Douglas DC-8-63F

Service difficulty reports · 1,883

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 = 'DC863F'
  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 ARWA9606066Skin · crackedPERMANENT REPAIR OF LOWER FUSELAGE AT LONGERON 36 FROM FS 600 TO 680 ACCOMPLISHED PER DRAWING ARW 015713-0013, FAA FORM 8110-APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9606065Door Cutout · damagedTEMPORARY REPAIR IN FORWARD LOWER CARGO COMPARTMENT DOOR CUTOUT, FORWARD CORNER, AT STA 280. REPAIRED FORWARD LOWER CORNER PER DC-8 SRM 53-2-0, FIG 22, CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606064Trapezoid Ftg · crackedRT MLG FITTING ASSEMBLY TO FUSELAGE, TRAPEZOID SHOWS 3 INCH CRACK AT 9, 10 AND 3 O'CLOCK. TRAPEZOID FITTING WAS REMOVED AND REPLACED IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-3-0 AND DOUGLAS TRAP FITTING REPLACEMENT GUIDE.Jun 14, 1996 · N441J · Doug DC863F · Fuselage, Landing Gear Attach FittingsSDR ARWA9606063Translating Ring · crackedNR 3 ENGINE TRANSLATING RING HAS 2 INCH CRACK IN RT FORWARD UPPER STRINGER. REPAIRED UPPER STRINGER IAW DC-8 SRM 78-3-3.Jun 14, 1996 · N441J · Doug DC863F · Engine Thrust ReverserSDR ARWA9606062Translating Ring · crackedNR 3 ENGINE TRANSLATING RING, AFT UPPER CORNER IS CRACKED. REPAIRED IAW ARROW AIR DRAWING NR ARW 015713-1182, FAA 8110-APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Engine Thrust ReverserSDR ARWA9606061Door Base · crackedLEFT AFT EMERGENCY DOOR BASE HAS LEVEL 1 CORROSION AND 4 INCH CRACK AT LONGERON 21L. REMOVED CORROSION AND REPAIRED AREA PER DC-8 SRM 53-2-0, FIG 1B, SHEET 3 AND 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Emergency ExitsSDR ARWA9606060Galley Door · crackedAFT GALLEY DOOR AT LONGERON 21R, FS 1220 TO 1240 HAS 2.5 INCH CRACK. REPAIRED CRACK PER DC-8 SRM 53-2-0, FIG 2.Jun 14, 1996 · N441J · Doug DC863F · Galley DoorsSDR ARWA9606059Floor Beam · corrodedSUPPORT ANGLE AT FLOOR BEAM HAS LEVEL 2 CORROSION AT FS 1723. REMOVED ANGLE, FABRICATED, TREATED AND INSTALLED ANGLE IAW DC-8 SRM 53-7-3, 51-1-4, 51-1-8 AND 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Floor BeamSDR ARWA9606058Longeron · corrodedRIGHT WING CENTER SECTION AT STA 960 THROUGH 980, LONGERON 22R, HAS CORROSION, CRACKS AND SHEARED RIVETS. REPAIRED AREA ACCORDING TO DACO ROD SKETCH NR 96-05-20-003.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Longeron/StringerSDR ARWA9606057Fillet · brokenMAIN CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT STA 940, RT UPPER PART, ALONG WITH BROKEN FILLET. REPAIRED AREA ACCORDING TO DACO ROD SKETCH NR 96-05-20-003.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606056Longeron · crackedLONGERON 24L HAS 3.5 INCH CRACK AT STA 960. LONGERON 24L WAS REPAIRED IAW DC-8 SRM 53-2-2, FIG 5. FABRICATED DOUBLERS PER DC-8 SRM 51-1-1. TREATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-8 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Longeron/StringerSDR ARWA9606055Cargo Door · crackedNR 3 LOWER CARGO DOOR HAS 1 INCH CRACK IN LEFT UPPER CORNER. REPAIRED NR 3 CARGO DOOR IAW DC-8 SRM 52-2-2 AND 52-4-1. FABRICATED AND TREATED DOUBLER IAW DC-8 SRM 51-1-4 AND 51-1-8. INSTALLED DC-8 IAW SRM 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Cargo/Baggage DoorsSDR ARWA9606054Skin · corrodedWING CENTER SECTION HAS LEVEL 2 CORROSION BETWEEN SKIN AND FILLER AT LONGERON 22L, FS 920 THROUGH 980. REPAIRED AREA ACCORDING TO DACO ROD SKETCH NR 96-05-20-003.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9606053Fitting · crackedMAIN CARGO COMPARTMENT HAS 3 INCH CRACK IN FITTING AT STA 780, LONGERON 22L. REPAIRED AREA PER ROD SKETCH NR 96-04-25-007, DOUGLAS-APPROVED ACTION NR 296570. FABRICATED AND TREATED DOUBLER PER DC-8 SRM 51-1-4, 51-1-8. INSTALLED DOUBLER PER DC-8 SRM 51-3-0, Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606052Former · crackedA 1 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 324.000. REPAIRED AREA IAW DRAWING ARW 015713-0310, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606051Former · crackedA 1 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 852. REPAIRED AREA IAW DRAWING ARW 015713-0302, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606050Former · crackedA .75 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 845.500. REPAIRED AREA IAW DRAWING ARW 015713-0303, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606049Former · crackedA 1 CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 733.000. REPAIRED AREA IAW DRAWING ARW 015713-0306, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606048Former · crackedA 1 INCH CRACK ON RIGHT WING LEADING EDGE FORMER AT STA XFS 723.000. REPAIRED AREA IAW DRAWING ARW 015713-0307, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606047Former · crackedA 1 INCH CRACK FOUND ON RIGHT WING LEADING EDGE FORMER AT STA XFS 766.250. REPAIRED AREA IAW DRAWING ARW 015713-0304, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606046Former · crackedA 1 INCH CRACK FOUND IN RIGHT WING LEADING EDGE FORMER AT STA XFS 347.750. REPAIRED AREA IAW DRAWING ARW 015713-0309, FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606045Former · crackedA .75 INCH CRACK ON RIGHT WING LEADING EDGE FORMER AT STA XFS 747.500. REPAIRED AREA IAW DRAWING ARW 015713-0305 FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Wing, Rib/BulkheadSDR ARWA9606044Skin · crackedEXTERIOR FUSELAGE HAS 1 CRACK AT LONGERON 33R STA 55, C3 DOOR. REPAIRED AREA PER DRAWING ARW 015713-0315, DER APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9606043Angle · crackedNR 3 ENGINE TRANSLATING RING UPPER ANGLE CRACKED. REPAIRED IAW DRAWING ARW 015713-1184 FAA FORM 8110 APPROVED.Jun 14, 1996 · N441J · Doug DC863F · Engine Thrust ReverserSDR ARWA9606042Fillet · brokenRIGHT WING UPPER SURFACE TRAILING EDGE HAS BROKEN FILLET AT STA XRS 289.000. FABRICATED FILLET IAW DC-8 SRM 57-3-3 AND 51-1-4. REMOVED AND REPLACED FILLET IAW DC-8 SRM 51-1-15.Jun 14, 1996 · N441J · Doug DC863F · Wing Miscellaneous StructureSDR ARWA9606041Skin · damagedTEMPORARY REPAIR ON RIGHT WING INBOARD FLAP AT STA XW 60.000. INSTALLED PERMANENT REPAIR PER DC-8 SRM 57-2-1, FIG 2Q. WING INBOARD FLAP PLATING CLEANED, TREATED AREA PER DC-8 SRM 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Trailing Edge FlapsSDR ARWA9606040Angle · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION ON ANGLE AT LONGERON 31R AT FS 200. REMOVED ANGLE AND FABRICATED NEW ANGLE IAW DC-8 SRM 53-4-1 AND 51-1-4. TREATED AND INSTALLED ANGLE PER DC-8 SRM 51-1-8 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606039Track · crackedRIGHT WING FLAP, NR 3 HINGE SLIDING COVER EXTERIOR TRACK IS BROKEN IN 2 PLACES. BROKEN TRACK REMOVED AND REPLACED IAW DC-8 MM 27-51-3.Jun 14, 1996 · N441J · Doug DC863F · Trailing Edge FlapsSDR ARWA9606038Plate · crackedRIGHT WING, LOWER SURFACE, PYLON LATERAL REINFORCEMENT PLATE CRACKED. REMOVED CRACKED PLATE, FABRICATED NEW DOUBLER PER DC-8 SRM 54-3-3 AND 51-1-4. TREATED AND INSTALLED PER DC-8 SRM 51-1-8, 51-1-17 AND 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Wing, Plate/SkinSDR ARWA9606037Skin · corrodedLEVEL 2 CORROSION FOUND AT EXTERIOR UPPER SKIN C-3, UPPER DOOR JAMB, AT FS 1160 TO 1220. REMOVED CORRODED SKIN. FABRICATED AND TREATED DOUBLERS IAW ARROW AIR SKETCH AND DC-8 SRM 51-1-4 AND 51-1-8. INSTALLED PER DC-8 SRM 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9606036Fitting · crackedAFT CARGO COMPARTMENT, LOWER VERTICAL STRUT CRACKED AT LONGERON 27R AT FS 1160. REMOVED AND REPLACED NEW FITTING PER DC-8 SRM 51-3-0.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606035Fitting · crackedAFT CARGO COMPARTMENT HAS BROKEN FITTING AT LONGERON 31R AT FS 1220. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-3-0.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606034Fitting · crackedCRACKED FITTING AT FS 1220 BETWEEN CEILING AND FLOOR BEAM. CRACKED FITTING REMOVED AND REPLACED IAW DC-8 SRM 51-1-20D AND 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606033Tail Cone · crackedTAIL CONE HAS CRACKS OF .5 AND 1.5 AT LONGERONS 7L AND 11L. REPAIRED CRACKS PER DC-8 SRM 53-2-0, FIG 1B, SHEET 3 AND 53-5-3, FIG 4, SHEETS 1 AND 2. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Aerodynamic FairingsSDR ARWA9606032Frame · corrodedAFT CARGO COMPARTMENT HAS LEVEL 2 CORROSION ON SIDEWALL UPPER AND LOWER FRAMES AT STA 1324. FRAMES WERE REPAIRED, TREATED AND INSTALLED PER DC-8 SRM 53-4-1, 51-1-4 , 51-1-8 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, FrameSDR ARWA9606031Fitting · crackedAFT CARGO COMPARTMENT HAS CORRODED AND BROKEN FITTING AT FS 1160, LONGERON 31R. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-3-0.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606030Frame · corrodedAFT CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FRAME UPPER CAP, FS 1000, LONGERONS 33R AND 34R. CORRODED CAP WAS REMOVED, FABRICATED, TREATED AND INSTALLED PER DC-8 SRM 53-4-1, 51-1-4, 51-1-8 AND 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, FrameSDR ARWA9606029Press Dome · crackedRT DOME CRACKED AT LOWER INNER RADIUS. REMOVED AND REPLACED DOME PER DRAWING NR 9750428.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, BulkheadSDR ARWA9606028Press Dome · corrodedLT DOME WITH EXFOLIATE CORROSION ON LOWER INNER RADIUS. REMOVED AND REPLACED DOME PER DRAWING NR 9750428.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, BulkheadSDR ARWA9606027Angle · corrodedLEVELS 1 AND 2 CORROSION AT INNER SURFACE STA 340 AND 280, LONGERONS 31L AND 26L. ATTACHMENT ANGLE WAS REMOVED AND REPLACED. FABRICATED ANGLE IAW DC-8 SRM 53-4-1 AND 51-1-4. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606026Longeron · corrodedFORWARD DECK, LONGERONS 35R AND 36 AT FS 500 HAVE LEVEL 2 CORROSION UNDER FRAME. REPAIRED AREA PER DC-8 SRM 51-1-21, 53-2-0, 51-1-8 AND 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Longeron/StringerSDR ARWA9606025Doubler · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FS 180, LONGERON 31R. REPLACED DOUBLER PER DC-8 SRM 51-1-21 AND 51-1-20D. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606024Fitting · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION BETWEEN FS 440 TO 460 AT LONGERON 31L. REMOVED AND REPLACED FITTING PER DC-8 SRM 51-1-20D AND 51-1-17.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606023Door Frame · corrodedFORWARD CARGO COMPARTMENT NR 2 DOOR FRAME AT STA 560 HAS LEVEL 2 CORROSION. FRAME WAS REMOVED AND NEW FRAME FABRICATED IAW DC-8 SRM 52-4-1 AND 51-1-4. TREATED AND INSTALLED PER DC-8 SRM 51-1-8, 51-1-17 AND 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606022Doubler · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT LONGERON 31R, FS 400 THROUGH 450. REPLACED EXTRUSION AND DOUBLER PER DC-8 SRM 53-2-1, FIG 7, SHEET 1 AND 53-4-1. CLEANED AND TREATED AREA PER DC-8 SRM 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606021Doubler · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT FS 215, LONGERON 31R DOUBLER. REMOVED AND REPLACED DOUBLER IAW DC-8 SRM 51-1-8 AND 53-2-0.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606020Skin · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION FROM FS 150 TO 190 AT LONGERON 31R. FORMED STRAP AND TREATED AND INSTALLED PER DC-8 SRM 53-4-1, 51-1-4, 51-1-8 AND 51-1-21.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Plate/SkinSDR ARWA9606019Door Housing · corrodedFORWARD CARGO COMPARTMENT HAS LEVEL 2 CORROSION AT UPPER SURFACE AT DOOR HOUSING, FS 280 PLUS 340. REPAIRED UPPER SURFACE IAW DC-8 SRM 53-2-0, FIG 1D. FABRICATED DOUBLER IAW DC-8 SRM 53-4-1, 51-1-1. TREATED AND INSTALLED IAW DC-8 SRM 51-1-8, 51-1-20D.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Miscellaneous StructureSDR ARWA9606018Frame · bentLT UPPER SURFACE CUSP EXTRUSION, FRAME AT LONGERON 21L, IS BENT. REPAIRED FRAME IAW DC-8 SRM 53-2-0, FIG 2. FORMED REPAIR PARTS IAW DC-8 SRM 53-4-1, 51-1-4 AND CLEANED AND TREATED AREA IAW DC-8 SRM 51-1-8.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, FrameSDR ARWA9606017Frame · brokenLT UPPER SURFACE CUSP EXTRUSION HAS BROKEN FRAME AT LONGERON 21L, FS 1560. REPAIRED FRAME IN ACCORDANCE WITH DC-8 SRM 57-2-0.Jun 14, 1996 · N441J · Doug DC863F · Fuselage Main, Frame
Back to Douglas DC-8-63F