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 IXXA0500137SSpar Cap · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACKED BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CORROSION FROM SLANT PANEL UPPER CAP. FOUND OUT OF LIMITS. CLEANED, TREATED AND PRIMED AREA. Mar 8, 2005 · N821BX · Doug DC871F · Wing SparSDR IXXA0500136SDoubler · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGES CENTER SECTION FORWARD CARGO COMPARTMENT FORWARD DOOR AFT JAMB INTERNAL DOUBLER CORROSION DAMAGE STA 335.000 L-35R 35L. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED EXISTMar 7, 2005 · N821BX · Doug DC871F · Cargo/Baggage DoorsSDR IXXA0500017OCable · looseUPON APPROACH TO SCHEDULED LANDING AT KTOL, FLAP SELECTOR HANDLE WOULD ALLOW 5 DEGREES TO BE SELECTED AND STOP. AFTER STAYING IN HOLDING PATTERN FOR APPOX 15-20 MINUTES FLAPS OPERATED NORMALLY. AIRCRAFT MADE UNEVENTFUL LANDING IN KTOL. UPON INSPECTION MX NOMar 5, 2005 · N829BX · Doug DC871F · Trailing Edge Flap Control SystemSDR IXXA0500139SRib · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT OUTBOARD PYLON STUB WING N 4 RIB EXTENDED LEADING EDGE CRACK DAMAGE AT STA XOLDO 67.750. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGE. FABRICATED NEW RIB. PERFORMED NDT INSPECTION, CLEANED, TREATED AND PRIMED AREMar 4, 2005 · N821BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA0500138SPanel · dentedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP AFT PANEL DENT DAMAGE BETWEEN STA XF 304.000-XF 333.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING, CLEANED, TREATED AND PRIMED AREA + INNER FACE ON NEW PLATINMar 4, 2005 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500135SFrame · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE FORWARD ACCESSORY COMPARTMENT STRUCTURE FRAME CRACK DAMAGE AT STA FS 55.00, L-24L. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND CRACKED FRAME SEGMENT. PERFORMED AN NDT INSPECTION. FABRICATED FRAMEMar 4, 2005 · N821BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500133SFrame · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE FORWARD ACCESSORY COMPARTMENT STRUCTURE FRAME CRACK DAMAGE AT STA FS 55.00,L-24R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS FROM REPAIR AREA. REMOVED DAMAGED FRAME SEGMENT. PERFORMED NDT INSPECTIONMar 4, 2005 · N821BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500126SFrame · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE FORWARD ACCESSORY COMPARTMENT STRUCTURE FRAME CRACK DAMAGE STA FS 55.00 L-24R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVAL OF DAMAGED AREA FRAME SEGMENT. PERFORMED NDT INSPECTION, FABRICATED Mar 4, 2005 · N821BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500156SAccess Door · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER LOWER AFT JAMB CORNER RAM AIR EXHAUST ACCESS DOOR COMPARTMENT CRACK DAMAGE AT STA FS -12.00, L-27R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING FILLER AND DAMAGED SMar 3, 2005 · N821BX · Doug DC871F · Service DoorsSDR IXXA0500149SPanel · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AROUND STA XRS 71.000, S-7 TO S-8. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS FROM REPAIR AREA AND PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER AND FILLER Mar 3, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500140SRepair · missingDURING A ROUTINE C CHECK INSPECTION, FOUND FUSELAGE AFT CENTER SECTION LOWER PLATING DRAIN HOLE REPAIR DOUBLER MISSING ONE ROW FASTENERS AT STA 180.000, L-35 RT TO L-36. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR DOUBLER. FABRICATED EXTERNAL REPAIRMar 3, 2005 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500123SSpar Cap · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING UPPER FRONT SPAR CAP STRUCTURE CRACK DAMAGE BETWEEN STA XFS-6 CAP. MAJOR REPAIR ACCOMPLISHED BY REMOVING FASTENERS. REMOVING CORROSION FROM SLANT PANEL UPPER CAP AND FOUND OUT OF LIMITS. CLEANED, TREATED ANMar 3, 2005 · N821BX · Doug DC871F · Wing SparSDR IXXA0500122SRepair · improperDURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD FLAP LOWER AFT PLATING INTERIM REPAIR AROUND STA XF 385.00. MAJOR REPAIR ACCOMPLISHED BY REMOVING EXISTING REPAIR IAW DC8 SRM 51-1-11 PG1, DC8 SRM 51-3-0 PG1. REMOVED DAMAGED AREA IAW DC8 SRM 57-2-5N FIG Mar 3, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500155SPlate · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RT INNER WING FWD TOP PANEL PLATING WITH CRACK DAMAGE AT STA XRS 74.869, S-14. