Mcdonnell Douglas DC-8-63

Service difficulty reports · 1,601

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 = 'DC863'
  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 ABXA030240Door Frame · crackedMAIN CARGO DOOR, LATCH NR 4, ATTACHING HOLES HAD 5 CRACKED HOLES. REMOVED AND REPLACED FRAME SECTION IAW ABX REA D852-36710MR.Aug 29, 2002 · N828AX · Doug DC863 · Cargo/Baggage DoorsSDR ABXA030238Door Frame · gougedMAIN CABIN L1 DOOR, INSIDE AFT CENTER FRAME AT EDGE, HAD A DEEP GOUGE WEAR AT POINT WHERE BAYONET CONTACTS LATCH. REPAIRED AREA IAW REA D852-44006MR.Aug 26, 2002 · N828AX · Doug DC863 · Passenger/Crew DoorsSDR ABXA030236Skin · corrodedAFT LOWER CARGO, STA 1000, LONGERON 36 SKIN CORRODED. REPAIRED AREA IAW REA D853-44013MR, AND DC-8 SRM 51-1-8, 51-3-0, AND 51-1-20D.Aug 25, 2002 · N828AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA030235Structure · damagedL2 LOWER DOOR CORNER, REPAIRS DO NOT CONFORM TO CURRENT SRM, OR ABX JOB CARD NEA 53100104-002. REPAIRED AREA IAW REA D853-44010MR.Aug 24, 2002 · N828AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA020083Landing Gear · corrodedRIGHT MAIN LANDING GEAR WAS CORRODED IN THE FORWARD ATTACH LUG. REPLACED THE RIGHT MAIN LANDING GEAR.Aug 20, 2002 · N818AX · Doug DC863 · Main Landing GearSDR ABXA020099Skin · damagedL1 DOOR FORWARD LOWER AND AFT CORNER REPAIRS. REPAIRED AREA IAW ABX REA D853-43922-MR, DC-8 SRM 53-2-0, 51-1-20D, 51-1-21, AND 51-3-0.Jul 11, 2002 · N826AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA020100Beam · corrodedMAIN CABIN STATION 940, RIGHT BUTT LINE 68, CORROSION UNDER BEAM AND SHEAR WEB PANEL, LOWER SIDE CORNER. REPAIRED AREA IAW REA D853-43931-MR.Jul 8, 2002 · N826AX · Doug DC863 · Fuselage Structure (General)SDR ABXA020098Fitting · corrodedRIGHT WING STATION 219, FLAP LINK SUPPORT (CANOE) WAS CORRODED AND PITTED UNDER AFT TRACK PLATES. REMOVED CORROSION FROM FLAP LINK SUPPORT FITTING AND FABRICATED REPAIR FILLERS IAW DC-8 SERVICE BULLETIN 27-164. REMOVED CORROSION FROM LEFT AND RIGHT SIDE SUPPJul 8, 2002 · N826AX · Doug DC863 · Wing Miscellaneous StructureSDR ABXA020097Web · corrodedMAIN CABIN STATION 960, CORROSION UNDER BEAM AND SHEAR WEB BY LEFT BUTT LINE 68. REPAIRED AREA IAW ABX REA D853-43930-MR.Jul 8, 2002 · N826AX · Doug DC863 · Fuselage Structure (General)SDR ABXA020095Floorbeam · corrodedAFT CARGO AT STA. 1300, RBL 16, FLOORBEAM WAS CORRODED. FABRICATED NEW REPAIR PARTS AND FLOORBEAM IAW ABX REA D853-43926-MR, 51-1-8, 53-2-0, 51-1-20D, 51-3-0, AND 51-1-21.Jul 5, 2002 · N826AX · Doug DC863 · Fuselage Main, Floor BeamSDR ARWA20020703Brake Assy · fireNR 1 MAIN BRAKE FIRE EXTINGUISHED WITH CO2 SMALL FIRE 15 SECOND DURATION A/C BRAKES WERE SLIGHTLY USED ON LANDING ROLL. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW MM 32-42-1, ALSO REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY IAW MM 32-40-1. ACCOMPLISHED VISUAL INJul 5, 2002 · N345JW · Doug DC863 · BrakeSDR ABXA020105Fitting · crackedCABIN UNDER FLOOR FRAME STIFFENER WAS CRACKED AT FS 780, LEFT BUTT LINE 47.0. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D, 51-3-2 AND 51-3-0.Jul 2, 2002 · N826AX · Doug DC863 · Fuselage Structure (General)SDR IXXA0200045OControl Box · defectiveEN ROUNT FROM TOL TO LAX, THE LANDING GEAR DOOR NOT LATCHED LIGHT ILLUMINATED FOLLOWING LANDING GEAR RETRACTION. THE FLIGHT CREW CYCLED THE GEAR BUT THE WARNING INDICATION REMAINED THE SAME. THE FLIGHT FOLLOWED COMPANY PROCEDURES AND CONTINUED TO LAX FOR AN Jun 29, 2002 · N786AL · Doug DC863 · Landing Gear Position and WarningSDR ABXA020094Longeron · corrodedAIR COND/PRESS COMPARTMENT AT FS 36, LONGERON 31 RIGHT, AT OUTBOARD SIDE WAS CORRODED AROUND FASTENERS. FABRICATED REPAIR STRAP AND REPAIRED AREA IAW REA D853-43733-MR, SRM 53-2-0, 51-1-8, 51-1-20D.Jun 27, 2002 · N826AX · Doug DC863 · Fuselage Structure (General)SDR ABXA020103Fitting · cracked#4 ALT HAD A CRACKED STRINGER END FITTING AT XRS 408. SPLICE - STRINGER 59 AFT SIDE. INSTALLED NEW END FITTING AND BOOST PUMP BRACKET IAW DC-8 SRM 51-1-24, 51-1-8, AND 51-1-20D.Jun 21, 2002 · N826AX · Doug DC863 · Wing StructureSDR ABXA020107Frame · corrodedAFT CARGO FRAME HAD CORROSION AROUND NUTPLATE AT FS 1140, LONGERON 30 LEFT. CORROSION WAS OUT OF LIMITS. TRIMMED OUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 51-1-8, 53-2-0, 51-1-20D, AND REA D853-43923-MR.Jun 18, 2002 · N826AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020106Fitting · crackedAFT ACCESSORY COMPARTMENT LONGERON END FITTING CRACKED AT FS 1690, LONGERON 32 LEFT. FABRICATED LONGERON AND FRAME REPAIRS, INSTALLED REPAIRS IAW DC-8 SRM 53-2-0, 53-2-2, 51-1-8, 51-1-20D, 51-3-0, AND REA D853-43934-MR.Jun 18, 2002 · N826AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA020096Pressure Panel · corrodedMAIN CABIN, STATION 857 TO 880, BUTT LINE 0, CORROSION FOUND UNDER FINGER DOUBLER AND UNDER CABLE SUPPORT BRACKET. REPAIRED AREA IAW REA D853-43928-MR.Jun 18, 2002 · N826AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA020104Flap Track · corrodedRIGHT WING INBOARD FLAP, INBOARD FLAP TRACK SHOWED EVIDENCE OF WEAR AND CORROSION. REPLACED THE RIGHT WING INBOARD FLAP, INBOARD FLAP TRACKS IAW DC-8 MM 27-51-03.Jun 17, 2002 · N826AX · Doug DC863 · Nacelle/Pylon StructureSDR ABXA020102Frame · crackedRIGHT NOSE TUNNEL STATION 32, FRAME WAS CRACKED. FABRICATED NEW FRAME AND REPAIRED AREA IAW DC-8 SRM 51-1-20D, 53-3-1, 53-2-0, AND 51-1-8.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, FrameSDR ABXA020112Track · corrodedAFT CARGO COMPARTMENT STATION 1440 TO 1540, RIGHT BUTT LINE 60, CORROSION UNDER FLOOR BOARD CLIP NUTS. FABRICATED 8 EACH SPLICES AND REPAIR TRACK, INSTALLED AND REPAIRED AREA IAW DC-8 SRM 51-3-0, 53-2-0, 53-2-3, AND 51-1-8.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020111Floorbeam · corrodedFORWARD CARGO TEE CHORD AT FS 70 WAS CORRODED BETWEEN LONGERON 29 LEFT - LONGERON 31 LEFT. FABRICATED REPAIR DOUBLER AND REPAIRED AREA IAW DC-8 SRM 51-1-27 AND REA D853-43935-MR.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, Floor BeamSDR ABXA020093Doubler · corrodedRIGHT WHEEL WELL UPPER PRESSURE DECK REPAIR DOUBLER EXFOLIATED ABOVE LONGERON 24, FS 879. REPAIRED AREA IAW ABX REA D853-43932-MR.Jun 17, 2002 · N826AX · Doug DC863 · Fuselage Main, BulkheadSDR ABXA020110Spar Cap · crackedRIGHT WING FORWARD LOWER SPAR CAP HAD CRACK INDICATIONS IN FASTENER HOLES #2 AND #4 FROM THE INBOARD SIDE. FABRICATED REPAIR PARTS AND REPAIRED AREA IAW ABX DC-8 JOB CARD J060232, DC-8 SRM 51-1-8, 51-1-20D, AND 51-1-25.Jun 16, 2002 · N826AX · Doug DC863 · Wing, Attach FittingsSDR ABXA020109Fitting · corrodedAIR COND/PRESS COMPARTMENT BETWEEN FS 56-70, LONGERON 36, END FITTING WAS CORRODED. REPLACED END FITTING IAW DC-8 SRM 51-1-20D.Jun 16, 2002 · N826AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA020108Longeron · corrodedAIR COND/PRESS COMPARTMENT AT FS 24, LONGERON 31 RIGHT WAS CORRODED AT ATTACH ANGLE ATTACHING FASTENERS. REMOVED CORRODED CLIP LONGERON TO FRAME. INSTALLED NEW ATTACH P/N 2643619-1 IAW DC-8 SRM 51-1-21A AND 51-1-24.Jun 16, 2002 · N826AX · Doug DC863 · Fuselage Main, StructureSDR 2002F01099Wire · damagedRED ' GEAR NOT LATCHED' LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. REPAIRED WIRE BY REPINNING ON LEFT UPLATCH SWITCH CONNECTOR IAW DC-8 MM 20-50-1. ACCOMPLISHED NORMAL UPLATCH CHECK AND EMERGENCY EXTENSION. OPS CHECKS GOODJun 10, 2002 · N950R · Doug DC863 · Landing Gear System WiringSDR 2002F01097Warning Light · illuminatedRED 'GEAR NOT LATCHED' LIGHT ON FORWARD INSTRUMENT PANEL ILLUMINATED. ABNORMAL PROCEDURE COMPLETED. (M)Jun 7, 2002 · N950R · Doug DC863 · Landing Gear Position and WarningSDR IXXA0200026OFlex Line · rupturedENROUTE FROM PDX TO TOL, DURING CLIMB OUT THE FLIGHT CREW NOTICED THE MAIN HYDRAULIC QUANTITY SYSTEM DECLINING. THE FLIGHT CREW FOLLOWED COMPANY PROCEDURES AND RETURN TO PDX FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED AND LOCATED A RUPTURED HYDRAULIC LINEMay 22, 2002 · N786AL · Doug DC863 · Hydraulic System, MainSDR ABXA020067Longeron · crackedFORWARD CARGO STATION 520, LONGERON 35 RIGHT, INBOARD FLANGE WAS CRACKED. REPAIRED AREA IAW REA D853-43899-MR.May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020065Fitting · corrodedFORWARD CARGO, FS 300, BETWEEN LONGERON 33 RIGHT - LONERON 34 RIGHT, "Z" FITTING WAS CORRODED. REPLACED "Z" FITTING AND REPAIRED AREA IAW DC-8 SRM 51-3-2, 51-1-20D AND DAC DRAWING #3755824.May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Attach FittingsSDR ABXA020063Strap · corrodedFORWARD CARGO STATION 485, LONGERON 34 RIGHT, DOUBLER ON BACKSIDE OF LONGERON WAS CORRODED. REPLACED STRAP IAW DC-8 SRM 51-1-24 AND 51-1-20D.May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, StructureSDR ABXA020062Shear Tie · corrodedAFT CARGO AT STATION 1520, BETWEEN LONGERON 35 RIGHT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D.May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Attach FittingsSDR ABXA020061Shear Tie · corrodedAFT CARGO AT STATION 1520, BETWEEN LONGERON 35 LEFT AND LONGERON 36, SHEAR TIE WAS CORRODED. REPAIRED AREA, FABRICATED AND INSTALLED NEW CLIP IAW DC-8 SRM 51-1-21, 53-2-0, 51-9-0, 53-4-1, 51-1-8 AND 51-1-20D.May 20, 2002 · N820AX · Doug DC863 · Fuselage Main, Attach FittingsSDR ABXA020060Fitting · corrodedFORWARD CARGO AT STA. 70, STRING 25 LEFT, LONGERON END FITTING WAS CORRODED. REPLACED FITTING IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-3-0.May 20, 2002 · N820AX · Doug DC863 · Fuselage Structure (General)SDR ABXA020066Attach Angle · corrodedAFT LOWER CARGO STATION 986, FLOOR ATTACH ANGLE, BETWEEN LONGERON 33 RIGHT AND LONGERON 34 RIGHT, WAS CORRODED. REPAIRED AREA AND INSTALLED NEW FLOOR ATTACH ANGLE IAW DC-8 SRM 51-1-21, 51-1-20D AND REA D853-43896-MR.May 19, 2002 · N820AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA020064Skin · crackedRIGHT WING, INBOARD OF THE #4 PYLON, STATION XFS 515.00 - 526.76, HAD CRACK INDICATION AT HOLES 2 AND 4 GOING