Turbine helicopter

N3132B

Bell 206

Registered No accidents on file
Built
—
Serial
3544
Class
Turbine helicopter
Engines
1
Status
Current as of October 2026
Registered owner
Usda Aphis Ws Atoc (Government)
Based
Cedar City, UT
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Registration record

N3132B on the FAA register

Type
Bell 206
Serial
3544
Engines
1
Registered owner
Usda Aphis Ws Atoc
Cedar City, UT
Certificate issued
2024-08-13
Airworthiness date
—
Registration expires
2031-08-31
Airworthiness class
—
Mode S (hex)
A35496
Mode S (octal)
50652226
Seats (type)
4
Weight class
up to 12,499 lb
Range (type)
374 nm
Status
Current as of October 2026
Registry history

Timeline

  • 2031-08-31
    Registration expires (renewal due).
  • 2024-08-13
    Certificate of registration issued as N3132B to the current registrant.
  • 2006-08-10
    N3132B previously assigned to a Piper 6X (s/n 3232061); cancelled.
  • 1992-02-18
    N3132B previously assigned to a Homebuilt KR-2 (s/n 043101101A); cancelled.
  • 1989-11-13
    N3132B previously assigned to a Cessna 170B (s/n 25374); cancelled.
Overview

About N3132B

N3132B is a Bell 206, serial number 3544. The FAA register lists Usda Aphis Ws Atoc as the registrant in Cedar City, Utah. The current certificate of registration was issued on August 13, 2024 and expires on August 31, 2031.

The FAA aircraft reference file describes the type as a turbine helicopter and 4 seats. Published figures for the type give a range of about 374 nm; actual performance depends on configuration, load and conditions.

No NTSB accident or incident reports and no FAA preliminary notices are on file for this airframe as N3132B. 1 earlier record involves a different aircraft that carried the same N-number.

Range
374 nm

Published figures for the Bell 206 type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

1989-05-23 Accident · Birchwood, AK Damage: Substantial Minor injury NTSB · ANC89FA076
Reported aircraft: Cessna 170B — a different aircraft that carried the N3132B registration before this airframe.
Probable cause: FAILURE OF THE PILOT TO ASSURE THAT THE FUEL SELECTOR WAS IN THE PROPER DETENT FOR TAKEOFF. A FACTOR RELATED TO THE ACCIDENT WAS: THE SOFT/MUDDY TERRAIN CONDITIONS IN THE EMERGENCY LANDING AREA.

Sources: NTSB aviation accident database and CAROL case system, FAA preliminary accident & incident notices. Search accident records

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Data: FAA Aircraft Registry (October 2026), including deregistered aircraft; NTSB and FAA accident data; fyiAero listing history. Individual owners' names are shown to signed-in users and street addresses are never shown. Type figures are published specifications, not this aircraft's.