Airworthiness Directive

AD 2007-26-10 Amendment 39-15312

Federal Aviation Administration · 14 CFR part 39

FR document
E7-25389
Amendment
39-15312
Published
2008-01-02
Models covered
1
Last live check
Not yet re-verified
AD

2007-26-10

FR doc E7-25389

AD 2007-26-10Published 2008-01-02Effective 2008-02-06

Requires replacing a certain servo actuator-to-actuator support attachment bolt (bolt) with an airworthy bolt.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 430 helicopters that requires replacing a certain servo actuator-to-actuator support attachment bolt (bolt) with an airworthy bolt. This action also requires establishing a retirement life for certain bolts and recording the retirement life on a component history card or equivalent record. This amendment is prompted by further evaluation of certain fatigue- critical parts, resulting in establishing a life limit of 5,000 hours for the affected bolts. The actions specified by this AD are intended to prevent fatigue failure of the bolt and subsequent loss of control of the helicopter.

Applies to 1 model in our index