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Aircraft record

N807DHDouglas DC-8-73F

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 4, 2022.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched580 service difficulty reports

Registration
Deregistered
Last based in
Las Vegas, NV
owner city / state
Engine
NONE
None
Owners
1
since 2022
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
580
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Last registered owner
Skybus Cargo Jet INC
Owner type
Corporation
City, state
Las Vegas, NV
Certificate issued
Aug 31, 2022
Canceled
Oct 4, 2022
Airworthiness
Standard · Transport
Airworthiness date
Jul 17, 1968

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-8-73F
Serial number
45990
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
AAFC31

Engine

Make and model
None None
Type
Turbo-jet

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

Ownership history

Ownership history from FAA records
  1. 2022Skybus Cargo Jet INCLas Vegas, NV

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB 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 (580)

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.

  • Landing gear · actuator · leakingNov 15, 2011

    AFTER DEPARTURE, ACFT LOST HYDRAULIC LEVEL TO JUST ABOVE THE EMERGENCY LEVEL. ALL PROCEDURES COMPLIED AND ACFT RETURNED TO DEPARTURE. ACFT GROUNDED ON ARRIVAL. R & R RT MLG ACTUATOR AND REPLENISHED HYDRAULICS IAW MM 37-32-2, & 12-03-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · corrodedJun 23, 2011

    RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSIOIN S-63, STA XW 408.000 (NR4 ALT TANK) PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16, FIG 7. REMOVED CORRODED FITTING IAW SRM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · corrodedJun 23, 2011

    RT OUTER WING FWD BOTTOM PANEL.- FITTING HAS EXFOLIATION CORROSION S-62 (NR 4 ALT TANK) STA XW 408.000 PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1, DWG 3640143. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0, PG 16, FIG 7. REMOVED CORRODED FITTING IAW SRM…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · longeron · corrodedJun 7, 2011

    FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153, SHEET 4, TR 53-193. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. CUT OUT LONGERON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · corrodedJun 7, 2011

    FWD ACCY COMPT- L33R SHOWS EXFOLIATION CORROSION AT STA 14.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2, FIG 10 SHEET 1,3, TR 53-153 SHEET 4, TR 53-193. REMOVED FASTENERS IAW SRM 51-1-21. REMOVED LEVEL II CORROSION IAW SRM 51-1-8, PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0, PG 2M. CUT OUT LONGERON…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · stringer · crackedJun 7, 2011

    RT INNER WING AFT TOP PANEL.- STRINGER NR4 CRACKED STA XRS 87.000. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 07-21-11, EVA D857-00408 REV IR DATED 07-06-11. CUT OUT DAMAGED STRINGER SEGMENT , FABRICATED SPLICES & NEW STRINGER SEGMENT IAW DWG ED-5386 DATED 06-28-11. PERFORMED DETAILED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · corrodedJun 6, 2011

    FWD ACCY COMPT FITTING CORRODED BY EXFOLIATION STA 8.000 L33R. PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1 REMOVED CORROSION IAW SRM 51-1-8 PG 17-18 FOUND WITHIN LIMITS IAW SRM 53-2-0, PG 2P. REMOVED CORRODED FITING IAW SRM 51-1-20 D SRM 51-3-0. CLEANED TREATED & PRIMED AREA IAW SRM 51-1-8B…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · deformedJun 6, 2011

    MAIN CARGO BAY FRAME DEFORMED BS 1580.000 L19TO 21R. PERFORMED MAJOR REPAIR IAW SRM 53-2-0 FIG. 2 SHEET 6, SRM 53-4-1 FIG. 51 SHEET 21. REMOVED DEFORMED FRAME SEGMENT & EXISTING ANGLES IAW SRM 51-1-20D. FABRICATED NEW SEGMENT IAW SRM 53-4-1 FIG. 51 SHEET 21 ITEM "A", SRM`S 53-2-0 FIG 2, SHEET 2…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · tee fitting · crackedJun 3, 2011

    R2 SERVICE DOOR INNER FITTING CRACKED 1". REMOVED CRACKED TEE FITTING IAW SRM 51-1-20D, SRM 51-1-21. CLEANED, TREATED & PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TEE FITTING IAW SRM 51-1-20D, SRM 51-1-21, SRM 51-3-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · corrodedJun 2, 2011

    EXT FUS LWR SKIN CORRODED STA 1460.000 - 1480.000, L34L TO 35L. PERFORMED MAJOR REPAIR IAW SRM 53-1-0, PG 1, SRM 53-4-1, FIG. 17A SHEET 2. REMOVED LEVEL II CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2M. REMOVED CORRODED PLATING WITH EXISTING REPAIRS IAW SRM 51-1-21…

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

Showing the 10 most recent of 580 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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