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Aircraft record

N830BX1968 Douglas DC-8-71F

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Apr 14, 2014.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched177 service difficulty reports

Registration
Deregistered
Last based in
Moorpark, CA
owner city / state
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
177
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Individual owner
City, state
Moorpark, CA
Canceled
Apr 14, 2014
Airworthiness
Standard · Transport
Airworthiness date
Jun 26, 1994

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-8-71F
Year
1968
Serial number
45973
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
AB5889

Engine

Make and model
Cfm Intl. Cfm56 Series
Type
Turbo-jet
Power
2200 hp

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

Ownership history

Ownership history from FAA records
  1. until 2014Individual ownerMoorpark, CA

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (177)

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.

  • Stabilizers · skin · dentedJun 14, 2011

    DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR LOWER SKIN PANEL DENTED AT SEVERAL POINTS AT STA XE 246.000 - XH 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED RT ELEVATOR BALANCE. FOUND WITHIN…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · skin · corrodedJun 10, 2011

    DURING ROUTINE C-CHECK INSP FOUND RT MLG INBD DOOR INNER SKIN CORRODED. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMER AREA AND REPAIR PARTS. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 52-2-0, SRM 51-1-21, SRM 52-1-0 PAGE 1, SRM 52-6-1, FIG…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedJun 8, 2011

    DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 798.000, LONGERON 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING SRM 51-1-20D, SRM 51-1-0, SRM 51-1-8B, SRM 51-1-20D, SRM 51-3-0, SRM 51-3-1, REPAIR SPEC…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · fitting · crackedJun 8, 2011

    DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD BATHTUB FITTING CRACKED AT STA 680.000, LONGERON 9 RT. REMOVED CRACKED BATHTUB FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW BATHTUB FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedJun 8, 2011

    DURING ROUTINE C-CHECK INSP FOUND LT WING T/E PANEL CORRODED AT STATION XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0, SRM 51-3-0, SRM 51-1-8B, SRM 51-3-0 AND SRM 51-3-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · corrodedJun 8, 2011

    DURING ROUTINE C-CHECK INSP FOUND RT WING UPPER SKIN CORRODED AT STA XW 55.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS INSTALLED NEW SKIN IAW SRM 51-1-8, SRM 57-2-0, SRM 51-3-0, ED-5116, SRM 57-3-1 FIGURE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · web · wornJun 8, 2011

    DURING ROUTINE C-CHECK INSP, FOUND NR 3 ENGINE THRUST REVERSER LT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · web · wornJun 8, 2011

    DURING ROUTINE C-CHECK INSP FOUND NR 3 ENGINE THRUST REVERSER RT COWL FIXED STRUCTURE WEB FLANGE WORN AT STA YN 203.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED FRAME SEGMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · corrodedJun 8, 2011

    DURING ROUTINE C-CHECK INSP, FOUND RT HORIZ STABILIZER T/E UPPER SKIN CORRODED AT STA XE 29.000 - 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INNER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIRED…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · skin · crackedJun 8, 2011

    DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR UPPER SKIN DENTED AND CRACKED AT STATION XE 246.000 - 285.000. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED RT ELEVATOR BALANCE. FOUND WITHIN LIMITS…

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

Showing the 10 most recent of 177 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

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