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Airworthiness Directives; Robert E. Rust Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A Airplanes

airworthiness · Rule · Final rule. · Published 2003-03-18 · Effective 2003-04-25 · 68 FR 12797

Document

Document number
03-6040
Federal Register citation
68 FR 12797
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2003-03-18
Effective date
2003-04-25
FAA docket
Docket No. 2000-CE-66-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to certain Robert E. Rust (R.E. Rust) Models DeHavilland DH.C1 Chipmunk 21, 22, and 22A airplanes. This AD requires you to check the airplane logbook to determine whether certain modifications have been incorporated on the airplane and incorporate the modifications that have not already been accomplished. This AD is the result of the manufacturer performing a design study on the structural integrity of certain parts and reports of service failure of other parts installed on the affected airplanes. The actions specified by this AD are intended to prevent reduced structural integrity in the primary structure of the airplane, which could result in failure of the rudder torque tube, elevator fasteners, and the vertical fin rear spar, or jamming or damage to the elevator. Such failures could lead to loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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