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Aircraft record

N984AX1968 Douglas DC-9-32

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Apr 10, 2013.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched60 service difficulty reports

Registration
Deregistered
Last based in
Plantation, FL
owner city / state
Owners
1
since 2008
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
60
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
Oct 15, 2008
Canceled
Apr 10, 2013
Airworthiness
Standard · Transport
Airworthiness date
Jun 27, 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-9-32
Year
1968
Serial number
47258
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
ADBA16

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. 2008 – 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 (60)

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.

  • Lights · power supply · dischargedNov 23, 2007

    EMERGENCY POWER LIGHTING INOPERATIVE, NO P-NUT BULB ILLUMINATION. REPLACED EMERGENCY LIGHT POWER SUPPLY IAW DC-9 AMM 33-53-02-4.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Lights · battery · dischargedSep 15, 2007

    EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT POWER SUPPLY BATTERIES IAW DC9 MM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · support fitting · crackedSep 28, 2006

    LEFT WING INBOARD SPOILER TORQUE TUBE SUPPORT ASSEMBLY CRACKED AT XRS-236. REMOVED AND REPLACED INBOARD SPOILER SUPPORT FITTING IAW DC9 MM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · panel · damagedJun 4, 2004

    COMPLY WITH COI 42381-001. REMOVED AND REPLACED WINDOW BELT RIGHT FUSELAGE EMERGENCY EXIT AREA. COMPLIED WITH COI 42381-001.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedMay 27, 2004

    FITTING CRACKED AFT SIDE FS 1038, LONGERON 15 RIGHT. REPLACED FITTING AT AFT SIDE OF FRAME FS 1038, LONGERON 15 RIGHT IAW DC-9 SRM 51-30-5 AND 51-30-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Nacelles and pylons · attach angle · crackedMay 17, 2003

    THE RIGHT LOWER PYLON ATTACH ANGLE WAS FOUND CRACKED WHILE PERFORMING AN INSPECTION OF THE NR 2 PYLON FOR AN ENGINE CHANGE. REPAIRED ATTACH ANGLE IAW DC-9 SRM 54-04, FIG 10.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · pump · failedDec 5, 2002

    EMERGENCY DECLARED & DIVERTED. A/C CROSSTIE LOCKOUT, LT AC BUS OFF LDC BUS OFF LT GEN. APU WOULD NOT PICK UP RT SIDE. INSP LT GEN LEADS, CHECKED RESISTANCE ON LT DP CURRENT TRANS (ALL THREE). CHKD 3 CURRENT TRANS FOR LT MAIN SYS. VISUALLY INSP 3 PHASE BUS WIRING. NO DEFECTS NOTED. APU OPS CHKD…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · structure · wornOct 30, 2002

    TRAILING EDGE, WING STA. 161, UPPER SURFACE HAD EXCESSIVE WEAR. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · window frame · crackedOct 22, 2002

    HFEC CRACK INDICATION AT WINDOW CUTOUT 14 RIGHT, 1/2 INCHES FROM UPPER FORWARD CORNER EDGE 1/4" LONG. REPAIRED AREA IAW REA D953-45678-MR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · window frame · crackedOct 22, 2002

    HFEC CRACK INDICATION AT WINDOW 21 RIGHT, 1/8 INCH FROM UPPER AFT EDGE, 3/16 INCH LONG. REPAIRED AREA IAW REA D953-45696-MR.

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

Showing the 10 most recent of 60 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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