N848AX1969 Douglas DC-8-61
This N-number isn't registered right now. Below is its last known registration, canceled Feb 13, 2007.
Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched50 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 20, 2026- Last registered owner
- Abx Air INC
- Owner type
- Corporation
- City, state
- Wilmington, OH
- Certificate issued
- Oct 7, 1991
- Canceled
- Feb 13, 2007
- Airworthiness
- Standard · Transport
- Airworthiness date
- Jul 13, 1993
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 dataAirframe
- Manufacturer
- Douglas
- Model
- DC-8-61
- Year
- 1969
- Serial number
- 46032
- 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
- AB9DA7
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- 1991 – 2007Abx Air INCWilmington, OH
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
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 (50)
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.
- Flight controls · linkage · lack of lubeApr 1, 2004
COULD NOT MOVE AILERON TRIM WHEEL DURING DESCENT INTO ILN. LUBED AND INSPECTED LT, RT AND WHEEL WELL AILERON LINKAGES. OPERATED AILERON TRIM THROUGH NUMBEROUS TIMES. OPERATED NORMAL.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · corrodedDec 8, 2003
FORWARD CARGO STA 300 TO 320, LONGERON 32 LEFT, ATTACH ANGLE HAD CORROSION. REMOVED CORROSION AND REPAIRED LONGERON IAW REA D853-48497MR AND DC-8 SRM 53-2-0.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · corrodedDec 3, 2003
AFT CARGO AT STA 1180, LONGERON 26 LEFT, LONGERON HAD CORROSION. REMOVED CORROSION, CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPAIR ANGLES AND WEB SPLICE, ALODINED, AND PRIMED IAW DC-8 SRM 51-1-8, 53-2-0, 53-2-2, 51-1-21, 51-1-20D, AND REA D853-48485MR.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Wings · skin · corrodedDec 3, 2003
LEFT WING UPPER XRS 519 - 624 CORROSION AROUND FASTENER HEADS (24 EACH). REPAIRED AREA IAW REA D857-48493MR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · skin · crackedDec 3, 2003
L1 FORWARD PAX DOOR, LOWER AFT CORNER HAD A CRACK IN EXTERNAL SKIN. REMOVED DAMAGED AREA, REPAIRED SKIN / DOUBLER TRIM OUT IAW SRM 53-2-0 AND REA D853-48470MR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · crackedDec 1, 2003
CRACK IN OUTER SKIN AT LOWER FORWARD CORNER OF AFT PASSENGER DOOR. REMOVED CRACKED OUTER SKIN, FABRICATED AND INSTALLED DOUBLERS AND FILLERS IAW DC-8 SRM 53-2-0, 51-1-8, 51-1-21, 51-1-20D AND REA D853-48472MR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · skin · crackedNov 29, 2003
R1 FORWARD SERVICE DOOR, LOWER AFT CORNER HAD A CRACK ON EXTERNAL SKIN. REPAIRED AREA BY FABRICATING REPAIR DOUBLER, FILLERS AND TRIPLERS, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-8, 53-2-0 AND REA D853-48471MR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · longeron · corrodedNov 28, 2003
AFT CARGO AT STA 1200 - 122 AND LONGERON 28 LEFT HAD CORROSION. REMOVED CORROSION, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 51-1-8, 51-1-20D AND REA D853-48483MR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · frame · corrodedNov 27, 2003
A/C ACCESS COMPARTMENT AT FS 56, BETWEEN LONGERON 35 LT AND 35 RT, FRAME LOWER FLANGE WAS CORRODED. REMOVED CORROSION, FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND REA D853-48484MR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · skin · misrepairedNov 26, 2003
L2 DOOR LOWER AFT CORNER HAD A REPAIR THAT DID NOT RESEMBLE SERVICE ENGINEERING SKETCH ES00863. REMOVED DISCREPANT REPAIR, FABRICATED REPAIR DOUBLERS AND FILLER, ALODINED, PRIMED, AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21, 53-2-0 AND REA D853-48474MR.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 50 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026