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED REPAIR DOUBLER AND FILLER PLUG. CLFeb 28, 2005 · N821BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA0500148SFastener · missingDURING A ROUTINE C CHECK INSPECTION, FOUND WING TO FUSELAGE LOWER PLATING DRAIN HOLE REPAIR MISSING ONE ROW OF FASTENERS AT STA FS 620.000, L-35R TO L-35R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING DOUBLER AND FASTENERS WITHIN REPAIR AREA AND REMOVED DAMAFeb 28, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500142SFastener · missingDURING A ROUTINE C CHECK INSPECTION, FOUND AFT CENTER SECTION LOWER PLATING DRAIN HOLE REPAIR ONE ROW FASTENERS MISSING STA 1380.000 L-35 RT L-36. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVED DAMAGED SECTION AND PERFORMED NDT INSPECTION. FAFeb 28, 2005 · N821BX · Doug DC871F · Fuselage Structure (General)SDR UPS05843967Throttle · stuckNR 2 THROTTLE STUCK IN IDLE DURING VISUAL APPROACH. NR 2 AND NR 3 REVERSERS USED IN FLIGHT PRIOR TO APPROACH. DURING T/S RAN ENG NR 2 & CYCLED T/R 3 TIMES AFTER CYCLING T/R THROTTLE CLD ONLY ADVANCE 2-3 BEFORE JAMB WITH ENG SHUTDOWN THROTTLE WLD MOVE FULL TRFeb 26, 2005 · N729UP · Doug DC871F · Power LeverSDR IXXA0500151SPlate · dentedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP UPPER AFT PLATING DENT DAMAGE AT STA XW 110.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING AND FINGER DOUBLER. CLEANED, TREATED AND PRIMED NEW PLATING INTERNAFeb 25, 2005 · N821BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA0500150SPlate · crackedDURING A ROUTINE C CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGED AT STA XRS 74.869, S-5. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. PERFORMED NDT INSPECTION AND FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CFeb 25, 2005 · N821BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA0500147SRepair · improperDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP FORWARD UPPER PLATING INTERIM REPAIR AT STA XW 87.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR AND THE DAMAGED AREA. FABRICATED NEW PLATING SEGMENT + INTERNAL SPLICE, EXTERNAL DOUBLFeb 25, 2005 · N821BX · Doug DC871F · Wing Main, Frame StructureSDR IXXA0500145SSkin · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING FORWARD TOP PANEL PLATING CRACK DAMAGE AT STA XRS 144.00 FRONT SPAR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOUBLER AND FILLER PLUG. Feb 25, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500144SLongeron · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE TAIL SECTION STRUCTURE LONGERON 17 RT HAS CRACK DAMAGE STA 1770.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED LONGERON. FABRICATED NEW LONGERON, CLEANED, TREATED AND PRIMED AREA. APPLIED SEALANT TO FAFeb 25, 2005 · N821BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0500143SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION, FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING INTERNAL CORROSION DAMAGE AROUND STA FS 1540.00, L-25R TO L-26R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION AND FOUND OUT OF LIMITS. REMOVED FASTENERS FROM REPAIR AREAFeb 24, 2005 · N821BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500134SPanel · crackedDURING A ROUTINE C-CHECK INSPECTION FOUND RT INNER WING AFT TOP PANEL PLATING CRACK DAMAGE AT STA XRS 74.869, S-2. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED SECTION. FABRICATED EXTERNAL DOUBLER + FILLER PLUG. CLEANED, TREATED AND PRIMED AREFeb 24, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500125SRepair · improperDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING INBOARD FLAP AFT LOWER PANEL INTERIM REPARI AT STA XW 34.