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Airworthiness Directives; Bombardier Inc. Model Otter DHC-3 Airplanes

airworthiness · Rule · Final rule. · Published 2004-03-01 · Effective 2004-04-20 · 69 FR 9523

Document

Document number
04-4373
Federal Register citation
69 FR 9523
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Bombardier Inc. Model Otter DHC-3
Publication date
2004-03-01
Effective date
2004-04-20
FAA docket
Docket No. 2000-CE-73-AD

Abstract

The FAA adopts a new airworthiness directive (AD) for certain Bombardier Inc. (formerly deHavilland Inc.) Model Otter DHC-3 airplanes that have turbine engines installed per one of three supplemental type certificates (STC). This AD prohibits you from operating any affected airplane with these engine and propeller configurations unless a new STC for an elevator servo-tab with a redundant control linkage is installed. This AD is the result of reports of the control rod to the elevator servo-tab system detaching from the elevator servo-tab, which caused the elevator servo-tab to flutter on airplanes with a turbine engine installed. We are issuing this AD to prevent a single failure of the elevator servo-tab system, which could cause severe tab flutter. This failure could lead to possible loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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