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Airworthiness Directive

AD 95-09-06 60 FR 21976 Active

Federal Aviation Administration · 14 CFR part 39

FR document
95-10589
Amendment
39-9209
Published
1995-05-04
Effective
1995-06-08
Models covered
1
Last live check
2026-10-03

Printed from https://aircraftdirectives.com/ad/95-09-06 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

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AD

95-09-06

FR doc 95-10589 · 60 FR 21976

AD 95-09-06Published 1995-05-04Effective 1995-06-08

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires installing a protective mechanical fuel valve switch guard on the fuel valve switch.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to Bell Helicopter Textron, Inc. (BHTI) Model 206A, 206B, 206L, 206L-1, and 206L-3 helicopters, that requires installing a protective mechanical fuel valve switch guard on the fuel valve switch. This amendment is prompted by reports of airmen inadvertently placing the fuel valve switch to the ``OFF'' position. The actions specified by this AD are intended to prevent the fuel valve switch from being inadvertently placed in the ``OFF'' position, which could result in an engine failure and a subsequent power-off landing.

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All Bell 206 JetRanger / LongRanger directives

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab)

Applies to 1 model in our index