Douglas DC-8-71F

Service difficulty reports · 8,938

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 = 'DC871F'
  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 UPS96805883Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE ON FITTING, FS 1190 LONGERONS 32 TO 33R. REPLACED FITTING PER SRM 51-1-20D.Mar 10, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805963Skin · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB L/E SKIN AT ATTACHING SCREW HOLES HAD HEAVY CORROSION AT STA XFS 125 AND 136 UPPER SIDE OF SKIN. REPAIRED SKIN PER SRM 55-2-1.Mar 8, 1996 · N797UP · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR UPS96805901Longeron · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 21L IS CRACKED FS 1260. REPAIRED LONGERON PER SRM 53-2-5.Mar 6, 1996 · N797UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS96805898Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT O/B AILERON SKIN AND LOWER DOUBLER CRACKED AT THE I/B CLOSURE RIB. REPAIRED PER UPS EO DC8-57-0652.Mar 5, 1996 · N797UP · Doug DC871F · AileronsSDR UPS96805882Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FITTING, AFT SIDE OF FS 1680 LONG 21R. REPLACED FITTING PER SRM 51-1-20D.Mar 5, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805881Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FITTING, FWD SIDE OF FS 1680 LONG 31R. REPLACED FITTING PER SRM 51-1-20D.Mar 5, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9635Turnbuckle · splitDFW - ON DEPARTURE, GEAR DOOR LIGHT WOULD NOT GO OUT WITH THE LANDING GEAR HANDLE IN THE 'UP' POSITION. CYCLING THE GEAR RESULTED IN NO CHANGE. THE AIRCRAFT RETURNED TO DFW FOR MAINTENANCE. MAINTENANCE FOUND THE RT MLG DOOR ACTUATOR FOLLOW-UP CABLE WAS OUT Mar 5, 1996 · N828BX · Doug DC871F · Landing Gear Door Retract SectionSDR UPS96805906Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 35L SPLICE FITTING CRACKED AT FS 1270. REPLACED FITTING PER SRM 51-1-20D.Mar 4, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805905Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 34L SPLICE FITTING CRACKED AT FS 1270. REPLACED FITTING PER SRM 51-1-20D.Mar 4, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805902Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LONGERON 31L SPLICE FITTING CRACKS AT FS 1290. REPLACED FITTING PER SRM 51-1-20D.Mar 4, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805962Bolts · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD SPOOL BOLTS 1, 2, 4, 5, 6 AND 7 ARE CORRODED. REPLACED BOLTS PER MM 52-36-01 (T/C 420269).Mar 3, 1996 · N797UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS96805880Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION ON FITTING FS 1228 LONG 27 TO 28L. REPLACED FITTING PER SRM 51-1-20D.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805879Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION LONGERON FITTING. REPLACED FITTING PER SRM 53-2-0 AND 51-1-20D.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805878Frame · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD SIDE OF FRAME FS 1360 ABOVE LONG 36. REPAIRED FRAME PER SRM 53-2-0, FIG 2.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Main, FrameSDR UPS96805877Fitting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CORNER FITTING FS 1394 INSIDE LONG FWD TORQUE BOX HOLE. REPLACED FITTING PER SRM 51-1-20D.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805876Longeron · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON LONGERON 34L FS 1380 TO 1400 FS 1520 TO 540. REPLACED LONGERON SECTION PER SRM 51-2-2.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS96805875Splice · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE AT SPLICE LONG 31L BETWEEN FS 1520 TO 1540. REPLACED SPLICE PER SRM 51-1-20D.