FITTING CORRODED AT FUSELAGE 70 LONGERON 36.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010314Fitting · corrodedAFT LOWER CARGO BATHTUB FITTING CORRODED AT FUSELAGE 1050 LONGERON 28 LEFT.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010313Frame · corrodedAFT LOWER CARGO FRAME CORRODED AT FUSELAGE 1500 LONGERON 36.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010312Frame · corrodedAFT LOWER CARGO FRAME CORRODED AT STATION FS 1050 LONGERON 35 LEFT.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010311Shear Tie · corrodedAFT LOWER CARGO SHEAR TIE CORRODED AT STATION FS 1020 BETWEEN LONGERON 35 RIGHT - LONGERON 36.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010310Longeron · corrodedAFT LOWER CARGO LONGERON 35 LEFT CORRODED AT STATION FS 1020.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010309Shear Tie · corrodedAFT LOWER CARGO, FUSELAGE 1040, LONGERON 35 RIGHT - 36, SHEAR TIE CORRODED.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010308Longeron · corrodedFS 1000 LONGERON 35 LEFT CORRODED ON INBOARD SIDE.Jun 8, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010565Skin · corrodedRIGHT HORIZONTAL STABILIZER LOWER SKIN WAS CORRODED AND BULGED, XE 149. REPAIRED AREA AND REPLACED SKIN IAW TSRM 95T0345001, DC-8 SRM 51-1-8, 51-1-21, AND 51-1-20D.Jun 7, 2001 · N818AX · Doug DC863 · Horizontal Stabilizer, Plate/SkinSDR ABXA010559Skin · damagedREMOVED AND REPLACED THE AFT LOWER SKIN, STATION 1350-1490. REPLACED THE AFT LOWER SKIN IAW DC-8 SRM 51-1-21, 51-3-2, 51-1-11, 51-1-26, 51-3-1, AND 51-3-3.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010387Frame · corrodedMAIN CABIN BETWEEN STA 1180 TO 1160, FRAME 1180 AT LONGERON 4 LEFT WAS CORRODED. REMOVED CORROSION, ALODINED AND PRIMED IAW DC-8 SRM 51-1-8. CORROSION WITHIN LIMITS IAW DC-8 SRM 53-2-0.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010386Longeron · crackedLONGERON 36 WAS CRACKED UNDER SPLICE FITTING AT STA 1350. RECEIVED LONGERON, DRILLED AND REAMED LONGERON IAW DC-8 SRM 51-3-2. INSTALLED IAW DC-8 SRM 51-1-20D.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010334Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 35 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010333Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 34 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010332Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 31 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010331Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, BETWEEN LONGERON 30 LEFT - 31 LEFT, PRODUCTION SPLICE FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010330Fitting · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 70, LONGERON 29 LEFT, END FITTING WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010329Skin · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 36 - 54, BETWEEN LONGERON 30 LEFT - 31 LEFT, WAS CORRODED FROM UNDER FINGER DOUBLER.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010328Frame · corrodedAIR COND/PRESSURIZATION COMPARTMENT AT FS 24, LONGERON 35 LEFT AND 35 RIGHT, FRAME WAS CORRODED AROUND ATTACH FASTENER TO LONGERON.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010327Frame · corrodedMAIN CABIN BETWEEN STATION 1260 TO 1240 FRAME 1260 WAS CORRODED AT CUSP.