Douglas DC-8-71F

Service difficulty reports · 8,938

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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 = 'DC871F'
  ORDER BY difficulty_date DESC"

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SDR UPS802183Skin Doubler · corrosionDURING 'C' CHECK, MAINTENANCE FOUND SKIN DOUBLER HEAVY CORROSION UNDER SHEAR TIE, FS 1600, LONGERON 28R. INSTALLED REPAIR IAW UPS EO DC8-53-1310 (MINOR).Feb 6, 1995 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR UPS802182Longeron · corrosionDURING 'C' CHECK, MAINTENANCE FOUND INTERGRANULAR CORROSION ON LONGERON 31L, FS 1560. INSTALLED REPAIR IAW UPS EO DC8-5310-6606-A.Feb 6, 1995 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS802187Eel Disarm · inopDURING POST FLIGHT CHECK, MAINTENANCE FOUND EMER DISARM CHECK INOP. SECURED OVERHEAD PANEL CAMLOCS (2 EACH) EMER DISARM CHECK. CHECKS NORMAL. EMER LIGHTS, OPS CK NORMAL.Feb 4, 1995 · N772UP · Doug DC871F · Emergency LightingSDR UPS802188Door Jamb · crackWHILE IN 'B' CHECK MAINTENANCE REPORTED LT AFT SERVICE DOOR AFT UPPER CORNER OF FUSELAGE CUTOUT STA 1660-6 CRACKS COMING FROM FASTENER HOLES. REPAIRED PER EO DC8-5330-4067-A. DOOR JAMB CORNER DAMAGE - TEMP REPAIR.Feb 2, 1995 · N755UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS802130Vane · delaminatedDURING 'C' CHECK MAINTENANCE FOUND RT WING NR 2 FLAP VANE DELAMINATED ON UPPER SURFACE. REPLACED VANE PER MM 27-51-14.Feb 2, 1995 · N707UP · Doug DC871F · Trailing Edge FlapsSDR UPS802129Rib · crackedDURING 'C' CHECK MAINTENANCE FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STA XFS 660. REPAIRED RIB PER MM 57-00-00.Feb 2, 1995 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS802128Vane · delaminatedDURING 'C' CHECK MAINTENANCE FOUND LT AND RT WING NR 5 FLAP VANES DELAMINATED ON UPPER SURFACES. REPLACED VANE ASSY PER MM 27-51-14.Feb 2, 1995 · N707UP · Doug DC871F · Trailing Edge FlapsSDR UPS802127Vane · delaminatedDURING 'C' CHECK MAINTENANCE FOUND LT AND RT WING NB 6 FLAP VANES DELAMINATED ON UPPER SURFACES. REPLACED VANE ASSY PER MM 27-51-14.Feb 2, 1995 · N707UP · Doug DC871F · Trailing Edge FlapsSDR UPS802126Ribs · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 9, 11, 12, 14, AND 16 UPPER RIBS CRACKED ON UPPER SURFACES. INSTALLED REPAIRS IAW MM 57-00-00, FIG. 801. (P/N 5769589, 5720123).Jan 31, 1995 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS802125Ribs · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 17, 21, 24, AND 27 UPPER RIBS CRACKED IN UPPER SURFACES. INSTALLED REPAIRS IAW MM 27-00-00, FIG. 801. (P/N 5769589, 5720123).Jan 31, 1995 · N707UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS802124Longeron · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND 4 INCH LONG CRACK AT LONGERON 36, FS 260-265. INSTALLED REPAIR IAW SEM 53-2-2, FIG. 10.Jan 31, 1995 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS802123Longeron · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND 4 INCH LONG CRACK AT LONGERON 36, FS 260-265. INSTALLED REPAIR IAW SEM 53-2-2, FIG. 10.Jan 31, 1995 · N707UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS802122Skin Doubler · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND FUSELAGE SKIN DOUBLER HAS 1 INCH LONG CRACK. RT AND LT AFT HEAT EXCHANGER CUTOUT LOWER AFT CORNERS. INSTALLED REPAIR IAW UPS EO DC8-5330-4732D.Jan 31, 1995 · N707UP · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9545Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS LOCATED AT THE FORWARD LOWER CARGO DOOR TRACK FITTING. THE FITTING WAS REMOVED AND MANUFACTURED IAW DRAWING HSE27-53-143 