Turbine helicopter

N114DR

1995 Bell UH-1H

Registered 1 NTSB/FAA record
Built
1995
Serial
66-00792
Class
Turbine helicopter
Engines
Lycoming T53-L-13
Status
Current as of October 2026
Registered owner
Northwest Helicopters I Inc (Corporation)
Based
Olympia, WA
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1995 Bell UH-1H
Representative photo of a Bell UH-1H. Not a photo of N114DR.
Registration record

N114DR on the FAA register

Type
1995 Bell UH-1H
Serial
66-00792
Engines
Lycoming T53-L-13
Registered owner
Northwest Helicopters I Inc
Olympia, WA
Certificate issued
2001-04-11
Airworthiness date
1995-06-02
Registration expires
2030-01-31
Airworthiness class
Restricted
Mode S (hex)
A03B6A
Mode S (octal)
50035552
Seats (type)
15
Weight class
up to 12,499 lb
Range (type)
274 nm
Cruise (type)
109 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2030-01-31
    Registration expires (renewal due).
  • 2002-06-21
    Accident at Clark Fork, ID; damage: substantial.
  • 2001-04-11
    Certificate of registration issued as N114DR to the current registrant.
  • 1995-06-02
    Airworthiness date on the current FAA record (restricted category).
  • 1993-06-16
    N114DR previously assigned to a Homebuilt Bensen Type (s/n DGR1); cancelled.
Overview

About N114DR

N114DR is a 1995 Bell UH-1H, serial number 66-00792. The FAA register lists Northwest Helicopters I Inc as the registrant in Olympia, Washington. The current certificate of registration was issued on April 11, 2001 and expires on January 31, 2030.

The FAA aircraft reference file describes the type as a turbine helicopter, one Lycoming T53-L-13 engine and 15 seats. Published figures for the type give a cruise speed of about 109 knots and a range of about 274 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is restricted category, dated June 2, 1995.

N114DR has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
109 kt
Range
274 nm
Fuel burn
10 gph

Published figures for the Bell UH-1H type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2002-06-21 Accident · Clark Fork, ID Damage: Substantial Fatal injury NTSB · SEA02FA108
Reported aircraft: Garlick UH-1H
Probable cause: A failure of unknown origin in the tail rotor drive assembly. Factors include mountainous terrain unsuitable for an emergency landing.

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.