← FAA Federal Register actions

Airworthiness Directives; Bombardier Model DHC-8-401 and -402 Airplanes

airworthiness · Rule · Final rule. · Published 2004-03-25 · Effective 2004-04-29 · 69 FR 15233

Document

Document number
04-6501
Federal Register citation
69 FR 15233
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bombardier Model DHC-8-401 and -402
Publication date
2004-03-25
Effective date
2004-04-29
FAA docket
Docket No. 2002-NM-120-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Bombardier Model DHC-8-401 and -402 airplanes, that requires modifying the wiring of the rudder trim switch, inspecting all wiring on the back of the aileron/rudder trim control panel for chafing, and replacing any chafed wiring with new wiring. This action is necessary to prevent a short circuit on the aileron/ rudder trim control panel that could cause a runaway condition of the rudder trim actuator, which could result in reduced controllability of the airplane. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown