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Aircraft record

N5342G1954 Dehavilland BEAVER U-6A

DeregisteredUnclaimedSource: FAA, updated Oct 17, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Feb 7, 2018.

Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Feb 2009)No ADs since 1998 matched

Registration
Deregistered
Last based in
Maxwell Afb, AL
owner city / state
Owners
1
since 1976
NTSB events
2
substantial, 2009
ADs may apply
0
confirm with A&P
Service reports
0
since 1995

Registration

FAA Aircraft Registry · Oct 17, 2026
Last registered owner
Civil Air Patrol INC
Owner type
Corporation
City, state
Maxwell Afb, AL
Certificate issued
Sep 13, 1976
Canceled
Feb 7, 2018
Airworthiness
Standard · Normal
Airworthiness date
Sep 23, 1998

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
Dehavilland
Model
BEAVER U-6A
Year
1954
Serial number
854
Aircraft type
Fixed wing single engine
Category
Land
Certification
Type Certificated
Seats
8
Engines
1
Max takeoff weight
Up to 12,499 lb
Mode S code
A6C1EE

Engine

Type
Reciprocating

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 1976 – 2018Civil Air Patrol INCMaxwell Afb, AL

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 (2)

Accident · substantial damage

Feb 20, 2009 · Kenai, AK

The flight instructor’s decision to attempt a touch-and-go landing toward rising terrain and with a tailwind, resulting in an in-flight collision with terrain during takeoff.

Damage
Substantial
Injuries
None
Report
ANC09LA022

From NTSB records; matched by serial number.Read NTSB report (search CAROL for ANC09LA022)

Accident · substantial damage

Aug 9, 1987 · Elmendorf Afb, AK

THE INSTRUCTOR (CFI) ELECTED TO DEMONSTRATE A NO-FLAP TAKEOFF WITH CALM/GLASSY WATER CONDS. AFTER THE FLOAT PLANE HAD ACCELERATED TO ABOUT 55 TO 60 KTS WITHOUT BECOMING AIRBORNE, HE ELECTED TO ABORT THE TAKEOFF. HE STATED THAT HE ATTEMPTED A LEFT TURN & THE FLOAT PLANE SETTLED OFF STEP, BUT THE FORWARD MOMENTUM CAUSED THE ACFT TO CONT STRAIGHT AHEAD. HE CALLED FOR 'RUDDERS,' MEANING WATER…

Damage
Substantial
Injuries
None
Report
ANC87FA118

From NTSB records; matched by N-number.Read NTSB report (search CAROL for ANC87FA118)

Accident history for this model

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 (0)

No Service Difficulty Reports found for this airframe since 1995.

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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