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 COOSDR040035Panel · corrodedLT WING, FIXED PANEL NR 571, PN 5648891-1, WITH CORROSION AND DELAMINATED AT SEVERAL PLACES.Aug 16, 2004 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA060349SFitting · corrodedDURING ROUTINE C CHECK, FOUND FITTING CORRODED AT STATION Y1280 LONGERON 33 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Aug 8, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA0400102OEngine · failedDURING CRUISE FROM KSUU TO PHIK, NR 4 ENGINE LOSS OF ALL OIL QUANTITY AND OIL PRESSURE OF 12PSI. ENGINE NR 4 OIL LIGHT CAME ON. CREW SHUT DOWN NR 4 ENGINE AND AFTER SHUT DOWN NR 4 ENGINE WINDMILLING OIL PRESSURE AT 5PSI. AIRCRAFT ARRIVED IN PHIK AND LANDED Aug 7, 2004 · N71CX · Doug DC862F · Engine Oil QuantitySDR IXXA060348SLongeron · crackedDURING ROUTINE C CHECK, FOUND LONGERON 25 RIGHT CRACKED AT STATION Y390. REPAIRED PER ALL APPLICABLE DATA.Aug 3, 2004 · N41CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA060394SSkin · debondedDURING ROUTINE C CHECK, FOUND LEFT ELEVATOR UPPER SKIN TRAILING EDGE DEBONDED AND CORRODED FROM STATION XE260 TO XE280. REPAIRED PER ALL APPLICABLE DATA.Aug 2, 2004 · N41CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA060392SWeb · crackedDURING ROUTINE C CHECK, FOUND LEFT ELEVATOR WEB CRACKED AT STATION XE77. REPAIRED PER ALL APPLICABLE DATA.Jul 26, 2004 · N41CX · Doug DC862F · Elevator, Plate/SkinSDR IXXA060301SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y1060 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jul 25, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060300SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y640 AT LONGERON 7 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jul 25, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060299SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1340 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jul 25, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060298SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME SPLICE WITH A DOUBLE DRILLED HOLE AT STATION Y1500 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jul 25, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060294SLongeron · crackedDURING ROUTINE C CHECK, FOUND CRACKED LONGERON AT STATION Y1500 LONGERON 24 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jul 25, 2004 · N41CX · Doug DC862F · Fuselage Main, Longeron/StringerSDR IXXA060296SAngle · corrodedDURING ROUTINE C CHECK, FOUND A CORRODED ANGLE AT STATION 1500 LONGERON 23 LEFT STRUCTURE BOX. REPAIRED PER ALL APPLICABLE DATA.Jul 23, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060416SSkin · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE SKIN CORRODED BETWEEN STATIONS XRS710 TO XRS761. REPAIRED PER ALL APPLICABLE DATA.Jul 21, 2004 · N41CX · Doug DC862F · Wing, Plate/SkinSDR IXXA060415SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP TRAILING EDGE PANEL FITTING CRACKED AT STATION XW375. REPLACED FITTING PER ALL APPLICABLE DATA.Jul 21, 2004 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA060393SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT HORIZONTAL STABILIZER FITTING CRACKED AT STATION XFS47 BETWEEN STRINGERS 1 AND 2. REPLACED PER ALL APPLICABLE DATA.Jul 21, 2004 · N41CX · Doug DC862F · Horizontal Stabilizer, Attach FittingsSDR IXXA060295SFitting · corrodedDURING ROUTINE C CHECK, FOUND CORRODED FITTING FROM STATION Y960 TO Y980, -Z10, +X25. REPLACED FITTING PER ALL APPLICABLE DATA.Jul 21, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060347SIntercostal · corrodedDURING ROUTINE C CHECK, FOUND CORRODED INTERCOSTAL FROM STATION Y460 TO Y480, BETWEEN LONGERONS 34 LEFT AND 35 LEFT REPAIRED PER ALL APPLICABLE DATA.Jul 19, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060447SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING AUXILIARY TANK RIB CRACKED AT STATION XFS20. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Wing, Rib/BulkheadSDR IXXA060359SFitting · crackedDURING ROUTINE C CHECK FOUND FITTING CRACKED AT STATION 798, -Z1, -X25. REPLACED FITTING PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Fuselage Miscellaneous StructureSDR IXXA060297SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME WITH A DOUBLE DRILLED HOLE AT STATION Y1480 AT LONGERON 7 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060293SFitting · crackedDURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION Y798, -Z1, +X25. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060292SFitting · crackedDURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION 781, -Z1, -X25. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060291SFitting · crackedDURING ROUTINE C CHECK, FOUND CRACKED FITTING AT STATION 781, -Z1, +X25. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060290SFitting · crackedDURING ROUTINE C CHECK, FOUND A CRACKED FITTING AT STATION 759, +X25, -Z1. REPAIRED PER ALL APPLICABLE DATA.Jul 15, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060289SSeat Track · damagedDURING ROUTINE C CHECK, FOUND SEAT TRACK AND FLOOR PANEL WITH A HOLE AT STATION Y1500 +X45. REPAIRED PER ALL APPLICABLE DATA.Jul 13, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060414SSkin · dentedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD AILERON SKIN DENTED FROM STATION XA646 TO XA674. REPLACED PER ALL APPLICABLE DATA.Jul 10, 2004 · N41CX · Doug DC862F · AileronsSDR IXXA060288SSeat Track · corrodedDURING ROUTINE C CHECK, FOUND SEAT TRACK CORRODED FROM STATION Y420 TO Y560, -X25. REPAIRED PER ALL APPLICABLE DATA.Jul 10, 2004 · N41CX · Doug DC862F · Fuselage, Seat/Cargo Attach FittingsSDR IXXA060287SSupport · wornDURING ROUTINE C CHECK, FOUND LEFT AFT ENTRY DOOR UPPER HINGE SUPPORT WORN. REPAIRED PER ALL APPLICABLE DATA.Jul 10, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060286SFrame · tool damageDURING ROUTINE C CHECK, FOUND FRAME FLANGE WITH A DOUBLE DRILLED HOLE AT STATION Y1000 AT LONGERON 13 RIGHT. REPAIRED PER ALL APPLICABLE DATA.Jul 9, 2004 · N41CX · Doug DC862F · Fuselage Main, FrameSDR IXXA060391SSkin · debondedDURING ROUTINE C CHECK, FOUND RUDDER RIGHT SIDE SKIN DEBONDED AND A LOOSE RIVET FROM STATION ZR59 TO ZR87. REPLACED PER ALL APPLICABLE DATA.Jul 7, 2004 · N41CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA060446SFitting · corrodedDURING ROUTINE C CHECK, FOUND RIGHT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATAJul 5, 2004 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA060413SSkin · debondedDURING ROUTINE C CHECK, FOUND LEFT WING INBOARD FLAP SKIN DEBONDED AT STATION XW115. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA060412SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XF219. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA060411SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUTBOARD FLAP HINGE FITTING CORRODED AT STATION XT340. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862F · Trailing Edge FlapsSDR IXXA060410SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUT BOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATA.Jul 5, 2004 · N41CX · Doug DC862F · Wing, Attach FittingsSDR IXXA060390SSkin · bentDURING ROUTINE C CHECK, FOUND RIGHT SIDE RUDDER SKIN BENT FROM STATION ZR208 TO ZR239. REPLACED PER ALL APPLICABLE DATA.Jul 4, 2004 · N41CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA060388SSkin · debondedDURING ROUTINE C CHECK, FOUND RUDDER SKIN DEBONDED AND CORRODED FROM STATION ZR150 TO ZR115. REPLACED PER ALL APPLICABLE DATA.Jul 4, 2004 · N41CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA060409SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS384. REPAIRED PER ALL APPLICABLE DATA.Jul 3, 2004 · N41CX · Doug DC862F · Wing, Rib/BulkheadSDR IXXA060408SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING FLAP HINGE BASE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA.Jul 2, 2004 · N41CX · Doug DC862F · Wing, Attach FittingsSDR IXXA060389SSkin · debondedDURING ROUTINE C CHECK, FOUND RUDDER SKIN DEBONDED AND CORRODED FROM STATION ZR59 TO ZR115. REPLACED PER ALL APPLICABLE DATA.Jul 2, 2004 · N41CX · Doug DC862F · Rudder, Plate/SkinSDR IXXA060285SAttach Fitting · crackedDURING ROUTINE C CHECK, FOUND LONGERON FITTING CRACKED AT STATION 1530 LONGERON 34 LEFT. REPAIRED PER ALL APPLICABLE DATA.Jul 2, 2004 · N41CX · Doug DC862F · Fuselage Main, Attach FittingsSDR IXXA060284SDoubler · corrodedDURING ROUTINE C CHECK, FOUND DOUBLER CORRODED AT STATION 198, -X61, -Z10. REPAIRED PER ALL APPLICABLE DATAJul 2, 2004 · N41CX · Doug DC862F · Fuselage Main, Plate/SkinSDR IXXA060283SWindow Frame · corrodedDURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1240 TO 1260 RIGHT SIDE. REPAIRED PER ALL APPLICABLE DATA.Jul 1, 2004 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA060282SWindow Frame · corrodedDURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1240 TO 1260 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA.Jul 1, 2004 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA060281SWindow Frame · corrodedDURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1280 TO 1300 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA.Jul 1, 2004 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA060280SWindow Frame · corrodedDURING ROUTINE C CHECK, FOUND WINDOW CUT OUT CORRODED FROM STATION 1320 TO 1340 LEFT SIDE. REPAIRED PER ALL APPLICABLE DATA.Jul 1, 2004 · N41CX · Doug DC862F · Fuselage Main, StructureSDR IXXA060258SWindow Frame · corrodedDURING ROUTINE C CHECK FOUND WINDOW CUT OUT FRAME CORRODED FROM STATION Y1400 TO STATION Y1420 RIGHT HAND SIDE. REPAIRED PER ALL APPLICABLE DATA.Jul 1, 2004 · N41CX · Doug DC862F · Fuselage Main, StructureSDR COOSDR040009Panel · corrodedEMPENNAGE RT STAB LOWER SECTION STRINGER NR 4 WITH CRACK AT XFS 47 AND CORROSION AT XFS 45.Jun 30, 2004 · N41CX · Doug DC862F · Horizontal Stabilizer, Plate/SkinSDR COOSDR040007Panel · debondedVERTICAL STABILIZER TRAILING EDGE SECTION, UPPER AND LOWER PANELS WITH SKIN DEBONDING.Jun 30, 2004 · N41CX · Doug DC862F · Vertical Stabilizer, Plate/SkinSDR COOSDR040008Panel · crackedLT HORIZONTAL STABILIZER STA XFS 47 NR 1 UPPER STRINGER CRACKED.Jun 30, 2004 · N41CX · Doug DC862F · Horizontal Stabilizer, Plate/Skin
Back to Douglas DC-8-62F