N550AS

Bell 412

Bell Helicopter Textron Inc.

3 Hours

Duration of Flight

402 NM

Range

140 MPH

Max Speed

N550AS

Gallery

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Aircraft Class
Aircraft Class
Under 12,500lbs
Max passengers
Max passengers
0
Range
Range
402 NM
Service Ceiling
Service Ceiling
20000 ft
Duration of Flight
Duration of Flight
3 Hours
Max Speed
Max Speed
140 MPH

Basic Information

Year Manufactured1982
LocationSalt Lake City, UT, US
Registration NumberN550AS
OwnershipBank of Utah Trustee
Serial Number33066

Airframe

Data valid as of 2015-09-22
AFTT (hrs)
Current
N/A
Flight
N/A
Est.
N/A
Landings/Cycles
Current
N/A
Flight
N/A
Est.
N/A
Nautical Miles
Current
N/A
Flight
N/A
Est.
N/A
No flights

No flight history available

Flight records for this aircraft have not been tracked yet.

AI Summary

Fact-checked by AI

Bell 412

Overview

Deregistered from the US register and exported (registered as 5Y-PAH). Last US owner listed as Bank of Utah Trustee; US deregistration/export activity reported in 2015.

Specifications

  • Engines: 2× Pratt & Whitney Canada PT6T-3 Twin-Pac (900 lbf each)
  • Range: 402 nm
  • Cruise: 122 kts
  • Ceiling: 20000 ft

Model & Market Context

The rotorcraft registered as N550AS is a single airframe of the Bell 412 family built by Bell Helicopter Textron Inc. and completed in 1982 with serial number 33066. Current title records identify the owner as Bank of Utah Trustee, a trust located in Salt Lake City, UT, US, and the helicopter is registered in the US civil registry. The airframe is powered by twin turbine modules and is commonly referenced by its specific construction serial when tracking maintenance and ownership history. Public registry actions beyond the current trust ownership and national registration are not published.

Cabin layout, seating configuration, and specific avionics fit for this serial are not published. Typical mission profiles associated with this airframe class align with medium-lift, multi-role rotorcraft operations, but mission history specific to N550AS is not published. The listed owner and trustee location indicate the administrative/operator base is Salt Lake City, UT, and the helicopter is recorded as a US-registered asset. Maintenance considerations tied to the twin PT6T-3 powerplants and the 1982 build year would normally drive lifecycle and inspection planning, though documented condition and valuation for this airframe are not published.

The Bell 412 occupies a performance niche as a twin-engine medium utility helicopter, with the twin PT6T-3 Twin-Pac providing the rated thrust values detailed for this airframe. In market terms, helicopters of this type are commonly compared with other medium twin-engine rotorcraft for utility, emergency services, and corporate transport roles; specific resale demand and appraisal for this serial are not published. Maintenance and resale considerations for an aircraft built in 1982 with twin PT6T series engines typically center on engine life limits, component serviceability, and documented maintenance pedigree, none of which are published for this particular airframe.

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