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Aircraft record

N988AX1967 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 Jan 15, 2010.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched90 service difficulty reports

Registration
Deregistered
Last based in
Groveland, FL
owner city / state
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
90
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Individual owner
City, state
Groveland, FL
Canceled
Jan 15, 2010
Airworthiness
Standard · Transport
Airworthiness date
Apr 13, 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-9-32
Year
1967
Serial number
47084
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
ADC8F2

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. until 2010Individual ownerGroveland, 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 (90)

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 · battery · inoperativeOct 4, 2005

    OVERHEAD COCKPIT EMERGENCY LIGHTS INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERIES IAW AMM 33-53-00-8.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · corrodedAug 5, 2004

    LONGERON 24 RT END CAP AT STA 945 WAS CORRODED. REPLACED END CAP IAW SRM 51-30-2 AND 51-30-5.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · pan · crackedAug 4, 2004

    FORWARD LOWER CARGO DOOR OUTER PAN CRACKED AT FASTENER HOLE AT UPPER FORWARD CORNER. REPLACED FORWARD LOWER CARGO DOOR ON N.R. 0399 IAW DC-9 SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Doors · pan · crackedAug 4, 2004

    FORWARD LOWER CARGO DOORS OUTER PAN HAD CRACK INDICATION IN OUTER RADIUS OF FORWARD HINGE. REPLACED DOOR ON NR 0399 IAW SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · pan · defectiveAug 4, 2004

    FORWARD LOWER CARGO DOOR HAD DEFECT INDICATION IN OUTER PAN ALONG UPPER EDGE AT FORWARD STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · pan · crackedAug 4, 2004

    FORWARD LOWER CARGO DOORS OUTER PAN WAS CRACKED AT HI-LOCK ALONG AFT EDGE, CENTER STOP PAD AREA. REPLACED DOOR ON NR 0399 IAW SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · skin · corrodedAug 4, 2004

    FORWARD LOWER CARGO DOORS EXTERIOR SKIN HAD PITTING, CORROSION AT AFT LOWER CORNER. REPLACED DOOR ON NR 0399 IAW SRM.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · skin · crackedAug 3, 2004

    FUSELAGE SKIN CRACKED AT RIVET ON LONGERON 22 LT BETWEEN FS 180-200. REPAIRED ON EA 53300031-001.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedAug 3, 2004

    RT MAIN FRAME STA 699 WAS CRACKED IN FORWARD UPPER FLANGE BETWEEN Z-CLIP FASTENERS. REPAIRED MAIN FRAME RT 699 IAW EA 53400120-001-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedAug 3, 2004

    LONGERON 4 LT CRACKED AT FS 160 SPLICED SECTION OF LONGERON IAW SRM 53-02.

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

Showing the 10 most recent of 90 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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