N417AE

Valid Registration

2014 BELL HELICOPTER TEXTRON CANADA 206L-4

N417AE is a 2014 BELL HELICOPTER TEXTRON CANADA 206L-4 registered to AIR EVAC EMS INC in O FALLON, MO. Its FAA registration status is Valid. It has 2 NTSB accident records on file. 9 Airworthiness Directives may apply.

Registration Details

N-Number
N417AE
Serial Number
52463
Manufacturer
BELL HELICOPTER TEXTRON CANADA
Model
206L-4
Year
2014
Registration Status
Valid
Airworthiness Date
2014-05-13
Owner
AIR EVAC EMS INC
Owner City
O FALLON
Owner State
MO

The BELL HELICOPTER TEXTRON CANADA 206L-4 is registered with the FAA under N-number N417AE. This airframe was manufactured in 2014. Its manufacturer serial number is 52463. The aircraft was issued its airworthiness certificate on 2014-05-13. The current registered owner is AIR EVAC EMS INC, based in O FALLON, MO. Registration data is sourced from the FAA Releasable Aircraft Database and refreshed weekly.

Accident History

Fatal injuries2009-09-25

Georgetown, SC, USA

Accident — EUROCOPTER AS-350 (NTSB ERA09FA537)

No injuries reported2008-05-21

Hiram, GA, USA

Accident — Eurocopter France AS350 B2 (NTSB MIA08LA106)

Severity reflects injuries to people involved, not damage to the aircraft. A “no injuries” accident can still involve significant aircraft damage.

N417AE has been involved in 2 NTSB accidents since 1982. Each record above includes the date, location, severity, and NTSB summary. Buyers should review the full accident narratives and verify repairs in the aircraft's logbooks before purchase.

Applicable Airworthiness Directives

9 found
AD 2011-4465Effective: 2011-03-10

Airworthiness Directives; Bell Helicopter Textron Canada Limited (BHTC) Model 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 222, 222B, 222U, 230, 407, 427, and 430 Helicopters

This document publishes in the Federal Register an amendment adopting Emergency Airworthiness Directive (AD) 2010-26-51, which was sent previously to all known U.S. owners and operators of the specified model helicopters by individual letters. This AD also supersedes existing AD 2009-08-03. This AD is prompted by another incident in which the tail rotor blade (blade) tip weight separated from a blade during flight causing vibration. This unsafe condition led to the determination that additional blades could be affected and should be added to the applicability. The actions specified by this AD are intended to prevent loss of the blade tip weight, loss of a blade, and subsequent loss of control of the helicopter.

Airworthiness Directives (ADs) are FAA-mandated safety directives that apply to specific aircraft, engines, or components. N417AE may be affected by 9 directives. All applicable ADs must be complied with for the aircraft to remain legally airworthy. Buyers should verify AD compliance in the aircraft's logbooks before purchase.

+8 more Airworthiness Directives found for this aircraft

Full list, with effective dates and links to the official Federal Register documents, is included in the paid report.

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Get the complete history for N417AE

Full accident narratives, all Airworthiness Directives, ownership chain, and a downloadable PDF.

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