Airworthiness Directive

AD 2008-14-01 73 FR 39569 Active

Federal Aviation Administration · 14 CFR part 39

FR document
E8-14718
Amendment
39-15596
Published
2008-07-10
Effective
2008-08-14
Models covered
3
Last live check
2026-09-30
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AD

2008-14-01

FR doc E8-14718 · 73 FR 39569

AD 2008-14-01Published 2008-07-10Effective 2008-08-14

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 rewiring and testing the fuel valve switch on each engine and testing the ignitor system.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 222, 222B, 222U, 230 and 430 helicopters that requires rewiring and testing the fuel valve switch on each engine and testing the ignitor system. This amendment is prompted by an in-flight incident in which a fuel valve switch failed, causing the fuel valve to inadvertently close. The actions specified by this AD are intended to prevent interruption of the fuel supply caused by failure of the fuel switch, which could result in loss of engine power and subsequent loss of control of the helicopter.

More directives for Bell 222

  1. AD 2026-17-51 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2026-08-28
  2. AD 2021-19-01 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2021-09-08
  3. AD 2016-08-17 Airworthiness Directives; Bell Helicopter Textron Canada Helicopters 2016-04-25
  4. AD 2013-18-06 Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) ... 2013-09-12
  5. AD 2010-26-51 Airworthiness Directives; Bell Helicopter Textron Canada Limited (BHTC) ... 2011-03-10

All Bell 222 directives

Applies to 3 models in our index