Douglas DC-8-62F

Service difficulty reports · 1,163

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 = 'DC862F'
  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 IXXA060249SSeat Track · wornDURING ROUTINE C CHECK FOUND SEAT TRACK WORN OUT OF LIMITS BETWEEN STATION Y717 TO Y742 AT -X25. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060248SSeat Track · damagedDURING ROUTINE C CHECK FOUND A SEAT TRACK WITH AN ELONGATED HOLE AT STATION 827.5 X=0, Z=0. REPAIRED PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060220SFillet · delaminatedDURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262K DELAMINATED AND CORRODED. REPLACED PANEL PER COOPESA EO COO-8-53-304-04.Jun 9, 2004 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA060218SFillet · delaminatedDURING ROUTINE C CHECK FOUND WING FILLET PANEL NUMBER 262F DELAMINATED AND CORRODED AT AFT FACE. REPLACED PANEL PER COOPESA EO NUMBER COO-8-53-304-04 DATED 08/06/2004.Jun 9, 2004 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA060215SFloorbeam · corrodedDURING ROUTINE C CHECK FOUND FLOORBEAM UPPER FLANGE CORRODED AT STATION 420 BETWEEN -X29 AND -X42. REPAIRED FLOORBEAM PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage Main, Floor BeamSDR IXXA060214SSkin · crackedDURING ROUTINE C CHECK FOUND SKIN BULGED AND CRACKED FROM STATION 1460 TO STATION 1480 BETWEEN LONGERONS 31 RIGHT AND 33 RIGHT. REPAIRED PER COOPESA EO COO-8-53-244-04 DATED 6/8/04.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA060213SFloorbeam · crackedDURING ROUTINE C CHECK FOUND FLOOR BEAM CRACKED AT STATION 1420, Z0, -X45. REPAIRED PER COOPESA EO COO-8-53-243-04 DATED 7/7/04.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage Main, Floor BeamSDR IXXA060211SFrame · crackedDURING ROUTINE C CHECK FOUND FRAME FORMER CRACKED AT STATION 380 BETWEEN LONGERONS 31 RIGHT HAND AND 32 RIGHT HAND. REMOVED DAMAGE, MANUFACTURED, AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060210SFloorbeam · crackedDURING ROUTINE C CHECK FOUND FLOORBEAM UPPER FLANGE CRACKED AT STATION 380, +X32. REPAIRED PER COOPESA EO COO-8-53-245-04 DATED 6/10/04.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage Main, Floor BeamSDR IXXA060209SFloorbeam · crackedDURING ROUTINE C CHECK FOUND CRACKED FLOORBEAM AT STATION Y360 AT +X28 AND +X32. REPAIRED PER COOPESA EO COO-8-53-264-04 DATED 6/15/04.Jun 9, 2004 · N41CX · Doug DC862F · Fuselage Main, Floor BeamSDR IXXA060219SPanel · dentedDURING ROUTINE C-CHECK FOUND WING FILLET PANEL NUMBER 162C DENTED. REPLACED OUTER SKIN AND HONEYCOMB SECTION PER COOPESA EO COO-CMP-8-53-260-04 DATED 07/14/2004.Jun 9, 2004 · N41CX · Doug DC862F · Aerodynamic FairingsSDR IXXA060427SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE CAVITY LOWER RIB CORRODED AND CRACKED AT STATION XFS360.25. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Wing, Rib/BulkheadSDR IXXA060426SSkin · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE SKIN CORRODED AT STATION XW250. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA060320SSkin · corrodedDURING ROUTINE C CHECK FOUND RIGHT HAND HORIZONTAL STABILIZER LEADING EDGE CORRODED FROM STATION XFS60 TO XFS142. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA060319SSkin · dentedDURING ROUTINE C CHECK, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE DENTED AT STATION XFS239. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR IXXA060247SSeat Track · corrodedDURING ROUTINE C CHECK FOUND SEAT TRACK CORRODED FROM STATION 1270 TO STATION 1420 AT +X40, Z=0. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060246SFrame · misdrilledDURING ROUTINE C CHECK FOUND A FRAME WITH A DOUBLE DRILLED HOLE AT STATION 460 LONGERON 21 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060212SSupport · corrodedDURING ROUTINE C CHECK FOUND LEFT WHEEL WELL FORWARD BULKHEAD SUPPORT CORRODED AT STATION 857, +X56 AND -Z25. REPLACED SUPPORT PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, BulkheadSDR IXXA060208SSkin · scratchedDURING ROUTINE C CHECK FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AT STATION 557.5 BETWEEN LONGERONS 29 RIGHT HAND AND 30 RIGHT HAND. REPAIRED PER COTNEY DRAWING W08-R12 DATED 7-22-04Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA060207SSupport · corrodedDURING ROUTINE C CHECK FOUND CEILING SUPPORTS CORRODED IN SEVERAL PLACES FROM STATION 1380 -28 BETWEEN -X41 AND +X41. REMOVED CORROSION AND REPLACED SUPPORTS AS NEEDED PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060206SSeat Track · corrodedDURING ROUTINE C CHECK, FOUND SEAT TRACK CORRODED AT STATION 1150 Z0 X0. REPLACED SEAT TRACK FROM STATION 1120 TO 1197 Z0 X0 PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060205SSkin · bulgedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN BULGED AT STATION 522 AT LONGERON 34 RIGHT HAND. REPAIRED PER COTNEY DRAWING W08-R08 DATED 7/22/04.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA060204SSkin · scratchedDURING ROUTINE C CHECK, FOUND EXTERNAL FUSELAGE SKIN SCRATCHED AT STATION 268.5 AT LONGERON 24 LEFT HAND. REPAIRED PER COTNEY DRAWING WO8-R14 DATED 7-20-04.