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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 2004-02-11 · Effective 2004-03-17 · 69 FR 6546

Document

Document number
04-2681
Federal Register citation
69 FR 6546
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-02-11
Effective date
2004-03-17
FAA docket
Docket No. 2002-NM-79-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-102, -103, -106, -201, - 202, -301, -311, and -315 airplanes, that requires a one-time inspection to determine the serial numbers of the elevator and aileron servos of the drive assemblies of the automatic flight control system, and follow-on corrective actions if necessary. This action is necessary to prevent separation of the screws from the autopilot clutch assembly of the SM-300 servo, which could result in uncommanded engagement of the autopilot servo and consequent reduced controllability of the airplane. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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