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.