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA060203SSkin · bulgedDURING ROUTINE C CHECK, FOUND FUSELAGE SKIN EXISTING DOUBLER BULGED AT STATION Y1530 BETWEEN LONGERONS 29 LEFT AND 32 LEFT. REMOVED CORROSION, MANUFACTURED AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA060202SFrame · corrodedDURING ROUTINE C CHECK, FOUND FRAME CORRODED ON UPPER CHORD LOWER FACE AT STATION 1100 BETWEEN LONGERON 33 LEFT AND 33 RIGHT. REMOVED CORROSION, MANUFACTURED AND INSTALLED REPAIR PARTS PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060201SChannel · corrodedDURING ROUTINE C CHECK, FOUND FLOOR CHANNELS CORRODED AND CRACKED FROM STATION 990 TO STATION 1120 -X7, AND +X7. REPLACED FLOOR CHANNELS FROM STATION 990 TO STATION 1120 -X7 AND+X7, PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060200SCargo Track · corrodedDURING ROUTINE C CHECK, FOUND CARGO TRACK AND SUPORT CHANNEL CORRODED FROM STATION 990 TO STATION 1120 - X 17 AT LONGERON 33 RIGHT HAND. REMOVED CORROSION ON CARGO TRACK, WITH IN LIMITS. REPLACED CARGO TRACK SUPPORT CHANNEL PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060199SCargo Track · corrodedDURING ROUTINE C CHECK, FOUND TRACK CORRODED FROM STATION 990 TO STATION 1380 + X17 AT LONGERON 33 LEFT HAND. REPLACED CARGO TRACK SECTION FROM STATION 1140 TO STATION 1380 + X17 PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060198SCargo Track · corrodedDURING ROUTINE C CHECK FOUND TRACK CORRODED FROM STATION Y990 TO Y1020 AT TX45 TO Z 0. REPLACED DAMAGED TRACK PER ALL APPLICABLE DATA.Jun 8, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060425SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING LEADING EDGE RIB CRACKED AT STATION XFS773. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862F · Wing, Rib/BulkheadSDR IXXA060356SFitting · crackedDURING ROUTINE C CHECK FOUND LONGERON 20 LEFT END FITTING CRACKED AT STATION Y1530. REPAIRED PER ALL APPLICABLE DATAJun 7, 2004 · N41CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA060245SFloor Support · corrodedDURING ROUTINE C CHECK, FOUND FLOOR SUPPORTS CORRODED AT STATION 1580 BETWEEN X35 AND -X35, Z0. REPLACED FLOOR SUPPORTS PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060244SFloor Support · corrodedDURING ROUTINE C CHECK, FOUND FLOOR SUPPORTS CORRODED BETWEEN STATION 1540 AND STATION 1620 FROM X40 AND -X4, Z0. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060243SFloor Support · corrodedDURING ROUTINE C CHECK FOUND FLOOR SUPPORTS CORRODED AT STATION Y1540, X40 AND -X40 AT Z0. REPLACED FLOOR SUPPORTS PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060242SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION 1460 LONGERON 9 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060240SFrame · tool damageDURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1240 BETWEEN LONGERONS 10 LEFT AND 11 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jun 7, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060184SFitting · crackedDURING ROUTINE C CHECK, FOUND END FITTING CRACKED AT STATION Y1530 LONGERON 21 RIGHT. REMOVED DAMAGED END FITTING. LOCATED, DRILLED, TREATED, PRIMED, AND INSTALLED NEW END FITTING AT STATION Y1530 LONGERON 21 RIGHT IAW DC8 SRM 51-1-20D, AND 53-2-0.Jun 7, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060355SIntercostal · corrodedDURING ROUTINE C CHECK FOUND INTERCOSTAL CORRODED FROM STATION Y270 TO Y255 BETWEEN LONGERONS 6 LEFT AND 7 LEFT. REPAIRED PER ALL APPLICABLE DATAJun 6, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060354SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y789 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N5311 · Doug DC862F · Fuselage Main, FrameSDR IXXA060353SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y759 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060352SFrame · misdrilledDURING ROUTINE C CHECK FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y742 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060351SLongeron · corrodedDURING ROUTINE C CHECK FOUND LONGERON 8 RIGHT CORRODED BETWEEN STATIONS Y300 TO Y348. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA060350SDoubler · corrodedDURING ROUTINE C CHECK, FOUND DOUBLER ATTACH FRAME CORRODED AT STATION Y255. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060241SFrame · tool damageDURING ROUTINE C CHECK, FOUND A FRAME RADIUS WITH A HOLE AT STATION 1400 LONGERON 14 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060239SFrame · wornDURING ROUTINE C CHECK, FOUND FRAME WORN IN SEVERAL PLACED AT STATION 480 BETWEEN LONGERONS 20 LEFT AND 21 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060238SFrame · tool damageDURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1140 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060237SFrame · tool damageDURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1120 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060236SFrame · tool damageDURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 1080 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060235SFrame · tool damageDURING ROUTINE C CHECK, FOUND A DOUBLE DRILLED HOLE AT STATION 960 LONGERON 14 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060234SFrame · misdrilledDURING ROUTINE C CHECK FOUND A DOUBLE DRILLED HOLE AT STATION 920 LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jun 6, 2004 · N41CX · Doug DC862F · Fuselage Main, Frame
Back to Douglas DC-8-62F