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 UPS805384Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LT WING L/E, 3 EACH, RIBS CRACKED AT STA. XFS 767, 846, 679. REPAIRED RIBS PER MM 57-00-00, FIG. 801.Jan 14, 1996 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS805383Web · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E LOWER SURFACE CRACKED IN WEB BETWEEN STA. XFS 608-614. REPAIRED WEB PER SRM 57-2-0.Jan 14, 1996 · N701UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS805382Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, B/T FITTING CRACKED AT F.S. 1230, BETWEEN LONGERONS 33R-34R. REPLACED FITTING PER SRM 51-1-20D.Jan 14, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805379Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E 2 EACH RIBS CRACKED AT STA XFS138, XFS 328. REPAIRED RIBS PER MM 27-00-00, FIG. 801.Jan 14, 1996 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS805410Fitting · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, FS 70 LONGERON 21R END FITTING CRACKED. REPLACED FITTING PER SRM 51-1-20D.Jan 12, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805408Skin · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B SLOT CUTOUT AFT O/B CORNER HAS A 1.0625 INCH CRACK. INSTALLED NEW PANEL SECTION PER SRM 51-3-0.Jan 12, 1996 · N748UP · Doug DC871F · Wing, Plate/SkinSDR RRXA96093Skin · corrodedWHEEL WELL AT Y= 790 TO Y= 795, X=33, SKIN HAS CORROSION DAMAGE PASS LIMITATIONS IAW SRM 53-2-0. REPAIRED INNER SKIN DAMAGE BY FABRICATING NEW SKIN PART IAW DAC-DRWG 5642970, SRM 53-2-0, 51-3-2, 51-1-22 AND TREATED AREA DC-8 SRM 51-1-8.Jan 12, 1996 · N8079U · Doug DC871F · Fuselage Main, Plate/SkinSDR RRXA96092Skin · corrodedWHEEL WELL AT Y= 790 TO Y= 795, X=-3, SKIN HAS SKIN CORROSION DAMAGE PASS LIMITATIONS IAW SRM 53-2-0. REPAIRED INNER SKIN DAMAGE BY FABRICATING NEW SKIN PART IAW DAC DRWG 5642970, SRM 53-2-0, 51-3-2, 51-1-22 AND TREATED AREA IAW DC-8 SRM 51-1-8.Jan 12, 1996 · N8079U · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS805411Fitting · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT HORIZ STAB CRACKED ON T-FITTING LOWER FWD I/B. REPLACED FITTING PER SRM 51-1-20D.Jan 10, 1996 · N701UP · Doug DC871F · Horizontal Stabilizer StructureSDR UPS805396Keel Beam · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, KEEL BEAM SPLICED RT SIDE CRACKED AT F.S. 940. REPLACED SPLICE PER SRM 51-3-0.Jan 10, 1996 · N701UP · Doug DC871F · Fuselage Main, KeelSDR UPS805385Fittings · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, T-FITTINGS, 2 EACH, CRACKED AT KEEL BEAM, CRACKED F.S. 940 AND 960. REPLACED FITTINGS PER SRM 51-1-21.Jan 10, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805189Fitting · corrodedWHILE IN FOR B-CHECK, MAINTENANCE REPORTED LONGERON 34R ATTACH FITTING AT STA 8.00 CRACKED, EVIDENCE OF CORROSION. WILL REPAIR/REPLACE FITTING PER UPS E.O. DC8 SRM.Jan 10, 1996 · N702UP · Doug DC871F · Fuselage Miscellaneous StructureSDR RRXA960001Actuator Pin · brokenKPIA-KDAY - FLT 525 - UPLATCH CHECK FAILED ON GEAR RETRACTION OUT OF KPIA. CYCLED GEAR NUMEROUS TIMES AND GEAR UNSAFE AND GEAR DOOR WARNING LIGHTS ILLUMINATED, N500MH FERRIED TO KMCN. MAINTENANCE FOUND THE LT MLG RETRACT CYLINDER PIN BROKEN. MAINTENANCE INSJan 10, 1996 · N500MH · Doug DC871F · Landing Gear Retraction/Extension SystemSDR RRXA9600001Actuator Pin · failedKDAY - FLT 525 - UPLATCH CHECK FAILED ON GEAR RETRACTION OUT OF KPIA. CYCLED GEAR NUMEROUS TIMES. GEAR UNSAFE AND GEAR DOOR WARNING LIGHTS ILLUMINATED. FERRIED A/C TO KMCN. MX FOUND THE LEFT MLG RETRACT CYCLINDER PIN BROKEN. MAINTENANCE INSPECTED THE BOSSJan 10, 1996 · N500MH · Doug DC871F · Landing Gear ActuatorSDR UPS805391Belt Frame · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, BELT FRAME CRACKED ON FORWARD SIDE F.S. 1440, LONGERON 23R. REPAIRED PER SRM 53-2-0.Jan 9, 1996 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS805381Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA. XFS 608, 596, 871, 