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Aircraft record

N803AX1968 Douglas DC-8-62

DeregisteredUnclaimedSource: FAA, updated Oct 16, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Apr 7, 2004.

Safety record in brief:1 NTSB accident (substantial damage, Mar 1996)No ADs since 1998 matched43 service difficulty reports

Registration
Deregistered
Last based in
Wilmington, OH
owner city / state
Owners
1
since 1986
NTSB events
1
substantial, 1996
ADs may apply
0
confirm with A&P
Service reports
43
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Last registered owner
Abx Air INC
Owner type
Corporation
City, state
Wilmington, OH
Certificate issued
Feb 3, 1986
Canceled
Apr 7, 2004
Airworthiness
Standard · Transport
Airworthiness date
Jun 2, 1986

We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.

Airframe & engine

FAA Registry + type data

Airframe

Manufacturer
Douglas
Model
DC-8-62
Year
1968
Serial number
45917
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
152
Engines
4
Max takeoff weight
20,000 and over lb
Type certificate data sheet
4A25
Mode S code
AAED18

Engine

Make and model
P & W Jt3d Series
Type
Turbo-jet
Power
17,700 lb thrust

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1986 – 2004Abx Air INCWilmington, OH

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 2026 · SDRs · Oct 16, 2026

NTSB events (1)

Accident · substantial damage

Mar 20, 1996 · Wilmington, OH

The pilot-in-command's inadequate visual lookout and the company/operator's inadequate crew/group coordination and communication during taxi and snow removal operations. Related factors were the snowy weather conditions affecting visibility and the snowplow on the taxiway.

Damage
Substantial
Injuries
None
Report
IAD96LA052

From NTSB records; matched by serial number.Read NTSB report (search CAROL for IAD96LA052)

ADs published since 1998 that may apply (0)

These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (43)

Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.

  • Doors · handle · brokenMay 12, 1999

    COCKPIT DOOR HANDLE BROKEN, WOULD NOT OPEN FROM AFT SIDE. REPLACED COCKPIT DOOR HANDLE IAW DC8 SRM 51-3-0.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · controls · fodJan 18, 1999

    DURING DESCENT, AIRCRAFT WOULD NOT TURN TO THE LEFT. PILOT REPORTED FEELING SOMETHING 'SNAP'. AFTERWARDS, AIRCRAFT WAS VERY SLUGGISH TURNING TO THE LEFT. TURNED OK TO RIGHT. CREW DECLARED EMERGENCY, LANDING WAS UNEVENTFUL. *S/D* VISUALLY INSPECTED LEFT AND RIGHT AILERON POWER PACK AREAS. FOUND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · door handle · out of adjustAug 26, 1998

    DURING PREFLIGHT, FOUND THAT THE COCKPIT DOOR WOULD NOT OPEN FROM CABIN SIDE. REPAIRED COCKPIT DOOR HANDLE AS REQUIRED, OPS CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · angle · crackedAug 21, 1998

    RIGHT WING LEADING EDGE INTERIOR, VERTICAL STIFFENER ANGLE IS CRACKED AT BOTTOM OUTBOARD END OF INBOARD SLOT BOX STATION XS 250.089. REPLACED ANGLE IAW DWG 9753293 AND DC8 SRM 51-1-20 AND 51-1-21.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · corrodedAug 12, 1998

    FRAME STATION 798 RIGHT BELOW CUSP AREA CORRODED OUT ON FORWARD AND AFT SIDE OF FITTING. REPAIRED IAW DWG 5641008 AND ABX REA D853-22904 MR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · doubler · crackedAug 12, 1998

    LONGERON 24R AT STATION 879 HAS A 3.6 INCH LONG CRACK RUNNING FORWARD AND AFT OF FITTING LOCATION. REPAIRED IAW DC8 SRM 53-2-2 AND 51-1-20D.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · corrosionAug 12, 1998

    RIGHT UPPER CUSP MEMBRANE FITTING HAS HEAVY CORROSION FS 340 TO 350. REPAIRED IAW DC8 SRM 51-1-20D.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · angle · crackedAug 12, 1998

    RIGHT WING LEADING EDGE AT STATION 778.500 UPPER LEADING EDGE RIB IS CRACKED AT THE AFT END. REPAIRED IAW DWG K 05056-7003.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedAug 12, 1998

    LONGERON END FITTING AT FRAME STATION 1520, LONGERON 28 LEFT AT MANUFACTURE SPLICE WAS CRACKED AND CORRODED. REPLACED FITTING IAW DC8 SRM 51-3-0 AND SRM 51-1-20.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedAug 11, 1998

    RIGHT WING LEADING EDGE AT STATION XFS 304.0 UPPER LEADING EDGE SKIN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED IAW DC8 SRM 57-2-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 43 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 16, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 16, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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