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Aircraft record

N801GP1969 Douglas DC-8-71F

DeregisteredUnclaimedSource: FAA, updated Oct 16, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 16, 2006.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched111 service difficulty reports

Registration
Deregistered
Last based in
Miami, FL
owner city / state
Owners
1
since 2003
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
111
since 1995

Registration

FAA Aircraft Registry · Oct 16, 2026
Last registered owner
Aeroturbine INC
Owner type
Corporation
City, state
Miami, FL
Certificate issued
Jun 19, 2003
Canceled
May 16, 2006
Airworthiness
Standard · Transport
Airworthiness date
Oct 5, 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
1969
Serial number
46039
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
AAE638

Engine

Make and model
Ge Cfm56 Series
Type
Turbo-jet
Power
9,800 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
  1. 2003 – 2006Aeroturbine INCMiami, FL

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 (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 (111)

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.

  • Fire protection · fire loop · failedApr 30, 2001

    ENGINE NR 1 ON TAKEOFF INTERMITTENT FIRE WARNING. AS PER QRH, ENG WAS SHUT DOWN AND FIRE LOOP TESTED. IT DID NOT RESET. DISCHARGED BOTTLE NR 1, WAITED 30 SEC, FIRE LOOP TESTED. IT DID NOT RESET, DISCHARGED BOTTLE NR 2, WAITED 30 SEC, LOOP DID NOT TEST. ALL OTHER INDICATIONS NORMAL. REMOVED AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · damagedMar 29, 2001

    APPROX 3 INCH TEAR IN FUSELAGE SKIN AT FWD LOWER CORNER BELOW CARGO DOOR DURING FWD DOOR GUARD INSTALLATION. REPAIRED DAMAGED AREA AT LOWER FORWARD CORNER OF MCD JAMB IAW GUIDELINES OF EWA ENGINEERING MEMO ML329011 THIS TEMPORARY REPAIR LIMITED TO 1000 CYCLES

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · outflow valve · failedMar 24, 2001

    ON DESCENT, CABIN BEGAN TO CLIMB. WENT TO MAX RATE ON AUTO CONTROLLER AND MAX FLOW ON PACKS, WOULD NOT STOP CLIMB, CABIN COULD NOT BE CONTROLLED MANUALLY EITHER. ANY ATTEMPT TO MANUALLY CONTROL PRESSURE CAUSED CABIN TO CLIMB HIGHER, MANUAL LEVER COULD NOT BE MOVED PAST 3/4 CLOSED. REMOVED AND…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Nacelles and pylons · plate · crackedFeb 21, 2001

    DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WING L/E SHIM PLATE AT I/B NR3 ENG. PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 02/19/01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · gougedFeb 15, 2001

    DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO LT. WING FLAP IN FITTING AT STA. 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 02/06/01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · clip · crackedFeb 15, 2001

    DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO ATTACH CLIP AT STA. 252 CAN'T AND R/H WING #4 MAIN INSIDE TANK THRU ACCESS HOLE 505D AND BETWEEN STRINGER 68 & 69, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · attach angle · crackedFeb 15, 2001

    DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. WING REAR SPAR FLAP ATTACH FITTING AT STA. XRS98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · drive link · gougedFeb 15, 2001

    DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO R/H O/B FLAP CENTER DRIVE LINK AT STA. 319, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED 02/15/01.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · attach angle · crackedFeb 15, 2001

    DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO AFT LWR CARGO COMPARTMENT BULKHEAD DIVIDERS ATTACH ANLGE AT STA Y+14, Z-7, X-24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · panel · delaminatedFeb 14, 2001

    DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING #3 SPOILER PANEL AT #3 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED ARE IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-61-1.

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

Showing the 10 most recent of 111 reports.

Sources

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

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