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Aircraft record

N966AXDouglas DC-9-41

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Sep 30, 2013.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched69 service difficulty reports

Registration
Deregistered
Last based in
Plantation, FL
owner city / state
Owners
1
since 2010
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
69
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Dhl Network Operations (usa) INC
Owner type
Corporation
City, state
Plantation, FL
Certificate issued
May 12, 2010
Canceled
Sep 30, 2013
Airworthiness
Standard · Transport
Airworthiness date
Feb 25, 1992

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-9-41
Serial number
47510
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
85
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AD7286

Engine

Make and model
P & W Jt8d Series
Type
Turbo-jet
Power
7,700 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. 2010 – 2013Dhl Network Operations (usa) INCPlantation, FL

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (69)

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 · bolt · looseSep 19, 2008

    LOOSE TIE BOLTS. WHEEL SCRAPPED. (K) BOLTS BACKED OFF. REQUIRES OVERHAUL. OVERHAULED IAW ABX SPEC WORKSHEET BS421A DATED 12/21/07 AND THE ABX WHEEL AND TIRE MANUAL, REV 18.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · actuator · damagedFeb 29, 2008

    UPON PUTTING GEAR HANDLE DOWN, HEARD LOUD BANG AND SHUTTER IN AIRCRAFT. NORMAL GEAR INDICATION. FOUND RIGHT MAIN LANDING GEAR ACTUATOR EYE BOLT PULLED OUT OF THE ACTUATOR. REPLACED THE RIGHT MAIN LANDING GEAR ACTUATOR IAW DC9 AMM 32-32-02.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery · dischargedOct 8, 2007

    EMERGENCY LIGHTS WOULD NOT ILLUMINATE DURING PREFLIGHT. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM 33-53-00-8.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · cusp web · crackedJan 31, 2007

    CUSP WEB CRACKED AT RIGHT BUTT LINE 54, STA 224. REPAIRED CUSP WEB AT RIGHT BUTT LINE 54, STA 224 IAW DC9 SRM 53-01, FIGURE 2.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedJan 28, 2007

    RIGHT FORWARD MAIN FRAME WAS CORRODED IN FORWARD UPPER FLANGE BETWEEN POINTS G & J OF ES01144, STA 737. REPAIRED MAIN FRAME IAW EA 53400120-001-2.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · corrodedJan 28, 2007

    SEAT TRACK CORRODED, RIGHT BUTT LINE 54, STA 225 TO 256. REMOVED AND REPLACED SEAT TRACK FS 200 - 300 AT RIGHT BUTT LINE 54.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · seat track · corrodedJan 28, 2007

    CENTER TRACK CORRODED BETWEEN FS 636 - 655. REMOVED AND REPLACED CENTER TRACK STA 590 - 972 IAW DC9 SRM 51-30-1 AND 51-10-4.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · corrodedJan 26, 2007

    LONGERON 30 CORRODED AT FS 794. REPAIRED IAW REA D953-55365 MR AND DC9 SRM 55-02, FIGURE 12.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedFeb 18, 2005

    CRACKED FRAME AT STA 1152, LONGERON 15 LEFT, FORWARD OF LEFT EPR TRANSMITTER. REPAIRED AREA IAW DC-9 SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · window frame · crackedFeb 17, 2005

    CRACK INDICATIONS ON LOWER RIGHT WINDSHIELD ZEE. REMOVED AND REPLACED NEW ZEE ANGLE IAW DC-9 SRM 51-30-5 AND 51-30-8.

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

Showing the 10 most recent of 69 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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