Turbine helicopter

N631HC

2016 Agusta AW109SP

Registered 1 NTSB/FAA record
Built
2016
Serial
22349
Class
Turbine helicopter
Engines
2 × Pratt & Whitney Canada PW207C
Status
Current as of October 2026
Registered owner
Intermountain Medical Transport LLC (LLC)
Based
Salt Lake City, UT
Registration record

N631HC on the FAA register

Type
2016 Agusta AW109SP
Serial
22349
Engines
2 × Pratt & Whitney Canada PW207C
Registered owner
Intermountain Medical Transport LLC
Salt Lake City, UT
Certificate issued
2026-06-19
Airworthiness date
2025-12-11
Registration expires
2033-06-30
Airworthiness class
Standard · acrobatic
Mode S (hex)
A84225
Mode S (octal)
52041045
Seats (type)
8
Weight class
up to 12,499 lb
Range (type)
512 nm
Cruise (type)
147 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2033-06-30
    Registration expires (renewal due).
  • 2026-06-19
    Certificate of registration issued as N631HC to the current registrant.
  • 2025-12-11
    Airworthiness date on the current FAA record (standard category (acrobatic)).
  • 2025-09-09
    N631HC previously assigned to a Agustawestland Spa AW109SP (s/n 22312); cancelled.
  • 2024-10-08
    Accident at Kamas, UT; damage: substantial.
  • 2016
    Manufactured (2016).
Overview

About N631HC

N631HC is a 2016 Agusta AW109SP, serial number 22349. The FAA register lists Intermountain Medical Transport LLC as the registrant in Salt Lake City, Utah. The current certificate of registration was issued on June 19, 2026 and expires on June 30, 2033.

The FAA aircraft reference file describes the type as a turbine helicopter, two Pratt & Whitney Canada PW207C engines and 8 seats. Published figures for the type give a cruise speed of about 147 knots and a range of about 512 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (acrobatic), dated December 11, 2025.

N631HC has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
147 kt
Range
512 nm
Fuel burn
14 gph

Published figures for the Agusta AW109SP type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2024-10-08 Accident · Kamas, UT Damage: Substantial Minor injury NTSB · WPR25LA006
Reported aircraft: Agustawestland Spa AW109SP
Probable cause: The pilot s exceedance of the helicopter s available power while landing in a confined area, which resulted in a loss of tail rotor effectiveness and a hard landing.
NTSB report ↗

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.