Turbine helicopter

N32AE

1979 Bell 206L I/C30P

Registered 1 NTSB/FAA record
Built
1979
Serial
45327
Class
Turbine helicopter
Engines
Allison 250 SER 250HP
Status
Current as of October 2026
Registered owner
Air Evac Ems Inc (Corporation)
Based
O Fallon, MO
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1979 Bell 206L I/C30P
Representative photo of a Bell 206L I/C30P. Not a photo of N32AE.
Registration record

N32AE on the FAA register

Type
1979 Bell 206L I/C30P (FAA: Bell Helicopter Textron 206L-1)
Serial
45327
Engines
Allison 250 SER 250HP
Registered owner
Air Evac Ems Inc
O Fallon, MO
Certificate issued
2005-10-26
Airworthiness date
1979-10-29
Registration expires
2028-07-31
Airworthiness class
Standard · normal
Mode S (hex)
A36BFC
Mode S (octal)
50665774
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).
  • 2020-03-05
    Accident at Clark, MO; damage: substantial.
  • 2005-10-26
    Certificate of registration issued as N32AE to the current registrant.
  • 1979-10-29
    Airworthiness date on the current FAA record (standard category (normal)).
Overview

About N32AE

N32AE is a 1979 Bell 206L I/C30P (FAA model 206L-1), serial number 45327. 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 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 October 29, 1979.

N32AE 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

2020-03-05 Accident · Clark, MO Damage: Substantial NTSB · CEN20LA113
Reported aircraft: Bell 206
Probable cause: The fatigue failure of the pneumatic line for reasons that could not be determined, which resulted in a loss of engine power and subsequent hard 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.