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805870Doubler · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER BETWEEN LONG 31L TO 33R FS 1227 TO 1264. REPLACED PER EO DC8-53-1599.Mar 3, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805966Doubler · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON FWD PRESS BULKHEAD RADIUS DOUBLER, FS 980 LONG 36. REPLACED RADIUS DOUBLER PER SRM 51-3-0.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805865Angle · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LOWER SUPPORT ANGLE UNDER SEAT TRACK NR 7 FS 781 TO 759. REPAIRED PER UPS EO.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805863Floor Beam · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION AND CRACK AT FWD BEAM, FS 920 LBL 65 AFT SIDE. REPAIRED PER UPS EO.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS96805861Seat Track · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON MAIN CABIN SEAT TRACK NR 5 AROUND FLOOR BEAM ATTACH HOLES FS 759-822, RBL 22. REPLACED TRACK SECTION PER SRM 53-2-3.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS96805860Seat Track · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED SEAT TRACK NR 1 HAS CORROSION DAMAGE AND CRACKS AT FS 759-781, LBL 55. REPLACED TRACK SECTION PER SRM 53-2-3.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR UPS96805859Angle · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON LOWER ATTACH ANGLE UNDER MAIN CABIN SEAT TRACK NR 4, FS 702, BL ZERO. SPLICED ANGLE PER SRM 53-2-0.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805858Skin · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION DAMAGE ON FUSELAGE INNER SKIN, STA 1600-1680, LONGERONS 21R-31R. REPLACED SECTION PER SRM 51-1-21.Mar 2, 1996 · N797UP · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA96101Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 27R BETWEEN Y=1220 TO Y=1240 CORRODED. CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 27R BY FABRICATING REPAIR STRAP AND INSTALLED IAW REO 01841 AND TREATED AREA IAW DC-8 SRM 51-1-8.Mar 2, 1996 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA96100Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 31R BETWEEN Y=990 TO Y=1010 CORRODED. CORROSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED LONGERON 31R BY FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW REO 01847 AND TREATED AREA IAW DC-8 SRM 51-1-Mar 2, 1996 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR RRXA96099Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND LONGERON 36 BETWEEN Y=980 TO Y=990 CORRODED. CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 36 BY REMOVING DAMAGE AND FABRICATING REPAIR STRAP AND SHIMS AND INSTALLED, IAW REO 01847 AND TREATED IAW DC-8 SRM 51-1-8.Mar 2, 1996 · N8084U · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS96805896Spar · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING REAR SPAR AT WW IS CRACKED AT LOWER HORIZONTAL CAP RBL 30 FS 857. REPAIRED PER UPS EO DC8-5710-8088A.Mar 1, 1996 · N797UP · Doug DC871F · Wing SparSDR UPS96805874Attach Angle · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY INTERGRANULAR CORROSION ON FRAME ANGLE FS 360 LONG 27L. REPAIRED PER SRM SRM 51-1-20D.Mar 1, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805873Frame · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BOLT FRAME FS 160 LONG 36 TO 35R. REPAIRED PER SRM 53-2-0 FIG 2 AND SRM 51-1-20D.Mar 1, 1996 · N797UP · Doug DC871F · Fuselage Main, FrameSDR UPS96805872Angle · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON ATTACH ANGLE AT FS 100 LONG 31R. REPLACED ANGLE PER SRM 51-1-21.Mar 1, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805667Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT MLG ATTACH FITTING RETRACT BRACKET ATTACH LUG, AFT LUG UPPER ATTACH HOLE HAS CORROSION DAMAGE INSIDE HOLE AND FWD LUG SURFACE. REPAIRED PER UPS EO.Mar 1, 1996 · N783UP · Doug DC871F · Wing, Landing Gear Attach FittingsSDR UPS96805965Doubler · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION DAMAGE ON FINGER STR DOUBLER FS 50 TO 67 LONG 21L. REPLACED