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVAL OF DAMAGED SECTION. PERFORMED NDT INSPECTION, FABRICATED NEW PLATING SEGMENT, INTEFeb 24, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500124SRepair · improperDURING A ROUTINE C CHECK, INSPECTION FOUND LT WING INBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIRS BETWEEN STA XW 87.000 AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR, AND REMOVED PLATING SEGMENT. PERFORMED NDT INSPECTION AND FABRICAFeb 23, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500141SRepair · unknownDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR STA XF 417.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGE FROM AREA. PERFORMED A NDT INSPECTION TO AREA AND FABRICATED A REPAIR DOUBLER AND Feb 19, 2005 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500154SPlate · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND LT OUTER WING INBOARD EXTENDED LEADING EDGE ELONGATED HOLE AROUND STA XFS 710.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF PLATING WITH IMPROPER REPAIR. FABRICATED NEW PLATING, CLEANED, TREATED AND PRIMED AREA AND NEW Feb 18, 2005 · N821BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA0500152SDoor Frame · wornDURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE AFT CENTER SECTION AFT CARGO COMPARTMENT AFT DOOR AFT JAMB WEAR DAMAGE AT STA FS 1440.00, L-30R TO L-31R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS AND DAMAGED AREA. PERFORMED AN NDT INSPECTION, FABRICATEFeb 17, 2005 · N821BX · Doug DC871F · Fuselage Main, StructureSDR IXXA0500153SPlate · dentedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP LOWER AFT PLATING DENTS DAMAGE BETWEEN STA XF 415.000 AND XW 408.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN. FABRICATED NEW SKIN, CLEANED, TREATED AND PRIMED AREA + NEW SKIN INTERNAFeb 17, 2005 · N821BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA0500132SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD FLAP UPPER FORWARD PLATING INTERIM REPAIR STA XF 227.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING AREA. PERFORMED AN NDT INSPECTION. FABRICATED NEW PLATING SEGMENT, INTERNAL SPLICE AND Feb 14, 2005 · N821BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500131SFastener · missingDURING A ROUTINE C-CHECK INSPECTION FOUND RT FUSELAGE AFT CENTER SECTION LOWER PLATING OLD OMEGA ANTENNA DOUBLER MISSING ON ROW FASTENERS AND MAX PITCH EXCEEDS LIMITS AT STA FS 1322.00L, 35.5R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF EXISTING REPAIR. REMOVED DAFeb 14, 2005 · N821BX · Doug DC871F · Fuselage Main, StructureSDR IXXA0500129SSkin · wornDURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE AFT CENTER SECTION AFT CARGO COMPARTMENT AFT DOOR FWD JAMB WEAR DAMAGE AT STA FS 1400.00, L-30R TO L-31R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS. REMOVED DAMAGED SECTION. PERFORMED NDT INSPECTION. FAFeb 14, 2005 · N821BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA0500127SSkin · damagedDURING A ROUTINE C CHECK INSPECTION, RT FUSELAGE FORWARD PASSENGER ENTRANCE DOOR UPPER AFT JAMB PLATING WEAR DAMAGE AT STA FS 25.000, L-21R. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGE. FABRICATED NEW SKIN, CLEANED, TREATED AND PRIMED AREA + NEW SKIN. APPLIFeb 14, 2005 · N821BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA0500128SRepair · damagedDURING A ROUTINE C CHECK INSPECTION, RT WING INBOARD FLAP AFT UPPER PLATING INTERIM REPAIRS AND DENT DAMAGE BETWEEN STA XW 2.00 CANT AND XW 91.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED PLATING. FABRICATED NEW PLATING. CLEANED, TREATED AND PRIMED AREFeb 13, 2005 · N821BX · Doug DC871F · Wing, Plate/SkinSDR UPS05843869Actuator · malfunctionedCREW LOST NR 2 INS WITH A WARNING LIGHT. SMELLED ELECTRICAL FUMES FROM PEDESTAL AREA. TURNED NR 2 INS OFF. NOTICED PTC WAS NOT FULLY RETRACTED AND HAD 3/8 EXTENSION SHOWING. FOLLOWED PROCEDURES FOR PTC NOT FULLY RETRACTED. CREW DECLARED EMERGENCY W/TULSA.Feb 9, 2005 · N748UP · Doug DC871F · Elevator Control SystemSDR IXXA0500191SVane · delaminatedDURING ROUTINE C-CHECK FOUND LEFT HAND OUTBOARD FLAP INBOARD FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE, RIG CHECK GOOD IAW DC8 MM 27-51-14.Feb 8, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500204SSeat Track · crackedDURING ROUTINE C-CHECK FOUND FLIGHT DECK COUIER SEAT TRACK AFT TRACK CRACKED ON END. REMOVED DAMAGE, MANUFACTURED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 51-1-8, AND 51-1-21.Feb 4, 2005 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0500192SVane · delaminatedDURING ROUTINE C-CHECK FOUND LEFT HAND FLAP STATION 219 FLAP VANE DELAMINATED. REMOVED AND REPLACED FLAP VANE, RIG CHECK GOOD IAW DC8 MM 27-51-14.Feb 4, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500188SSeat Track · gougedDURING ROUTINE C-CHECK FOUND MAIN CABIN SEAT TRACK GOUGED AT STATION 235 LEFT BUTT LINE 45.5. GOUGE IS OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-Feb 3, 2005 · N820BX · Doug DC871F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0500168SBushing · migratedDURING A ROUTINE C- CHECK FOUND NUMBER 3 ENGINE OUTBOARD THRUST REVERSER TRANSITION COWL BUSHING MIGRATED AT FRICTION PAD. REPAIRED MIGRATING BUSHING BY REMOVING FASTENERS, REMOVING DAMAGED EDGE ANGLE, FABRICATING NEW ANGLE AND BONDING INTO PLACE. ALODINED, Feb 2, 2005 · N820BX · Doug DC871F · Engine Thrust ReverserSDR IXXA0500165SAngle · crackedDURING ROUTINE C-CHECK FOUND SUPPORT ANGLE CRACKED AT THE RIGHT WHEEL WELL STATION 790 LONGERON 23 RIGHT SWING DOWN PANEL. MANUFACTURED REPAIR ANGLES. LOCATED, DRILLED, TRIMMED, ALODINED, PRIMED, AND INSTALLED REPAIR ANGLES IAW DC8 DRAWING 5643404, DC8 SRM 5Jan 31, 2005 · N820BX · Doug DC871F · Wing Miscellaneous StructureSDR UPS05843806Warning Light · illuminatedINSPECTION TYPE:N/A ATB - NR 4 ENG OIL PRESS LIGHT CAME ON IN FLT. OIL PRESS AT CLIMB THRUST WAS 60 & OPS AFTER SHUTDOWN (WINDMILLING). NR 4 ENG LOW OIL PRESSURE LIGHT DEFERRED PER MEL 79-6 OIL PRESSURE & OIL QTY WERE NORMAL PER FLT CREW, PLACARD INSTALLED MJan 28, 2005 · N772UP · Doug DC871F · Engine Oil Indicating SystemSDR IXXA0500203SFloorboard · delaminatedDURING ROUTINE C-CHECK FOUND CABIN FLOORBOARD DELAMINATED AT STATION 1120 TO STATION 1260 RIGHT BUTT LINE 54. REMOVED DAMAGED FLOORBOARD, MANUFACTURED NEW FLOORBOARD, LOCATED, DRILLED AND INSTALLED NEW FLOORBOARD IAW DC8 SRM 51-3-0, 51-1-11 AND DOUGLAS SPEC 3Jan 27, 2005 · N820BX · Doug DC871F · Fuselage Floor PanelSDR IXXA0500190SWeb · crackedDURING ROUTINE C-CHECK FOUND LEFT HAND PASSENGER DOOR FORWARD WEB JUST ABOVE OPENING MECHANISM CRACKED. STOP DRILLED CRACK AND FABRICATED DOUBLER. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED DOUBLER AND FASTENERS IAW DC8 SRM 52-3-2, 52-2-0 51-1-21, AND 5Jan 27, 2005 · N820BX · Doug DC871F · Passenger/Crew DoorsSDR IXXA050185SRib · crackedDURING ROUTINE C-CHECK FOUND FORWARD RIGHT HAND SERVICE DOOR UPPER INTERNAL RIB CRACKED. STOP DRILLED CRACK. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0, 52-3-0, 51-9-0 AND 51-1-8.Jan 27, 2005 · N820BX · Doug DC871F · Service DoorsSDR IXXA0500170SFrame · crackedDURING A ROUTINE C-CHECK FOUND FRAME JUST AFT OF AIRSTART COMPARTMENT CRACKED AT 2 LOCATIONS. REMOVED FASTENERS, AND DAMAGED AREA. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS, IAW DC8 SRM 53-2-0, 51-1-20D, 51-3-0, 5Jan 27, 2005 · N820BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500202SShroud · wornDURING ROUTINE C-CHECK FOUND, NR 3 ENGINE INLET FAN ABRADABLE SHROUD WORN, APPROXIMATELY 40 PERCENT MATERIAL MISSING. REMOVED 2 ACOUSTICAL PANELS, AND DAMAGE. CLEANED AREA AND APPLIED FIBERGLASS REPAIR IAW CFM56 MM 72-33-00.Jan 26, 2005 · N820BX · Doug DC871F · Engine Cowling SystemSDR IXXA050197SDoubler · gougedDURING ROUTINE C-CHECK FOUND LEFT OUTBOARD TRAILING EDGE FLAP UPPER SKIN REPAIR PATCH GOUGED AT CENTER HINGE. REMOVED FASTENERS AND DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW DOUBLER, AND FASTENERS IAW DC8 SRM 5Jan 26, 2005 · N820BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500186SAngle · crackedDURING ROUTINE C-CHECK FOUND LEFT WING OUTBOARD FLAP INBOARD CENTER AFT INSIDE PANEL NUMBER 551 AREA ANGLE CRACKED AND 3 FASTENERS MISSING. REMOVED FASTENERS, AND ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW ANGLE AND INSTJan 26, 2005 · N820BX · Doug DC871F · Trailing Edge Flaps
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