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
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.
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 reportsShow fewer 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.