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Aircraft record

N722CX1968 Douglas DC-8-72

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 18, 2013.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched96 service difficulty reports

Registration
Deregistered
Last based in
Orlando, FL
owner city / state
Owners
1
since 2010
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
96
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Cargo Aircraft Management INC
Owner type
Corporation
City, state
Orlando, FL
Certificate issued
Jan 13, 2010
Canceled
Oct 18, 2013
Airworthiness
Standard · Transport
Airworthiness date
May 2, 2005

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-8-72
Year
1968
Serial number
46130
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
A9AB42

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. 2010 – 2013Cargo Aircraft Management INCOrlando, FL

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 (96)

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 · vent · crackedMar 24, 2006

    DURING ROUTINE C-CHECK INSPECTION, REMOVED THE FWD BUFFET VENT TRIMMER VALVE AND PLUG OUTLET ON FUSELAGE. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-2-1 FIG 7. REMOVED FWD BUFFET VENT TRIMMER VALVE IAW DC-8 MM 38-20-11 PAGES 201-202. REMOVED EXISTING INTERNAL DOUBLER AND REMOVED AREA IAW DC8 SRM 53-2-1…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Structures (general) · none · noneFeb 24, 2006

    DURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-198 R9 INSTALL COMAT BOX. PERFORMED MAJOR ALTERATION IAW FAA FORM 8110-3 DATE 09-23-05, ATI DWG A95166-4 REV N DATE 09-23-05. INSTALLED COMAT BOX IAW ATI DWG 95166-4. COMPLIED WITH EO 25-DC8-198.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · panel · displacedFeb 24, 2006

    DURING ROUTINE C-CHECK INSPECTION, EO 25-DC8-520 R4 PARTITION UPPER ATTACHMENT RELOCATION TO FS-STC00171 LA-D. PERFORMED ALTERATION MAJOR IAW FAA FORM 8110-3 DATE 10-04-05. EO 25-DC-8-520 REV STATES 4 DATES 11-11-2005, ATI DWG C40-MO2 REV C DATE 10-04-05. FABRICATED DOUBLERS, STRAPS IAW ATI DWG…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Structures (general) · none · noneFeb 24, 2006

    DURING ROUTINE C-CHECK INSPECTION, ELT ANTENNA REMOVAL AND BLANKING PLATE INSTALLATION. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 02-06-06, ENGINEERING AUTHORIZATION AA71-2 REV IR DATE 01-24-06. REMOVED ELT ANTENNA IAW DC-8 MM 25-60-0 PAGE 201. FABRICATED BLANKING PLATE (AL 7075 T6 0.125)…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Structures (general) · none · noneFeb 16, 2006

    DURING C CHECK, INSTALLATION OF DOUBLER ON FS 188.000 L-1 TO L-2R REQUIRED DUE TO SEXTANT EQUIPMENT REMOVAL. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 06029 DATED 01-23-06, SEMAN DWG ED-4167 DATE 01-21-06, EO SEMAN # 2006100 DATE 01-23-06. REMOVED EXISTING SPACER, REMOVED DAMAGED AREA IAW…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · repair · misinstalledFeb 16, 2006

    DURING ROUTINE C-CHECK INSPECTION, RT INBD AILERON SHOWS SEVERAL SPOTS OF CORROSION AND NON STANDARD REPAIR ON LWR PLATING, STA XA 550.000. PERFORMED MAJOR REPAIR. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED EXISTING PANEL PLATING (CORRODED) + REPAIR NON STANDARD. FABRICATED NEW PANEL PLATING…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Water and waste · drain mast · pluggedFeb 16, 2006

    DURING ROUTINE C-CHECK INSPECTION, INSTL; FWD LAV DRAIN MAST PLUG AT LOWER CENTER LINE. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 01-19-06, ATI DWG H74-102 REV B DATED 01-19-06, EO SEMAN 2006114 DATED 01-19-06. REMOVED EXISTING DRAIN MAST IAW DC8 SRM 51-3-0. FABRICATED REPAIR DOUBLER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Structures (general) · plate · unknownJan 26, 2006

    FWD LAVATORY DRAIN MAST BLANKING PLATE AT 460 BL O REPLACES 53-DC8-928. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATE 09-21-05, AT SKETCH FO3-RO5 REV. B DATED 09-21-05, EO SEMAN 2006112 DATE 01-05-06. REMOVED (02 EA) EXISTING DRAIN MAST IAW DC-8 SRM 51-3-0. FABRICATED (02 EA) REPAIR DOUBLER AT…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedJan 26, 2006

    DURING ROUTINE C-CHECK INSPECTION, RT WING NR 4 WING DOUBLER LWR SKIN CRACKED .25 INCH, XS 520.222. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1A FIG 1 PAGE 3. REMOVED CRACKED DOUBLER IAW DC8 SRM 51-1-20D. STOP DRILLED CRACK. FABRICATED EXTERNAL REPAIR DOUBLER (AL7075 T6 0.063) IAW DC8 SRM 57-2-1A…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedJan 26, 2006

    DURING ROUTINE C CHECK INSPECTION, 'FWD ACCY COMPT- L-34R CRACKED BETWEEN STA 208.000 - STA 270.000. REMOVED CRACKED L-34R IAW DC-8 SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8B. INSTALLED NEW LONGERON WITH RIVETS + HILOKS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D, DC-8 SRM…

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

Showing the 10 most recent of 96 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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