Turbine helicopter

N395AE

Bell 206L I/C30P / 206L-1

Registered 1 NTSB/FAA record
Built
—
Serial
45551
Class
Turbine helicopter
Engines
Allison 250-C28B
Status
Current as of October 2026
Registered owner
Air Evac Ems Inc (Corporation)
Based
O Fallon, MO
Registration record

N395AE on the FAA register

Type
Bell 206L I/C30P / 206L-1
Serial
45551
Engines
Allison 250-C28B
Registered owner
Air Evac Ems Inc
O Fallon, MO
Certificate issued
2009-08-03
Airworthiness date
1981-10-13
Registration expires
2028-02-29
Airworthiness class
Multiple
Mode S (hex)
A49561
Mode S (octal)
51112541
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

  • 2028-02-29
    Registration expires (renewal due).
  • 2019-04-15
    Accident at Dublin, GA; damage: substantial.
  • 2009-08-03
    Certificate of registration issued as N395AE.
  • 1981-10-13
    Airworthiness date on the current FAA record (multiple category).
Overview

About N395AE

N395AE is a Bell 206L I/C30P / 206L-1, serial number 45551. The FAA register lists Air Evac Ems Inc as the registrant in O Fallon, Missouri. The current certificate of registration was issued on August 3, 2009 and expires on February 29, 2028.

The FAA aircraft reference file describes the type as a turbine helicopter, one Allison 250-C28B 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 multiple category, dated October 13, 1981.

N395AE 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 / 206L-1 type. They describe the model, not this airframe's equipment or condition.

Safety record

Accident & incident history

2019-04-15 Accident · Dublin, GA Damage: Substantial NTSB · ERA19LA152
Reported aircraft: Bell 206
Probable cause: A partial loss of engine power on takeoff due to separation of the diffuser assembly as a result of incomplete braze joint surfaces on the vane airfoils.

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.