AND THE REMOVED FITTING. THIS DRAWING WAS FAA DER APPROVED. THE FITTING WAS INSTALLED IAWJan 31, 1995 · N825BX · Doug DC871F · Cargo/Baggage DoorsSDR UPS802110Battery Pack · dischargedMAINTENANCE REPORTED EMERGENCY EXIT LIGHTS FAILED OPS TEST. REMOVED AND REPLACED BATTERY PACK. OPS CHECK GOOD.Jan 29, 1995 · N744UP · Doug DC871F · Emergency LightingSDR UPS802109Frame · corrosionWHILE IN 'C' CHECK, MAINTENANCE FOUND DURING A CORROSION BULGE INSPECTION, FRAME HEAVILY CORRODED ON OPEN UP AT FS 20, LONGERON 33R. INSTALLED REPAIR IAW SRM 53-2-0.Jan 27, 1995 · N707UP · Doug DC871F · Fuselage Main, FrameSDR UPS802108Fitting · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D.Jan 27, 1995 · N707UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS802107Support Fitting · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND FS 680 TO FS 687, LONG 22R FRONT SPAR/WING SKIN SUPPORT FITTING HAS HEAVY CORROSION. INSTALLED REPAIR IAW SRM 51-1-20D.Jan 27, 1995 · N707UP · Doug DC871F · Wing Miscellaneous StructureSDR IXXA9548Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION REMOVAL FROM THE EXTERNAL PLATING AT FS 610 BETWEEN LONGERONS 29 AND 31 WENT BEYOND SRM LIMITS. THE DAMAGE WAS REPAIRED IAW DRAWING BSE27-53-140, WHICH WAS FAA DER APPROVED AND E.O. 53-DC8-137. (X)Jan 24, 1995 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9547Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE LOWER FORWARD CARGO DOOR, LOCK FITTING WAS FOUND CRACKED. THIS FITTING WAS LOCATED AT THE SECOND POSITION FORWARD. THE FITTING WAS REMOVED AND MANUFACTURED IAW DRAWING HSE27-52-142, WHICH WAS FAA DER APPROVED AND E.O. 5Jan 24, 1995 · N825BX · Doug DC871F · Cargo/Baggage DoorsSDR UPS802086Escape Slide · low pressureMAINTENANCE REPORTED EVACUATION SLIDE BELOW LIMITS. REMOVED AND REPLACED EVAC SLIDE IAW 25-60-01.Jan 22, 1995 · N713UP · Doug DC871F · Escape SlideSDR IXXA9546Plating · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND AT THE AFT NOSE WHEELWELL DOOR CUT OUT IN EXTERNAL PLATING. REPAIR OF THE CRACK IN THE LEFT AFT CORNER WAS ACCOMPLISHED BY STOP DRILLING THE CRACK, INSTALLING AN EXTERNAL REPAIR DOUBLER. REPAIR WAS ACCOMPLJan 18, 1995 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9535Fitting · crackedDURING REPLACEMENT OF LT MLG TRUNNION FITTING, INSPECTION FOUND LT SPAR CAP FITTING CRACKED. THE SPAR CAP FITTING WAS REPLACED IAW DOUGLAS INSTALLATION GUIDE, THE AIRCRAFT SRM, AND MM. (X)Jan 18, 1995 · N821BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA9532Angle · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACKED ANGLE ON THE RT AFT SERVICE DOOR WAS NOTED. THE ANGLE WAS REMOVED AND LOCALLY MANUFACTURED IAW DRAWING N821BX-04 WHICH WAS FAA DER APPROVED. THE NEW ANGLE WAS INSTALLED IAW AIRCRAFT SRM AND MM. (X)Jan 16, 1995 · N821BX · Doug DC871F · Service DoorsSDR IXXA9529Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A 1 INCH CRACK WAS FOUND AT FS 280, AND LONGERON 36. REPAIR OF THE CRACK WAS ACCOMPLISHED IAW AIRCRAFT SRM. (X)Jan 9, 1995 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9528Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS LOCATED AT THE NOSE WHEELWELL DOOR CUT-OUT. THE EXTERNAL PLATING WAS CRACKED AT THE RIGHT AFT CORNER. REPAIR OF THE CRACK WAS ACCOMPLISHED IAW AIRCRAFT SRM 53-2-1 WHICH INSTALLED AN EXTERNAL REPAIR DOUBLER. (X)Jan 9, 1995 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA9526Bulkhead Web · crackedDURING ROUTINE C-CHECK, A 1 INCH CRACK WAS LOCATED IN THE AFT PRESSURE BULKHEAD, FS 1766, AT LONGERON 11 LEFT. REPAIR WAS ACCOMPLISHED IAW AIRCRAFT SRM AND SB 53-73. (X)Jan 9, 1995 · N821BX · Doug DC871F · Fuselage Main, BulkheadSDR IXXA9534Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACKED FITTING ON THE LT AFT SERVICE DOOR WAS FOUND. THE FORWARD UPPER FITTING EXHIBITED A .250 INCH CRACK. THE FITTING WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM. (X)Jan 6, 1995 · N821BX · Doug DC871F · Service DoorsSDR UP801915Beam · crackMAINTENANCE REPORTED APPROX 1.75 INCH CRACK AT BOTTOM RADIUS OF NR 3 ANGLE (BEAM) ON PRESSURE BULKHEAD AT CENTER. INSTALLED REPAIR IAW EO DC8-6310-6306A, TEMP REV 53-81, 53-7-0.Jan 5, 1995 · N700UP · Doug DC871F · Fuselage Main, BulkheadSDR UPS801908Connector · loosePILOT REPORTED, LEFT MLG DOES NOT INDICATE DOWN AND LOCKED WITH GEAR HANDLE DOWN. CYCLED GEAR 3 TIMES. ERM CHECKLIST COMPLETED WITH REQUIRED VISUAL FLY BY (CHANGED BULBS-DID NOT WORK). FOUND PLUG P1-213 LOOSE AND CONTAMINATED. CLEANED AND SECURED PLUGS ANDJan 4, 1995 · N797UP · Doug DC871F · Landing Gear Position and WarningSDR IXXA9527Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE RIGHT LEADING EDGE. THE CRACK MEASURED 6 INCHES AND WAS LOCATED AT XFS 585. THE REPAIR WAS ACCOMPLISHED IAW AIRCRAFT SRM. SRM REFERENCE 57-2-1. (X)Jan 4, 1995 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA9525Longeron · corrodedDURING ROUTINE C-CHECK AND CORROSION PREVENTION AND CORROSION CONTROL INSPECTION, LEVEL 2 CORROSION WAS FOUND BETWEEN FS 980 AND FS 1060, LONGERON 31 LEFT. THE LONGERON WAS REMOVED AND REPLACED IAW AIRCRAFT SRM. CORROSION DAMAGE WAS CONFINED TO THE LONGERON.Jan 4, 1995 · N821BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS801907Prox Switch · malfunctionPILOT REPORTED DOORS NOT LATCHED LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. COMPLIED WITH CHECK LIST AND CYCLED GEAR, WORKED NORMAL. REMOVED AND REPLACED RT MLG DOOR PROX SWITCH WITH SERVICEABLE UNIT. PERFORMED OPS CHECK OK.Jan 3, 1995 · N708UP · Doug DC871F · Landing Gear Position and WarningSDR IXXA9537Trunnion · crackedDURING ROUTINE C-CHECK INSPECTION, THE LT MLG TRUNNION FITTING WAS FOUND CRACKED. INSPECTION WAS ACCOMPLISHED IAW SB 57-94. THE CRACK WAS LOCATED, 8 INCHES, IN THE FORWARD LANDING GEAR ATTACH LUG. THE FITTING WAS REMOVED AND REPLACED IAW DOUGLAS INSTALLATIOJan 3, 1995 · N821BX · Doug DC871F · Wing, Landing Gear Attach FittingsSDR IXXA9536Longeron · crackedDURING ROUTINE C-CHECK INSPECTION. LONGERON 24 WAS FOUND WITH 2 CRACKS. THE RT LONGERON 24 HAD BOTH A 7 INCH AND 1 INCH CRACK AT SEPARATE LOCATIONS. THE LONGERON WAS REMOVED AND REPLACED IAW THE AIRCRAFT SRM, DOUGLAS INSTALLATION GUIDE, AND THE MM. (X)Jan 3, 1995 · N821BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA9533Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, A 1.25 INCH CRACK WAS FOUND ON THE STA 857 FITTING OF LONGERON 24. REPAIR ON THE LONGERON FITTING WAS ACCOMPLISHED IAW THE AIRCRAFT SRM. SRM REFERENCE 53-2-2. (X)Jan 3, 1995 · N821BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA9531Skin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND IN THE PLATING OF THE LT FORWARD ENTRY DOOR. THE CRACK WAS LOCATED AT THE UPPER AFT CORNER. REPAIR TO THE EXTERNAL PLATING WAS ACCOMPLISHED IAW AIRCRAFT SRM. (X)Jan 3, 1995 · N821BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA9530Fitting · crackedDURING ROUTINE C-CHECK INSPECTION. LONGERON AND FITTINGS AT SEVERAL LOCATIONS WERE FOUND CRACKED. END FITTINGS AT FS 260, AND LONGERONS 34 AND 35 LEFT AS WELL AS LONGERON 36. ALL FITTINGS WERE REPLACED WITH NEW IAW AIRCRAFT SRM. (X)Jan 2, 1995 · N821BX · Doug DC871F · Fuselage Miscellaneous Structure
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