Douglas DC-8-71F

Service difficulty reports · 8,938

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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 IXXA0500241SFrame · crackedDURING ROUTINE C-CHECK FOUND FRAME CRACKED AT STATION 420 LONGERON 35 RIGHT. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED AND INSTALLED REPAIR PARTS AND NEW FASTENERS AT STATION 420 BETWEEN LONGERONS 33 LEFT AND 35 LEFT Oct 20, 2004 · N825BX · Doug DC871F · Fuselage Main, FrameSDR IXXA0500209SRepair · temporaryDURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING EXTERNAL DOUBLER AT STATION 1702 LONGERON 26 LEFT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR DOUBLER AT STATION 1690 TO 1713 LONGERON 24 LEFT TOOct 18, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA060058SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 464.000. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT LEFT WING LEADING EDGE UPPER RIB AOct 17, 2004 · N825BX · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060056SStrap · crackedDURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 347.750. REMOVE DAMAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEFT WING CENTER LEADINOct 16, 2004 · N825BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA060057SStrap · crackedDURING ROUTINE C CHECK, FOUND LEFT WIND CENTER LEADING EDGE RIB SUPPORT STRAP CRACKED AT STATION XFS 366.500. REMOVE DAMAGED STRAP. FABRICATED NEW STRAP, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW STRAP AND FASTENERS AT LEFT WING CENTER LEADINOct 16, 2004 · N825BX · Doug DC871F · Wing Miscellaneous StructureSDR IXXA060041SRepair · damagedDURING ROUTINE C-CHECK REPLACED EXISTING FUSELAGE SKIN REPAIR FROM STATION 1735 TO STATION 1750 BETWEEN LONGERON 14 RT AND 17 RT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS AS NEEDED, AND EXISTING REPAIR. FABRICATED DOUBLER AND FILLERS, LOCATED, DRILLED, TRIMMOct 16, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060040SRepair · damagedDURING ROUTINE C-CHECK REPLACED EXISTING FUSELAGE SKIN REPAIR DUE TO DTA REQUIREMENTS AT STATION 1360 LONGERON 16 LT SIDE. REMOVED NECESSARY FASTENERS AND EXISTING REPAIR. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUOct 16, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR COOSDR040043Panel · corrodedVERTICAL STABILIZER, LT SIDE PANEL CORRODED AND DELAMINATED, LOCATED FROM STA ZR 253.000 TO STA ZV 299.125. (K)Oct 15, 2004 · N825BX · Doug DC871F · Vertical Stabilizer, Plate/SkinSDR COOSDR040044Skin · corrodedLOWER FUSELAGE SKIN WITH CORROSION AT Y-STA 680.0 AND Y-STA 687.0, BETWEEN LONG 31R AND LONG 34R. (K)Oct 15, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR COOSDR040045Fitting · crackedFWD CARGO COMPARTMENT FROM Y-STA 440 TO Y-STA 460, LONGERON 31R SPLICE FITTING, PN 3750257-1, CRACKED. (K)Oct 15, 2004 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR COOSDR040047Skin · crackedFWD PASSENGER DOOR HOLD OPEN PAN, PN 4643785, AND FUSELAGE EXTERNAL SKIN CRACKED AT Y-STA 15.000. (K)Oct 15, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR COOSDR040048Fitting · corrodedMAIN CARGO CABIN, SUPPORT FITTING, PN 4597643-1, CORRODED AT Y-STA 60-X65, Z 0 INCH. (K)Oct 15, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR COOSDR040049Fitting · crackedMAIN CARGO CABIN, FROM Y STA 650 TO Y-STA 680, LONGERON 1 FITTING WITH CRACK. (K)Oct 15, 2004 · N825BK · Doug DC871F · Fuselage Main, Attach FittingsSDR IXXA060055SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING TRAILING EDGE FLAP DRIVE LINK FITTING CRACKED AT STATION XW 97.906. REMOVED DRIVE LINK. REMOVED DAMAGED DRIVE LINK FITTING. RECEIVED NEW DRIVE LINK FITTING AND INSTALLED NEW FITTING AT STATION 97.906. INSTALLED DRIVEOct 12, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060015SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XFS 132.250. REMOVED FASTENERS AS NEEDED TO PERFORMED REPAIR. REMOVED DAMAGE. FABRICATED DOUBLER AND FILLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED DOUBLER, FILLER AND NEWOct 11, 2004 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA060013SSkin · crackedDURING ROUTINE C CHECK, FOUND RIGHT HAND WING SKIN CRACKED AT STATION 143.000. REMOVED FUEL DUCTS. REMOVED FASTENERS AS NEEDED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS AND FASTENERS WETOct 11, 2004 · N825BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0060010SRepair · scheduled maintDURING ROUTINE C CHECK REMOVE EXISTING EXTERNAL SKIN REPAIR AT STATION 172 LONGERON 35 RIGHT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS AS NEEDED AND EXISTING DOUBLER. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED, INSTALLED NEW REPOct 11, 2004 · N825BX · Doug DC871F · Aircraft StructuresSDR IXXA06007SDoubler · damagedDURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 550, LONGERON 35 RT. REMOVED NECESSARY FASTENERS AND EXISTING REPAIR. FABRICATED NEW REPAIR PARTS, LOCATED, DRILLED REMOVED, TREATED, PRIMED, INSTALLED NEW REPAIR PARTS, AND FASTENOct 11, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060006SDoubler · damagedDURING ROUTINE C-CHECK REMOVED EXISTING EXTERNAL FUSELAGE SKIN REPAIR AT STATION 543 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED NECESSARY FASTENERS AND EXISTING SKIN REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMOct 11, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060005SDoubler · damagedDURING ROUTINE C-CHECK REMOVED EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 543 LONGERON 35 RT DUE TP DTA REQUIREMENTS. REMOVED AFFECTED FASTENERS AND EXISTING SKIN REPAIR. FABRICATED REPAIR PARTS, LOCATED, DRILLED,REMOVED, TREATED, PRIMED, INSTALLED REPAIOct 11, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060004SDoubler · damagedDURING ROUTINE C-CHECK REPLACE EXISTING FUSELAGE SKIN REPAIR AT STATION 1144 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED AFFECTED FASTENERS AND EXISTING REPAIR. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED TREATED, PRIMED INSTALLED REOct 11, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA060003SDoubler · damagedDURING ROUTINE C CHECK REPLACE EXTERNAL FUSELAGE SKIN REPAIR AT STATION 1795 LONGERON 35 LT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR, AND EXISTING DOUBLER. FABRICATED REPAIR PARTS, LOCATED, DRILLED TREATED, PRIMED, INSTALLED REPAIR POct 11, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA060002SDoubler · damagedDURING ROUTINE C-CHECK, REPLACE EXISTING FUSELAGE SKIN REPAIR LOCATED AT STATION 1686 LONGERON 35 RT DUE TO DTA REQUIREMENTS. REMOVED FASTENERS NEEDED TO PERFORM REPAIR. REMOVED EXISTING DOUBLER. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATOct 11, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA0600001SDoubler · damagedDURING ROURINE C-CHECK REPLACE EXTERNAL FUSELAGE SKIN AT STATION 1695 LONGERON 36 REPAIR DUE TO DTA REQUIREMENTS. REMOVED EXISTING REPAIR. REMOVED DAMAGE, FABRICATED REPAIR PARTS, LOCATED, DRILLED, REMOVED, TREATED, PRIMED AND INSTALLED REPAIR PARTS AND INSTALOct 11, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500228SRepair · temporaryDURING ROUTINE C-CHECK TO COMPLY WITH DTA REQUIREMENTS REMOVED EXISTING DOUBLER AT STATION 1544 LONGERON 35 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTS AND FASTENERS AT STATION 1537 TO STATION 1551 BETWEENOct 11, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA0500210SSkin · corrodedDURING ROUTINE C-CHECK FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STATION 680, LONGERON 33 LEFT AND 34 LEFT. REMOVED DAMAGE, FABRICATED REPAIR PARTS. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AT STATION 674 TO STATION 696 BETWEEN LONGERON 3Oct 11, 2004 · N825BX · Doug DC871F · Fuselage Main, Plate/SkinSDR IXXA0500207SRepair · temporaryDURING ROUTINE C-CHECK, TO COMPLY WITH DTA REQUIREMENT REMOVED EXISTING DOUBLER AT STATION 74 LONGERON 35 RIGHT. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS AT STATION 70 TO 78.5, LONGERONS 34 LEFT TO LONGOct 11, 2004 · N825BX · Doug DC871F · Fuselage Structure (General)SDR IXXA060021SSkin · delaminatedDURING ROUTINE C-CHECK FOUND LT WING IB FLAP TRAILING EDGE PANEL UPPER SKIN DELAMINATED. REMOVED FASTENEERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN SECTION. FABRICATED FINGER DOUBLERS AND NEW UPPER SKIN SECTION. LOCATED, DRILLED, TRIMMED, TREATED, PROct 10, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060020SSkin · crackedDURING ROUTINE C CHECK FOUND LEFT HAND WING UPPER SKIN CRACKED AT STATION XRS 22.7 AT CENTER SPAR. REMOVED ALL FASTENERS COMMON TO REPAIR AREA. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED NEW REPAIR PARTOct 10, 2004 · N825BX · Doug DC871F · Wing, Plate/SkinSDR UPS04843455Rib · crackedINSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 753.750. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-21 & 51-20D.Oct 10, 2004 · N755UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843454Rib · crackedINSPECTION TYPE:C3, RIGHT WING CENTER L/E INTERNAL DOUBLER AND L/E SKIN IS CRACKED AT DRAIN HOLE XFS 335.250. REMOVED INTERNAL DOUBLER AND STOP DRILLED 2 CRACKS IAW DC-8 SRM 51-1-21 & 57-2-0 FIG 6. REMOVED, FABRICATED AND INSTALLED EXTERNAL IAW 51-1-20D, 51-Oct 10, 2004 · N755UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843453Rib · crackedINSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB IS CHAFED THROUGHT AT XS 515-720. BLENDED CHAFED AREA IAW DC-8 SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2, 57-3-1 & 51-1-20D.Oct 10, 2004 · N755UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843452Rib · crackedINSPECTION TYPE: C3, RIGHT WING O/B L/E RIB IS CRACKED WITH CORROSION AT XFS 772.500. REMOVED FASTENERS AND CORROSION IAW DD-8 SRM 51-1-21 & 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG 19 & 57-2-0 FIG 2.Oct 10, 2004 · N755UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04843450Intercostal · crackedINSPECTION TYPE: C3, RT WING CENTER L/E INTERCOSTAL IS CRACKED AT XFS 387.750. STOP DRILLED CRACK AT STA XFS 387.750 IAW SRM 57-02-00-0 FIG 002. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 57-02-00-0 FIG 2 & DC-8 SRM 51-1-20D.Oct 10, 2004 · N755UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS04843448Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE TWO LOWER RIBS CRACKED AT XFS 622.500 AND XSF 616.250. INSTALLED REPAIR DOUBLERS ON TWO RIBS AT XFS 622.500 AND XSF 616.250 IAW SRM 57-3-2 FIG 6 SHEET 2.Oct 10, 2004 · N755UP · Doug DC871F · Wing, Rib/BulkheadSDR IXXA060081SAngle · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 810 AT +X18. REMOVED DAMAGE. FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR ANGLE AND FASTENERS AT STATION 810 BETWEEN +X17.5 AND +X31 IAW DC8 SRMOct 9, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060080SAngle · crackedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE ANGLE CRACKED AT STATION 810 AT +X2. REMOVED DAMAGE. FABRICATED REPAIR ANGLE, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR ANGLE AND FASTENERS AT STATION 810 BETWEEN +X2 AND +X12. IAW DC8 SRM 53Oct 9, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060079SAttach Fitting · crackedDURING ROUTINE C CHECK, FOUND AFT FUSELAGE LONGERON ATTACH FITTING CRACKED AT STATION 1690 LONGERON 28 LEFT. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED FITTING. FABRICATED NEW FITTING, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED NEW LONGERON ATTACH FITTIOct 9, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060048SSupport Beam · crackedDURING ROUTINE C CHECK, FOUND EMERGENCY EXIT DOOR BEAM INBOARD CHORD CRACKED AT CENTER SECTION FROM STATION 1110.000 TO STATION 1140.000 AT STOP FITTING 7. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED CHORD. FAB`D NEW CHORD, LOCATED, DRILLED, TRIMMED, TREATOct 9, 2004 · N825BX · Doug DC871F · Fuselage Miscellaneous StructureSDR IXXA060028SSkin · dentedDURING ROUTINE C CHECK FOUND VERTICAL STABILIZER LEADING EDGE DENTED OUT OF LIMITS AT STATION ZFS149. REMOVED DAMAGE. FABRICATED FILLER AND DOUBLER. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED FILLER, DOUBLER, AND FASTENERS WET WITH SEALANT FROM STATOct 9, 2004 · N825BX · Doug DC871F · Vertical Stabilizer, Plate/SkinSDR IXXA0500211SAttach Fitting · crackedDURING ROUTINE C-CHECK FOUND LONGERON ATTACH FITTING CRACKED AT STATION 1690 LONGERON 23 RIGHT. REMOVED DAMAGED FITTING, FABRICATED NEW FITTING. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW LONGERON ATTACH FITTING IAW DC8 MM 20-16-0, DC8 SRM 51-3-1, 5Oct 9, 2004 · N825BX · Doug DC871F · Fuselage Main, Attach FittingsSDR UPS04843457Frame · crackedINSPECTION TYPE: C3, LT WING LEADING EDGE OUTER SECTION STA XFS-759 UPPER FORMER HAS A CRACK AT AFT FASTENER. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG19, 51-1-20D &51-1-21.Oct 9, 2004 · N755UP · Doug DC871F · Wing SparSDR UPS04843451Channel · crackedINSPECTION TYPE: C3, LT WING LEADING CENTER SECTION LOWER SUPPORT U-CHANNEL HAS A CRACK AT AFT 2 FASTENERS 2 INCHES LONG STA XFS 510. STOPPED DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DWG 5770375 AND DC-8 SRM 51-1-21 & 51-1Oct 9, 2004 · N755UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS04843333Lamp · inoperativeINSPECTION TYPE:N/A 3 EA LIGHTS FOR EMERGENCY LIGHTING AT ENTRY DOOR INOP. RELAMPED LIGHTS. OPS CHECKS GOOD.Oct 9, 2004 · N706UP · Doug DC871F · Emergency LightingSDR IXXA060049SBeam · crackedDURING ROUTINE C CHECK, FOUND AFT SERVICE DOOR BEAM NUMBER 1 CRACKED AT AFT SECTION. REMOVED SERVICE DOOR. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED BEAM. FAB`D NEW BEAM. LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW BEAM NUMBER 1 AND FASTEOct 8, 2004 · N825BX · Doug DC871F · Service DoorsSDR IXXA0500212SDoubler · corrodedDURING ROUTINE C-CHECK FOUND CENTER FUEL TANK LOWER DOUBLER SKIN BETWEEN FRONT SPAR STATION 683.055 AND STRINGER 65 CORRODED. REMOVED CORROSION, FABRICATED REPAIR PARTS, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PARTS, AND FASTENERS. IAW COOPESA EO Oct 8, 2004 · N825BX · Doug DC871F · Fuselage Main, StructureSDR IXXA0400112OEngine · failedON CLIMB-OUT AT 30,000 CLIMB POWER SETTING, NR 4 ENGINE FUEL FLOW STATED FLUX AND ENGINE LOST POWER. ROLLED BACK TO FLIGHT IDLE AND WOULD NOT RESPOND TO THROTTLE MOVEMENT. OTHER ENGINE INDICATIONS WERE NORMAL ENGINE WAS SHUT DOWN AND AIRCRAFT LANDED WITHOUT Oct 8, 2004 · N823BX · Doug DC871F · Fuel Flow IndicatingSDR IXXA060086SDoubler · 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 IXXA060089SSkin · puncturedDURING ROUTINE C CHECK FOUND RIGHT HAND WING INBOARD FLAP OUTBOARD VANE UPPER SIDE SKIN PUNCTURED. REMOVED VANE. REMOVED DAMAGED. MANUFACTURED REPAIR PARTS, PERFORMED HOT BOND. INSTALLED VANE. IAW DC8 MM 27-51-14, DC8 SRM 51-1-9A.Oct 7, 2004 · N825BX · Doug DC871F · Trailing Edge FlapsSDR IXXA060088SSkin · delaminatedDURING ROUTINE C-CHECK FOUND RT WING IB FLAP OB VANE UPPER SKIN DELAMINATED. REMOVED FLAP VANE. REMOVED DELAMINATED SKIN, PERFORMED HOT BOND TO DAMAGED AREA. INSTALLED VANE. IAW MM 27-51-14, SRM 51-1-9A.Oct 7, 2004 · N825BX · Doug DC871F · Trailing Edge Flaps
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