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Airworthiness Directives; Bombardier Model DHC-8-102, -103, and -106 Airplanes

airworthiness · Rule · Final rule. · Published 2004-07-13 · Effective 2004-08-17 · 69 FR 41928

Document

Document number
04-15513
Federal Register citation
69 FR 41928
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-07-13
Effective date
2004-08-17
FAA docket
Docket No. 2002-NM-339-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, and -106 airplanes, that requires repetitive detailed inspections of the left and right aileron tab actuator arm channels for cracking, and corrective actions if necessary. This proposal also provides an optional terminating action for the repetitive inspections. This action is necessary to prevent increased roll forces due to cracking of the left and right aileron tab actuator arms, which could be interpreted by the pilot as a flight control problem and might lead to 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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