← FAA Federal Register actions

Airworthiness Directives; Bombardier, Inc. Airplanes

airworthiness · Rule · Final rule. · Published 2013-10-31 · Effective 2013-12-05 · 78 FR 65198

Document

Document number
2013-25629
Federal Register citation
78 FR 65198
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2013-10-31
Effective date
2013-12-05
FAA docket
Docket No. FAA-2012-0594

Abstract

We are adopting a new airworthiness directive (AD) for certain Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes. This AD was prompted by reports of movement of the rudder pedals being impeded due to corrosion of the trunnion shaft of the rudder feel trim unit (RFTU). This AD requires an inspection to determine if certain RFTUs are installed, an operational check for signs of seizure of affected parts, repetitive lubrication of certain RFTUs, and replacement of the RFTU if necessary. Installing replacement RFTUs having conformal bushings terminates the repetitive lubrication requirements. We are issuing this AD to detect and correct any sign of rough movement or seizure of the trunnion shaft and its bushing, which could cause a rudder control jam or a large and rapid alternating rudder input leading to a structural failure of the vertical fin.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown