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 XXA060086SDoubler · crackedDURING ROUTINE C-CHECK, FOUND EXISTING DOUBLER CRACKED AT STATION 1620 BETWEEN LONGERON 17 LEFT AND 24 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER AND Oct 7, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060083SWeb · crackedDURING ROUTINE C CHECK, FOUND WEB CRACKED FROM STATION 920 TO 940 AT -X25, Z0. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER AND REPAIR DOUBLER AND FASTENERS FROM STATION 935.250 TO STATION 938.75Oct 7, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060053SAngle · crackedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE LOWER ANGLE CRACKED AT STATION XE 29.77. REMOVED DAMAGE, FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND FASTENERS IN LEFT HORIZONTAL Oct 7, 2004 · N825BX · Doug DC871F · Horizontal Stabilizer Miscellaneous StructureSDR IXXA060045SAttach Fitting · corrodedDURING ROUTINE C-CHECK FOUND MAIN CARGO CABIN SUPPORT END FITTING CORRODED AT STATION Y55 -X65 Z0. REMOVED FASTENERS AS NEEDED TO REMOVE END FITTING. MANUFACTURED NEW END FITTING, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW END FITTING AND FASTENERS AT STOct 7, 2004 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA060044SCusp Web · corrodedDURING ROUTINE C-CHECK FOUND RT CUSP HORIZONTAL FLANGE CORRODED AT STATION 30 LONGERON 21 RT. REMOVED AIR CONDITIONING DUCTS. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND FASTENERS AT STATION Oct 7, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060043SWeb · corrodedDURING ROUTINE C CHECK, FOUND FLOOR PANEL CORRODED FROM STATION 40 TO STATION 55 BETWEEN +X60 AND -X60.7=0. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGED FLOOR PANEL WEB. FAB`D NEW WEB, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FLOOR PANEL WEB FROOct 7, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060042SFitting · crackedDURING ROUTINE C CHECK FOUND LONGERON 1 FITTING CRACKED AT STATION 650. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. MANUFACTURED NEW FITTING, LOCATED DRILLED TREATED, PRIMED, INSTALLED FITTING AND FASTENERS WET WITH SEALANT AT LONGERON 1 STATION 65Oct 7, 2004 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843310Battery Pack · will not testEMERGENCY LIGHTING WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK, GROUND OPS CHECK NORMAL.Oct 7, 2004 · N705UP · Doug DC871F · Emergency LightingSDR IXXA060077SWeb · crackedDURING ROUTINE C CHECK, FOUND WEB CRACKED IN THE AFT CARGO COMPARTMENT, AFT DOOR JAMB FROM STATION 1440 TO STATION 1446 BETWEEN LONGERON 32 RT AND LONGERON 34 RT. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLEDOct 6, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060029SFrame · crackedDURING ROUTINE C-CHECK FOUND LT FRAME CRACKED AT STATION 1978. REMOVED EXISTING FASTENERS, AND FRAME. FABRICATED FRAME, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS WET WITH SEALANT. IAW SRM 53-2-051-1-21, 53-5-1, 51-1-4, 51-1-5, ANOct 6, 2004 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA060023SSkin · corrodedDURING ROUTINE C CHECK, FOUND THE LT WING UPPER SURFACE CORRODED AT STATION XFS304. REMOVED LEFT WING CENTER SECTION LEADING EDGE TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLEDOct 6, 2004 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA060022SSkin · corrodedDURING ROUTINE C-CHECK FOUND LT WING UPPER SURFACE CORRODED BEOND LIMITS AT STATION XRS111.000 AT FORWARD SPAR. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLEROct 6, 2004 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0500227SAngle · crackedDURING ROUTINE C-CHECK FOUND RIGHT HAND CUSP CRACKED AT STATION 1050 LONGERON 21 RIGHT. CLEANED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 51-21-1, 51-2-1, 51-1-5 AND 51-1-8.Oct 6, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060091SRib · crackedDURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 404. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT STATOct 5, 2004 · N825BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060090SRib · crackedDURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 397.75. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT SOct 5, 2004 · N825BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060076SWeb · crackedDURING ROUTINE C-CHECK, FOUND WEB CRACKED IN THE AFT CARGO COMPARTMENT STATION 1267 BETWEEN +X40 AND -Z8. REMOVED DAMAGED AREA. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER AND FASTENERS FROM STATION 1265 TO 1269 BETWEEN +XOct 5, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060075SSupport Channel · crackedDURING ROUTINE C CHECK FOUND FLOOR SUPPORT CHANNEL CRACKED IN THE AFT CARGO COMPARTMENT AT STATION 1263 BETWEEN LONGERON 33 LEFT AND 34 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPORT CHANNEL, FABRICATED NEW FLOOR SUPPORT CHANNEL, LOCATED, DROct 5, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060074SBulkhead · crackedDURING ROUTINE C CHECK, FOUND WEB CRACKED AT STATION -175 FORWARD BULKHEAD LOWER SECTION. