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Aircraft record

N821BX1966 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 May 1, 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
May 1, 2014
Airworthiness
Standard · Transport
Airworthiness date
May 28, 1991

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
1966
Serial number
45811
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
AB34C1

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.

  • Fuel · wire harness · damagedAug 9, 2011

    DURING CLIMBOUT, NR 3 MAIN TANK BOOST PUMP C/B`S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MAIN TANK FUEL BOOST PUMP WIRING HARNESS IAW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · wire harness · damagedAug 9, 2011

    DURING CLIMB OUT, NR 3 MAIN TANK BOOST PUMP C/B'S POPPED. THE CREW PERFORMED COM PROCEDURES, BUT NO HELP. THE CREW RETURNED TO DEPARTUE WITHOUT FURTHER INCIDENT. MX TROUBLESHOT AND FOUND NR 2 PIN RECESSED AT BOOST PUMP CONNECTOR PLUG. THEY REPLACED NR 3 MAIN TANK FUEL BOOST PUMP WIRING HARNESS IAW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · skin · dentedMar 4, 2011

    DURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP LOWER SKIN SCRATCH AND DENTS XF AT STA 174.000 TO XF 219.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 57-7-1, FIG 4, TR 57-94, SRM 51-1-21, 57-1-0 PAGE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Wings · spar cap · crackedFeb 11, 2011

    DURING ROUTINE C-CHECK INSP FOUND RT WING FRONT SPAR L/E LOWER CAP CRACKED AT STA XFS 500.233. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP, NO DISCREPANCY FOUND. FABRICATED SPLICE ANGLES, EXTERNAL DOUBLER, STRAP. CLEANED, TREATED, PRIMED AREA AND REPAIRED PARTS. INSTALLED NEW…

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

    DURING ROUTINE C-CHECK INSP, FOUND RT MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 680.000 LONGERON 6, RT. REMOVED CRACKED FITTING. CLEANED AND APPLIED PRIMER TO AREA. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, AND SRM 51-3-1.

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

    DURING ROUTINE C-CHECK INSP, FOUND AFT CARGO COMPARTMENT FITTING CRACKED AT STA 1160.000. R & R AFT CARGO COMPARTMENT FITTING IAW SRM 51-1-20D.

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

    DURING ROUTINE C-CHECK INSPECTION, FOUND SKIN CRACKED AT STA 55.000, 70.000 LONGERON 33 RT AND LONGERON 34 RT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR DOUBLER, FILLER AND FINGER DOUBLERS. CLEANED, TREATED, PRIMED…

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

    DURING ROUTINE C-CHECK INSP, FOUND FWD LOWER CARGO FWD DOOR AND JAMB INTERIOR CORRODED AT STA 335.000, LONGERON 36 TO LONGERON 35 RT. REMOVED DAMAGED ANGLE. FABRICATED REPAIR ANGLE, FILLER AND REPAIR STRAP. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 51-2-1, FIG…

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

    DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD FLAP RIB CRACKED AT STA XF 129.000. REMOVED DAMAGED RIB. FABRICATED NEW RIB. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIME AREA AND REPAIR PARTS. INSTALLED NEW RIB IAW SRM CHAP 57-7-1 FIGURE 2, SHEET 4, SRM 51-1-21, SRM 57-1-0 FIG 1, SRM 57-7-1…

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

    DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 702.000 LONGERON 19 RT. REMOVED CRACKED FITTING.INSTALLED NEW FITTING IAW SRM 51-1-21D AND SRM 51-3-1.

    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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