827, 803, 785, 779, AND 749. REPAIRED RIBS PER MM 57-00-00, FIG. 801.Jan 9, 1996 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS805380Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA XFS 841, 836, 817, 797, 771, 652, 620, AND 626. REPAIRED RIBS PER MM 57-00-00, FIG. 801.Jan 9, 1996 · N701UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS805341Frame · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT FRAME STA 781 BETWEEN LONG 18 AND 19 CRACKED. REPAIRED IAW UPS EO DC8-53-1553 AND TIMCO REO 01764.Jan 9, 1996 · N713UP · Doug DC871F · Fuselage Main, FrameSDR UPS805340Spar · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING, NR 1 MAIN TANK O/B SECTION CRACKED LOWER CENTER SPAR AND WEB THROUGH ACCESS PNL 506A. REPAIRED IAW UPS EO DC8-5710-7895A.Jan 9, 1996 · N713UP · Doug DC871F · Wing SparSDR UPS805339Stringer · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING, STRINGER 54 LOWER CRACKED AT STA XW 485. REPAIRED IAW UPS EO DC8-5710-7184.Jan 9, 1996 · N713UP · Doug DC871F · Wing, Longeron/StringerSDR UPS805470Web · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED MODERATE CORROSION LWR. SIDE WEB FS 70 LONGERON 21R. REPAIRED WEB PER SRM 53-2-0.Jan 8, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805412Skin · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, 2 CRACKS ON SKIN FS 160 FWD UPPER CORNER OF FWD SERVICE DOOR. REPAIRED SKIN PER SRM 53-0 FIG 14.Jan 8, 1996 · N701UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS805397Longerons · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LONGERONS CRACKED 35L, F.S. 260-270. REPLACED LONGERON SECTION F.S. 250-310 PER SRM 51-1-20D.Jan 8, 1996 · N701UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS805395Canoe Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING NR 5 FLAP SUPPORT CANOE FITTING CRACKED UPPER FORWARD FASTENER HOLE, STA 428. REPLACED FITTING PER MM 27-51-12.Jan 8, 1996 · N701UP · Doug DC871F · Trailing Edge FlapsSDR UPS805377Angle · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, HEAVY CORROSION ON VERT. SUPPORT ANGLE FORWARD SIDE, F.S. 1040 LONGERON 27R. REPLACED ANGLE PER SRM 51-1-20D.Jan 8, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805376Doubler · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, F.S. 72 JACK PAD DOUBLER HAS CORROSION. REPLACED DOUBLER PER SRM 51-1-20D.Jan 8, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805467Doubler · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER, FS 620 LONGERON 35R. REPAIRED PER UPS E.O.Jan 6, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805351Skin · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION ON RT WING L/E BETWEEN XFS 608 TO XFS 614, LOWER SURFACE. REPLACED DOUBLER SECTION PER DOUGLAS PRINT 5769600.Jan 6, 1996 · N710UP · Doug DC871F · Wing, Plate/SkinSDR UPS805350Te Wedge · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING T/E EDGE O/B WEDGE HAS CORROSION ON INNER LOWER SURFACE. REPAIRED PER 51-1-21.Jan 6, 1996 · N710UP · Doug DC871F · Wing, Plate/SkinSDR UPS805466Belt Frame · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BELT FRAME LWR. LIP. LONGERON 36, FS 200. REPAIRED FRAME PER SRM 53-2-0 AND 51-1-20D.Jan 5, 1996 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS805465Cusp Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON CUSP FITTING FS 1580 LONGERON 21R. REPLACED FITTING PER SRM 51-3-0.Jan 5, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805352Flap Track · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, BOTH I/B AND O/B FLAP TRACK ASSYS HAVE CORROSION PITS, LOWER SIDE RT AFT I/B FLAP ASSY STA XW 98. REPLACED TRACKS PER MM 27-51-03.Jan 5, 1996 · N710UP · Doug DC871F · Trailing Edge FlapsSDR UPS805475Doubler · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON INNER DOUBLER FS 1050-1350 LONGERON 31L-31R. REPLACED DOUBLER PER SRM 50-2-0 AND 51-1-20D AND UPS E.O.Jan 4, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805473Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED 