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Airworthiness Directives; Short Brothers Model SD3-60 Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2005-08-26 · Effective 2005-09-12 · 70 FR 50160

Document

Document number
05-16750
Federal Register citation
70 FR 50160
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Short Brothers Model SD3-60
Publication date
2005-08-26
Effective date
2005-09-12
FAA docket
Docket No. FAA-2005-22168

Abstract

The FAA is adopting a new airworthiness directive (AD) for all Short Brothers Model SD3-60 airplanes. This AD requires an inspection of the rudder for damage, an inspection of the balance weight attachment for discrepancies, an inspection of the rudder horn spar and cleats for cracking and corrosion, and corrective action if necessary. This AD results from events in which fatigue cracking was found on the rudder horn spar. We are issuing this AD to detect and correct cracking and corrosion of the rudder horn spar, which could lead to detachment of the mass balance weight of the rudder. The detachment of the mass balance weight could jam or restrict the movement of the rudder, which could result in reduced controllability of the airplane. Loss of a mass balance weight could also damage other parts of the airplane, which could result in reduced controllability of the airplane, or could result in an injury to a person or damage to property on the ground.

Source

Authoritative
Federal Register document
Machine
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