2008-14-01: Fuel valve switch
FAA order 2008-14-01 is an airworthiness directive in force since August 14, 2008. The FAA's subject line: Fuel valve switch. It names Bell 222, Bell 230, Bell 430: about 64 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: engine.
What it applies to as the FAA lists it
Dates and paperwork
- In force since
- August 14, 2008
- Published
- July 10, 2008 (signed June 12, 2008)
- Docket
- FAA-2008-0039
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The FAA's summary their words, unchanged
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.
The order itself the regulatory text, as published
Show the full text (2,820 characters)
Related safety bulletins advice on the same designs, not orders
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 26, 2026. Connections as data: /graph/directive/2008-14-01.json · aircraft systems.