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED WEB. FABRICATED WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND FASTENERS AT STATION -175 FORWARD BOct 5, 2004 · N825BX · Doug DC871F · Fuselage Main, BulkheadSDR IXXA060073SRib · crackedDURING ROUTINE C CHECK, FOUND RIB CRACKED AT STATION -175 FORWARD BULKHEAD RIGHT LOWER SECTION. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FASTENERS AT STATION -17Oct 5, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060030SFrame · crackedDURING ROUTINE C-CHECK FOUND RT FRAME CRACKED AT STATION 1978. REMOVED EXISTING FASTENERS, AND FRAME. FABRICATED FRAME, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED FRAME AND FASTENERS WET WITH SEALANT. IAW DC8 SRM 53-2-051-1-21, 53-5-1, 51-1-4, 51-1-5Oct 5, 2004 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA060027SSkin · crackedDURING ROUTINE C-CHECK FOUND LT WING IB FLAP LEADING EDGE UPPER SKIN CRACKED AT STATION XW84. REMOVED FLAP VANE, AND NOSE PANEL TO FACILITATE REPAIR. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED DOUBLOct 5, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060026SSkin · dentedDURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP UPPER SURFACE DENTED OUT OF LIMITS AT STATION XW35. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANT FROM STOct 5, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060025SSkin · dentedDURING ROUTINE C-CHECK FOUND LT WING IB TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39 AFT AREA. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALANTOct 5, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060024SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE DENTED OUT OF LIMITS AT STATION XW39. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, REMOVED, TREATED, PRIMED, AND INSTALLED FILLER AND DOUBLER WET WITH SEALAOct 5, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060019SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED AT STATION XF208. REMOVED FASTENERS AS NEEDED TO REMOVE RIGHT WING OUTBOARD FLAP LOWER SKIN FROM STATION XF169 TO STATION XF213. FABRICATED, NEW SKIN AND FINGER DOUBLERS, LOCATED, DRILLOct 5, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060016SSkin · delaminatedDURING ROUTINE C CHECK, FOUND RIGHT HAND WING SPOILER NUMBER 3 DELAMINATED AT STATION XRS 218. REMOVED RIGHT HAND NUMBER 3 SPOILER. REMOVED UPPER, LOWER SKIN AND HONEYCOMB CORE. FABRICATED NEW REPAIR PARTS. INSTALLED AND BONDED REPAIR PARTS IN NUMBER 3 RIGOct 5, 2004 · N825BX · Doug DC871F · SpoilersSDR IXXA0500233SLongeron · crackedDURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 100 LONGERON 7 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, 51-1-5 AND 51-1-8.Oct 5, 2004 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0500232SLongeron · crackedDURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 100 LONGERON 9 RIGHT. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, 51-1-5 AND 51-1-8.Oct 5, 2004 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0500231SLongeron · crackedDURING ROUTINE C-CHECK FOUND LONGERON CRACKED AT STATION 280 LONGERON 7 RIGHT. CLEANED DAMAGE FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 53-4-1, AND 51-1-8.Oct 5, 2004 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0500230SLongeron · crackedDURING ROUTINE C-CHECK FOUND A CRACKED LONGERON AT STATION 1747 LONGERON 15 RIGHT. CLEANED DAMAGED AREA, FABRICATED REPAIR PARTS, LOCATED, DRILLED TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND FASTENERS IAW DC8 SRM 53-2-2, 52-1-5, AND 51-1-8.Oct 5, 2004 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA060095SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XW65. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB. LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FASTENERS AT RIGHT WING TRAILINOct 4, 2004 · N825BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060094SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING INBOARD FLAP TRAILING EDGE HAS SEVERAL DENTS BETWEEN STATIONS XW64 AND XW101. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS. IAW DC8Oct 4, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060093SSkin · dentedDURING ROUTINE C-CHECK FOUND RT WING OB FLAP UPPER LEADING EDGE SKIN DENTED AT STATION XF 418. REMOVED DAMAGED. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING OB FLAP UPPER LEADING EDGE ATOct 4, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060092SSkin · dentedDURING ROUTINE C-CHECK, FOUND RIGHT WING INBOARD FLAP LOWER SURFACE HAS SEVERAL DENTS BETWEEN STATION XW15 AND XW45. REMOVED DAMAGED SKIN. FABRICATED REPAIR PARTS. PERFORMED HOT BOND TO DAMAGED AREA IAW DC8 SRM 57-1-0, 51-1-9, 51-1-5 AND 51-1-8.Oct 4, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060054SSupport Fitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING FLAP CANOE FITTING UPPER SUPPORT CRACKED AT STATION XRS 235. