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Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135BJ, -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2005-12-08 · Effective 2005-12-23 · 70 FR 72902

Document

Document number
05-23656
Federal Register citation
70 FR 72902
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2005-12-08
Effective date
2005-12-23
FAA docket
Docket No. FAA-2005-23187

Abstract

The FAA is adopting a new airworthiness directive (AD) for all EMBRAER Model EMB-135BJ, -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes. This AD requires reviewing the airplane maintenance records for recent reports of vibration from the tail section or rudder pedals. This AD also requires repetitively inspecting the skin, attachment fittings, and control rods of rudder II to detect cracking, loose parts, wear, or damage; and related investigative/corrective actions if necessary. This AD results from reports of rudder vibration due to wear. We are issuing this AD to prevent failure of multiple hinge fittings, which could result in severe vibration, and to prevent failure of the rudder control rods, which could result in jamming of the rudder II; and possible structural failure and reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
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