FINGER DOUBLER PER SRM 51-1-21.Feb 29, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805964Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT HORIZONTAL STAB FITTING HAD CORROSION DAMAGE AT NR 4 STR STA XFS 135 BOTTOM INSIDE SKIN. REPLACED FITTING PER SRM 51-1-20D.Feb 28, 1996 · N797UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS96805961Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MCD JAMB HEAVY CORROSION ON ATTACH ANGLE FITTING FWD OF NR 1 SPOOL FITTING. REPLACED ANGLE FITTING PER SRM 51-3-0.Feb 28, 1996 · N797UP · Doug DC871F · Cargo/Baggage DoorsSDR UPS96805871Fitting · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION AT FS 920 FITTING AFT OF LONG 24R. REPLACED FITTING PER SRM 53-2-0.Feb 28, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805867Fitting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FS 980 FWD OF FRAME FITTING LONGERON 20R. REPLACED FITTING PER SRM 51-1-20D.Feb 28, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805854Skin · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING T/E, STA XW700 TO STA XW 710 HAS CORROSION BULGES ON SKIN. REPAIRED SKIN IAW DOUG DRAWING NR 5644654.Feb 28, 1996 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS96805893Spar · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED 6 CRACKS TOTALING 13 INCHES LONG AND HEAVY CORROSION AT LT WING REAR SPAR STA XRS615 TO STA XRS659. REPAIRED PER UPS EO DC8-57-0651.Feb 27, 1996 · N797UP · Doug DC871F · Wing SparSDR UPS96805868Doubler · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON BOLT FRAME DOUBLER FS 857 LONGERON 19R. REPLACED FRAME DOUBLER PER SRM 51-1-20D.Feb 27, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805866Intercostal · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON FS 1265 LONGERON 11R AT INTERCOSTAL. REPAIRED INTERCOSTAL PER SRM 51-1-20D, 53-2-0.Feb 27, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805853Skin · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED VERTICAL STABILIZER T/E, BOTH SIDES HAVE CORROSION BETWEEN NR 4 RUDDER SUPPORT FITTING. REPLACED SKIN PANEL BY REBONDING NEW ONES IAW SRM 51-1-19.Feb 27, 1996 · N797UP · Doug DC871F · Vertical Stabilizer, Plate/SkinSDR UPS805596Exc Rope Cover · out of adjustMAINTENANCE REPORTED, CAPTAINS ESCAPE ROPE WILL NOT REMAIN SECURE IN STOWED POSITION. PERFORMED INTERIM REPAIR TO CAPT'S ESCAPE ROPE COVER AND DEFERRED PER EO DC8-2510-7055 A FINAL REPAIR REQUIRED PRIOR TO FIRST FLIGHT ON 3-4-96.Feb 27, 1996 · N709UP · Doug DC871F · Emergency EquipmentSDR UPS96805904Spar · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CRACK IN TOP SIDE OF RT WING STA XRS 358 SPAR CAP. REPAIRED PER SRM 57-2-0 AND UPS EO DC8-5720-487.Feb 26, 1996 · N797UP · Doug DC871F · Wing SparSDR UPS96805903Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED 5 INCH LONG CRACK AT RT WING EXTERNAL LEADING EDGE ABOVE PYLON NR 4. REPAIRED L/E SKIN PER SRM 57-2-1A.Feb 26, 1996 · N797UP · Doug DC871F · Wing, Plate/SkinSDR UPS96805666Skin · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT ELEVATOR UPPER SKIN HAS 2 CRACK'S AT STA 77.67 NEAR T/E. REPAIRED SKIN PER UPS EO.Feb 26, 1996 · N783UP · Doug DC871F · Elevator, Plate/SkinSDR UPS96805869Splice · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED CORROSION ON LONGERON 8R SPLICE FS 210. REPLACED SPLICE FITTING PER SRM 51-1-20D.Feb 25, 1996 · N797UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS96805895Skin · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED MODERATE CORROSION DAMAGE ON FUSELAGE SKIN AT THE CUTOUT FOR THE AFT ENTRY DOOR HOLD OPEN HOOK. REPAIRED PER UPS EO DC8-53-1608.Feb 24, 1996 · N797UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS96805900Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING NR 1 SPOILER DELAMINATION ON UPPER SURFACE. REPLACED SPOILER ASSY PER MM 27-61-01.Feb 23, 1996 · N797UP · Doug DC871F · Spoilers
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