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Airworthiness Directives; Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 Airplanes

airworthiness · Rule · Final rule. · Published 2005-06-07 · Effective 2005-07-12 · 70 FR 32986

Document

Document number
05-11054
Federal Register citation
70 FR 32986
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-06-07
Effective date
2005-07-12
FAA docket
Docket No. FAA-2005-20756

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bombardier Model DHC-8-102, -103, -106, -201, -202, -301, -311 and -315 airplanes. This AD requires installation of check valves in Numbers 1 and 2 hydraulic systems, removal of the filters from the brake shuttle valves, and removal of the internal garter spring from the brake shuttle valves. This AD results from two instances of brake failure due to the loss of hydraulic fluid from both Numbers 1 and 2 hydraulic systems and one incident of brake failure due to filter blockage in the shuttle valve. We are issuing this AD to prevent the loss of hydraulic power from both hydraulic systems, which could lead to reduced controllability of the airplane, and to prevent brake failure, which could result in the loss of directional control on the ground and consequent departure from the runway during landing.

Source

Authoritative
Federal Register document
Machine
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