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW SUPPORT, LOCATED, DRILLED, TRIMMED, TEREATED, PRIMED, INSTALLED NEW SUPPORT AND FASTWENEROct 4, 2004 · N825BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA060018SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP LOWER SKIN DENTED BETWEEN STATION XF309 AND XF333. REMOVED FASTENERS AS NEEDED. REMOVED LOWER SKIN SECTION. FABRICATED NEW SKIN SECTION AND FILLERS. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTOct 4, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060017SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT WING OUT BOARD FLAP DENTED AT STATION XW384. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND NEW FASTENESR WET WITH SEALANT FOct 4, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0500216SLongeron · corrodedDURING ROUTINE C-CHECK FOUND LONGERON 28 RIGHT CORRODED AT STATION 330 TO 370. REMOVED DAMAGED LONGERON SECTION. FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW COOPESA EO COO-8-53-377-04.Oct 4, 2004 · N825BX · Doug DC871F · Fuselage Main, Longeron/StringerSDR IXXA0500214SCloseout Panel · corrodedDURING ROUTINE C-CHECK FOUND AFT WING FILLET PANEL NUMBER 161X SKIN DISBONDED AND CORRODED. FABRICATED NEW PANEL, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW FILLET PANEL IAW COOPESA EO COO-8-53-431-04.Oct 4, 2004 · N825BX · Doug DC871F · Wing, Plate/SkinSDR UPS04843280Web · crackedINSPECTION TYPE:C2 AC BAY SUBFLOOR WEB CRACKED BETWEEN STA 8 & STA 16 AT L21L. REPAIRED IAW DC-8 SRM 51-1-21A & UPS EO DC8 5350-7876-A.Oct 4, 2004 · N715UP · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060101SRib · crackedDURING ROUTINE C-CHECK FOUND FORWARD ENTRY DOOR CUT OUT, AFT RIB CRACKED BETWEEN LONGERON 19 LT AND 20 LT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB, LOCATED, DRILLED,TREATED, PRIMED, INSTALLED NEW RIB AND NEW FASTENERS. IAW SRM 53Oct 3, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA060096SRib · crackedDURING ROUTINE C-CHECK, FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS360. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS360. IAW SRM 57-2-0,Oct 3, 2004 · N825BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060072SWeb · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 857 AT -X16. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS AT STATION 857 FROM -X11 TO -X21 IAW DC8 SROct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060071SWeb · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 810 AT -X68. REMOVED DAMAGED. FABRICATED FILLER AND DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER AND FASTENERS AT STATION 810 BETWEEN -X50 AND -X70 IAW DOct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060070SWeb · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE WEB CRACKED AT STATION 857 AND +X16. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLERS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW DOUBLER, FILLERS AND FASTENERS AT STATION 857 FROM +X11 TO +XOct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060069SAngle · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 857 AND +X16. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW ANGLE AND FASTENERS AT STATION 857 FROOct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060068SSupport Angle · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SUPPORT ANGLE CRACKED AT STATION 640 BETWEEN +X70 AND -Z35. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED SUPPORT ANGLE. FABRICATED NEW SUPPROT ANGLE, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW SUPPORT ANGOct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060067SDoubler · wornDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE DOUBLER WORN AT STATION 980 BETWEEN +X65 TO -Z54. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED DOUBLER. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW EXTERNAL FUSELAGE DOUBLEROct 3, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060066SAngle · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 980 BETWEEN +X65 TO -Z54. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW EXTERNAL FUSELAGE ANGLE ANOct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060065SSupport Angle · corrodedDURING ROUTINE C CHECK, FOUND FLOOR SUPPORT ANGLE CORRODED IN THE FORWARD CARGO COMPARTMENT BETWEEN STATION 580 AND 637 AT LONGERON 33 RIGHT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FLOOR SUPPROT ANGLE. FABRICATED NEW ANGLE. LOCATED, DRILLED, TRIMMED,Oct 3, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous Structure
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