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Aircraft record

N941AXDouglas DC-9-31

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Mar 31, 2016.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched101 service difficulty reports

Registration
Deregistered
Last based in
Fernley, NV
owner city / state
Owners
1
since 2008
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
101
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Logistic Air INC
Owner type
Corporation
City, state
Fernley, NV
Certificate issued
Dec 10, 2008
Canceled
Mar 31, 2016
Airworthiness
Standard · Transport
Airworthiness date
Nov 6, 1989

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-9-31
Serial number
47419
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
AD10F5

Engine

Type
Turbo-jet

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 – 2016Logistic Air INCFernley, NV

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 (101)

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.

  • Fuselage · doubler · crackedFeb 16, 2006

    LEFT CLEARVIEW WINDOW STEEL SHIM WAS CRACKED AT TWO RIVETS. REMOVED AND REPLACED DOUBLER ON LEFT CLEARVIEW UPPER AFT CORNER IAW DC9 SRM 51-30-2 AND 51-30-1.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · doubler · crackedFeb 16, 2006

    RIGHT CLEARVIEW WINDOW STEEL SHIM WAS CRACKED AT RIVET. REMOVED NOTED SHIM DOUBLER AND INSTALLED NEW DOUBLER IAW DC9 DRAWING 5754088.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · frame · crackedFeb 14, 2006

    RIGHT FORWARD MAIN FRAME WAS CRACKED BEYOND LIMITS OF REPAIR. REMOVED AND REPLACED MAIN FRAME ON JOB CARD EA 53400322-001-2.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Fuselage · door · crackedFeb 14, 2006

    DOUBLER AT RIGHT UPPER AFT, AFT PRESSURE BULKHEAD DOOR CORNER HAD A .875 INCH RADIAL CRACK. REPAIRED AREA IAW REA D953-53267MR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · fitting · crackedFeb 13, 2006

    FITTING CRACKED FORWARD OF INBOARD DOOR ACTUATOR. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Wings · fitting · crackedApr 28, 2004

    LEFT FLAP HAD CRACKED FITTING AT SPLICE BETWEEN NR 4 AND 5 REMOVEABLE TRAILING EDGE SEGMENTS. REPLACED 2 EACH NEW FITTINGS IAW DC-9 SRM 51-30-2 AND 51-30-1. P/N: 9955813-509 AND -507.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Stabilizers · panel · crackedApr 27, 2004

    LT AND RT ANGLES INSIDE WRAP PANEL FORWARD OF RAM AIR SCOOP WERE CRACKED. REPLACED ANGLES IAW DC-9 SRM 51-30-2 AND 51-30-5. P/N: 5912188-49 AND -50.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedApr 26, 2004

    LONGERON 30 CRACKED, STA. 588. REPAIRED LONGERON 30 IAW REA D953-49676MR. REPAIRED FRAME AT FS 579 IAW DC-9 SRM 53-03.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · longeron · crackedApr 26, 2004

    LONGERON 29 LT CRACKED AT STA. 588. REPAIRED LONGERON 29 LT IAW DC-9 SRM 53-02 AND REA D953-49676MR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · door frame · crackedApr 26, 2004

    AFT PRESSURE BULKHEAD DOOR JAMB LEFT UPPER STOP FITTING CRACKED ON HORIZONTAL LEG. REPLACED FITTING IAW DC-9 SRM 51-30-2.

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

Showing the 10 most recent of 101 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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