Turbine helicopter

N27AE

1978 Bell 206L I/C30P

Registered 2 NTSB/FAA records
Built
1978
Serial
45192
Class
Turbine helicopter
Engines
Allison 250 SER 400HP
Status
Current as of October 2026
Registered owner
Air Evac Ems Inc (Corporation)
Based
O Fallon, MO
1978 Bell 206L I/C30P
Representative photo of a Bell 206L I/C30P. Not a photo of N27AE.
Registration record

N27AE on the FAA register

Type
1978 Bell 206L I/C30P (FAA: Bell Helicopter Textron 206L-1)
Serial
45192
Engines
Allison 250 SER 400HP
Registered owner
Air Evac Ems Inc
O Fallon, MO
Certificate issued
2005-10-26
Airworthiness date
1978-12-20
Registration expires
2028-07-31
Airworthiness class
Standard · normal
Mode S (hex)
A2A428
Mode S (octal)
50522050
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

  • 2028-07-31
    Registration expires (renewal due).
  • 2005-10-26
    Certificate of registration issued as N27AE to the current registrant.
  • 2003-01-31
    Accident at West Plains, MO; damage: substantial.
  • 1998-09-28
    N27AE previously assigned to a Bell 206L-3 (s/n 51141); cancelled.
  • 1998-05-24
    Accident at Springdale, AR; damage: substantial.
  • 1978-12-20
    Airworthiness date on the current FAA record (standard category (normal)).
Overview

About N27AE

N27AE is a 1978 Bell 206L I/C30P (FAA model 206L-1), serial number 45192. The FAA register lists Air Evac Ems Inc as the registrant in O Fallon, Missouri. The current certificate of registration was issued on October 26, 2005 and expires on July 31, 2028.

The FAA aircraft reference file describes the type as a turbine helicopter, one Allison 250 SER 400HP 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 December 20, 1978.

N27AE has 2 accident/incident records 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

2003-01-31 Accident · West Plains, MO Damage: Substantial NTSB · CHI03LA062
Reported aircraft: Bell 206L-1
Probable cause: The excessive descent rate that required an abrupt flare, resulting in the main rotor severing the tailboom.
1998-05-24 Accident · Springdale, AR Damage: Substantial Serious injury NTSB · FTW98FA239
Reported aircraft: Bell 206L-3
Probable cause: The failure of maintenance personnel to properly assemble the engine's accessory gearbox, which resulted in a total loss of engine power due to partial blockage of the main oil passage by an o-ring. The blockage reduced oil flow to the turbine shafting, which led to the total failure of the gas producer turbine shaft and the power (free) turbine shaft. A factor was the lack of suitable terrain for the forced 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.