Turbine helicopter

N108AE

1981 Bell 206L I/C30P

Registered 1 NTSB/FAA record
Built
1981
Serial
45730
Class
Turbine helicopter
Engines
Allison 250 SER 250HP
Status
Current as of October 2026
Registered owner
Air Evac Ems Inc (Corporation)
Based
Ofallon, MO
1981 Bell 206L I/C30P
Representative photo of a Bell 206L I/C30P. Not a photo of N108AE.
Registration record

N108AE on the FAA register

Type
1981 Bell 206L I/C30P (FAA: Bell Helicopter Textron 206L-1)
Serial
45730
Engines
Allison 250 SER 250HP
Registered owner
Air Evac Ems Inc
Ofallon, MO
Certificate issued
2005-10-26
Airworthiness date
1981-09-18
Registration expires
2028-08-31
Airworthiness class
Standard · normal
Mode S (hex)
A02271
Mode S (octal)
50021161
Seats (type)
7
Weight class
up to 12,499 lb
Range (type)
339 nm
Cruise (type)
124 kt
Status
Current as of October 2026
Registry history

Timeline

  • 2028-08-31
    Registration expires (renewal due).
  • 2005-10-26
    Certificate of registration issued as N108AE.
  • 2002-11-08
    Accident at Albany, KY; damage: substantial.
  • 1981-09-18
    Airworthiness date on the current FAA record (standard category (normal)).
Overview

About N108AE

N108AE is a 1981 Bell 206L I/C30P (FAA model 206L-1), serial number 45730. The FAA register lists Air Evac Ems Inc as the registrant in Ofallon, Missouri. The current certificate of registration was issued on October 26, 2005 and expires on August 31, 2028.

The FAA aircraft reference file describes the type as a turbine helicopter, one Allison 250 SER 250HP engine and 7 seats. Published figures for the type give a cruise speed of about 124 knots and a range of about 339 nm; actual performance depends on configuration, load and conditions. Its airworthiness certificate is standard category (normal), dated September 18, 1981.

N108AE has 1 accident/incident record on file (most serious damage: substantial); details are below.

Cruise
124 kt
Range
339 nm
Fuel burn
12 gph

Published figures for the Bell 206L I/C30P type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2002-11-08 Accident · Albany, KY Damage: Substantial NTSB · IAD03LA015
Reported aircraft: Bell 206L1
Probable cause: The pilot's inadequate in-flight planning, which resulted in an angle of approach in relative wind conditions conducive to a loss of helicopter tail rotor effectiveness. A factor was the obstacles surrounding the landing field.

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.