2 EACH FITTINGS HAVE HEAVY CORROSION AT FS 1220 LONGERON 35R, AND FS 1175 LONGERON 33R. REPLACED FITTINGS PER SRM 51-1-20D.Jan 4, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805468Fitting · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON END FITTING FS 70 LONGERON 30L. REPLACED END FITTING PER SRM 51-1-20D.Jan 4, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805447Skin · corrodedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, HEAVY CORROSION AT FUSELAGE EXTERNAL SKIN PANEL FS 1060 AND FS 1070 UNDER KEEL PLATE. REPAIRED SKIN PER UPS EO.Jan 4, 1996 · N701UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS805477Frame · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION UPPER FLANGE OF FRAME FS 1140 LONGERON 34L-35L. REPAIRED PER UPS E.O.Jan 3, 1996 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS805476Bolt Frame · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION UPPER FLANGE BOLT FRAME, FS 1120 LONGERON 36. REPAIRED PER SRM 53-2-0.Jan 3, 1996 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS805474Fitting · crackedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION AND CRACKED FITTINGS, FS 1150 LONGERON 34R-33R. REPLACED FITTINGS PER SRM 51-1-20D AND 51-1-8.Jan 3, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805469Shear Tie · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON SHEAR TIE, FS 1060 LONGERON 35R - 36R. REPLACED SHEAR TIE PER SRM 51-1-20D.Jan 3, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805378Fitting · corrosionWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 2 EACH FITTINGS CRACKED AT FORWARD END, F.S. 1220, LONGERON 17R, AND F.S. 1260, LONGERON 18R. REPLACED FITTINGS PER SRM 51-1-20D.Jan 3, 1996 · N701UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805353Frame · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION ON AFT SIDE OF BOLT FRAME FS 80, LONGERON 26R. REPAIRED BOLT FRAME PER SRM 53-2-0 FIG 2.Jan 3, 1996 · N710UP · Doug DC871F · Fuselage Main, FrameSDR IXXA9601Connector · looseON TAKEOFF OUT OF ONT, THE FLT CREW OBSERVED A LANDING GEAR DOOR UNSAFE INDICATION AFTER GEAR RETRACTION. THE LANDING GEAR WAS CYCLED, AND THE WARNING LIGHT EXTINGUISHED. TOL MAINTENANCE INSPECTED THE LANDING GEAR DOOR WARNING SYSTEM AND FOUND THE ELECTRICALJan 3, 1996 · N828BX · Doug DC871F · Landing Gear Door Retract SectionSDR UPS805481Floor Beam · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED EXFOLIATION CORROSION ON UPPER FLANGE OF FLOOR BEAM, FS 55 RBL 45. REPAIRED PER UPS E.O.Jan 2, 1996 · N701UP · Doug DC871F · Fuselage Main, Floor BeamSDR UPS805480Blkhd Cap · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BULKHEAD CAP FS 980 LONGERON 34R-35R. REPAIRED PER UPS E.O.Jan 2, 1996 · N701UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS805479Frame · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION ON BELT FRAME FS 1280 LONGERON 22R. REPAIRED FRAME PER SRM 53-2-0, FIG. 2Jan 2, 1996 · N701UP · Doug DC871F · Fuselage Main, FrameSDR UPS805478Longeron · corrodedWHILE IN FOR C CHECK, MAINTENANCE REPORTED HEAVY CORROSION LONGERON 35R, FS 1018. REPLACED SECTION PER SRM 51-1-20D.Jan 2, 1996 · N701UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS805355Angle · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, CORROSION BULGE ON VERTICAL ATTACH ANGLE AND WEB FS 798, RBL 40. REPLACED ANGLE PER SRM 51-1-21.Jan 2, 1996 · N810UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805354Fitting · corrosionWHILE IN FOR C-CHECK MAINTENANCE REPORTED, HEAVY CORROSION ON MAIN CABIN VERTICAL ATTACH FITTING, FS 802, RBL 40. REPLACED FITTING PER SRM 51-1-20D.Jan 2, 1996 · N810UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS805375Fitting · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, 2ND DR. LATCH FITTING FROM FORWARD LOWER SIDE OF A B/B DR. HAS CORROSION AND CRACKS. REPLACED FITTING PER SRM 50-1-20.Dec 31, 1995 · N701UP · Doug DC871F · Cargo/Baggage Doors
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