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010326Frame · corrodedMAIN CABIN BETWEEN STATION 1180 TO 1160 FRAME 1180 AT LONGERON 4 LEFT WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010325Longeron · corrodedMAIN CABIN BETWEEN STATION 1120 TO 1100 LONGERON 16 LEFT WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010324Frame · corrodedMAIN CABIN BETWEEN STATION 1360 TO 1347 FRAME AT STATION 1360 BETWEEN LONGERON 12 LEFT TO 5 A WAS CORRODED.Jun 7, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010323Spar · corrodedLEFT HORIZONTAL STABILIZER LEADING EDGE LOWER SPAR XE 114 WAS CORRODED INSIDE AROUND A RIVET BUCKTAIL.Jun 7, 2001 · N818AX · Doug DC863 · Horizontal Stabilizer, Spar/RibSDR ABXA010300Shear Tie · corrodedAFT CARGO AT STATION 1140 BETWEEN LONGERON 34 RIGHT AND 35 RIGHT, SHEAR TIE AND FRAME CORRODED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010299Shear Tie · crackedAFT CARGO AT STATION 1120 BETWEEN LONGERON 35 LEFT AND 36 LEFT, SHEAR TIE CRACKED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, StructureSDR ABXA010298Frame · corrodedAFT FUSELAGE AT STATION 1734 BETWEEN LONGERON 6 LEFT TO 7 LEFT FRAME WAS CORRODED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, FrameSDR ABXA010297Longeron · corrodedAFT FUSELAGE BETWEEN STATION 1717 TO 1700 LONGERON 20 LEFT WAS CORRODED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010296Longeron · corrodedAFT FUSELAGE BETWEEN STATION 1680 TO 1667 LONGERON 22 LEFT WAS CORRODED.Jun 6, 2001 · N818AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR ABXA010564Skin · corrodedCORROSION ON EXTERNAL SKIN OF THE VERTICAL STABILIZER, JUST ABOVE THE FUSELAGE TO VERTICAL ATTACHING ANGLE REPAIR DOUBLER. REPAIRED AREA AND INSTALLED NEW SKIN IAW DC-8 SRM 55-2-0, 51-1-21, 51-3-0, 51-1-22, 51-9-0, 51-1-26, 51-1-20D, 51-1-15, 51-1-16, AND DC-8Jun 5, 2001 · N818AX · Doug DC863 · Vertical Stabilizer, Plate/SkinSDR ABXA010563Skin · corrodedTAILCONE HAD CORROSION AND DETERIORATING SEALANT JUST ABOVE THE LOWER TAILCONE LIGHT IN THE SEAM. REPAIRED AREA AND INSTALLED NEW SKIN IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-21, 51-1-11, AND DC-8 DWG 5704665.Jun 5, 2001 · N818AX · Doug DC863 · Aerodynamic FairingsSDR ABXA010562Fitting · crackedLONGERON SPLICE FITTING AT STATION 450, LONGERON 31 LEFT WAS CRACKED. REPLACED SPLICE FITTING IAW DAC DWG 3750257 AND DC-8 SRM 51-1-8.Jun 5, 2001 · N818AX · Doug DC863 · Fuselage Structure (General)SDR ABXA010338Fitting · crackedRIGHT WHEEL WELL LONGERON 24 BATHTUB FITTING HAD CRACK EXTENDING BEYOND ORIGINAL STOP DRILL. REPAIRED AREA IAW DC-8 SRM 53-2-2, AND 51-1-8.Jun 5, 2001 · N818AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010295Spar Cap · corrodedRIGHT ELEVATOR UPPER SPAR CAP XE 65 WAS CORRODED BOTH SIDES OF THE RIB AND OUTER WEB.Jun 5, 2001 · N818AX · Doug DC863 · Elevator, Spar/RibSDR ABXA010294Spar Cap · corrodedRIGHT ELEVATOR UPPER SPAR CAP XE 95 WAS CORRODED BOTH SIDES OF RIB, INSIDE AREA.Jun 5, 2001 · N818AX · Doug DC863 · Elevator, Spar/RibSDR ABXA010561Bulkhead · gougedFORWARD RADOME BULKHEAD, FORWARD SIDE, LOWER 0600 POSITION, GOUGE IN WEB. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-21, 51-1-8, 51-1-20, AND DAC DWG 4644898.Jun 4, 2001 · N818AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA010560Spar Cap · gougedNR 4 PYLON INBOARD UPPER SPAR CAP GOUGED AT STATION YN 295. REPAIRED AREA IAW REA D854-40850-MR.Jun 4, 2001 · N818AX · Doug DC863 · Nacelle/Pylon, Frame/Spar/Rib
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