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Airworthiness Directives; Bombardier Model DHC-8-301, -311, and -315 Airplanes

airworthiness · Rule · Final rule. · Published 2004-06-29 · Effective 2004-08-03 · 69 FR 38812

Document

Document number
04-14319
Federal Register citation
69 FR 38812
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-06-29
Effective date
2004-08-03
FAA docket
Docket No. 2002-NM-297-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-301, -311, and -315 airplanes. This AD requires determining the modification number of the angle of attack (AOA) sensor vanes; testing the movement of the affected vanes to evaluate sticking against both the upper and the lower vane travel end stops; and corrective action, if necessary. This action is necessary to prevent an incorrect AOA indication to the stall warning system in flight, which could result in an inadvertent stall and consequent loss of control of the airplane. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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