OUTBOARD. REPAIRED AREA AND INSTALLED NEW FILLER AND DOUBLER IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-3-0, 51-1-20D AND REA D857-43890-MR.May 17, 2002 · N820AX · Doug DC863 · Wing, Plate/SkinSDR ABXA010896Fitting · crackedEMPENNAGE INTERIOR LONGERON 17 LEFT, END FITTING WAS CRACKED AT F.S. 1769. REPLACED END FITTING IAW DC-8 SRM 51-1-21, 51-3-2 AND 51-1-20D.May 16, 2002 · N813AX · Doug DC863 · Fuselage Structure (General)SDR ABXA010895Spar · crackedLEFT WING AT STATION 515 - 526, HOLES 4 AND 5 FROM THE INBOARD SIDE, SHOWED CRACK INDICATION. REPAIRED AREA IAW REA D857-43866MR.May 13, 2002 · N813AX · Doug DC863 · Wing, Plate/SkinSDR ABXA010894Fitting · crackedEMPENNAGE INTERIOR LONGERON 17 RIGHT, WAS CRACKED AT F.S. 1769. REPAIRED AREA IAW DC-8 SRM 53-2-0, 51-1-8 AND 51-1-20D.May 13, 2002 · N813AX · Doug DC863 · Fuselage Structure (General)SDR ABXA010893Fitting · crackedEMPENNAGE INTERIOR LONGERON 17 RIGHT, END FITTING WAS CRACKED AT FS 1769. REPLACED END FITTING IAW DC-8 SRM 51-3-2 AND 51-1-20D.May 13, 2002 · N813AX · Doug DC863 · Fuselage Miscellaneous StructureSDR ABXA010891Skin · crackedL-1 DOOR, LOWER FORWARD CORNER, HAD A CRACK INDICATION AT EDGE OF MIDDLE LAYER SKIN. FABRICATED DOUBLER AND TRIPLER, AND REPAIRED AREA IAW DC-8 SRM 51-1-21, 53-20, 53-2-0, 51-1-8, AND DOUGLAS NDT SPM 06-10-01-001.May 13, 2002 · N813AX · Doug DC863 · Fuselage Main, Plate/SkinSDR ABXA010892Strap · brokenLOWER FRONT SPAR CAP, OUTBOARD OF #3 PYLON, #4 MAIN STRAP WAS BROKEN. REPLACED STRAP AND COMPLIED WITH REA #D857-43875.May 8, 2002 · N813AX · Doug DC863 · Wing, Attach FittingsSDR ABXA010829Seal · blownON CLIMBOUT, HYDRAULIC QUANTITY DROPPED TO STANDPIPE. EMERGENCY DECLARED. FOUND SLOT CONTROL VALVE MOUNT BOLT SEAL BLOWN. REPLACED SEAL. SLOT SYSTEM OPS AND LEAK CHECKED GOOD IAW DC-8 MM.Apr 22, 2002 · N817AX · Doug DC863 · Hydraulic System, MainSDR ABXA010818Downlock Switch · malfunctionedUPON LANDING, LANDING GEAR EXTENSION, THE NOSE LANDING GEAR GREEN LIGHT DID NOT ILLUMINATE. CHANGED BOTH BULBS, NO HELP. RECYCLED GEAR, NO HELP. RECYCLED GEAR A SECOND TIME AND GREEN LIGHT ILLUMINATED. INSPECTED NOSE LANDING GEAR, NO DEFECTS NOTED. REMOVEApr 10, 2002 · N823AX · Doug DC863 · Landing Gear Position and WarningSDR COOSDR02050Floorbeam · corrodedMAIN CARGO COMPONENT, STA 1680, Z0, +X7 INCHES AND X 15 INCHES, FLOOR BEAM UPPER CHORD CORRODED.Apr 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR COOSDR02051Frame · corrodedAFT CARGO COMPONENT STA 1600 BETWEEN LONG 34 LEFT AND 34 RIGHT FRAME, CORRODED.Apr 1, 2002 · N950R · Doug DC863 · Fuselage Main, FrameSDR COOSDR02012Floorbeam · crackedMAIN CARGO COMPARTMENT. Y STA 1580, Z0, +49.0 AND +X56.0, FLOORBEAM UPPER CHORD WITH CRACK.Mar 8, 2002 · N950R · Doug DC863 · Fuselage Main, Floor BeamSDR ABXA010802Longeron · crackedFORWARD CARGO, STATION 300 - 320, LONGERON 35 LEFT, ATTACH ANGLE CRACKED. REPAIRED AREA AND INSTALLED NEW SECTION OF LONGERON, NEW -Z- FITTINGS, SPLICES AND NEW WEB IAW DC-8 SRM 51-1-20D, 53-2-0, 51-1-8, 51-1-24 AND REA D853-43046MR.Mar 1, 2002 · N825AX · Doug DC863 · Fuselage Main, Longeron/StringerSDR COOSDR02044Floorbeam · crackedMAIN CARGO CABIN - STA Y=1600-FLOOR BEAM UPPER CHORD CRACKED.Mar 1, 2002 · N950R · Doug DC863 · Fuselage Main, Floor Beam
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