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Airworthiness Directives; Aerospace Technologies of Australia Pty Ltd. (Formerly Government Aircraft Factory) Models N22B, N22S, and N24A Airplanes

airworthiness · Rule · Final rule. · Published 1997-05-29 · Effective 1997-07-11 · 62 FR 28997

Document

Document number
97-14077
Federal Register citation
62 FR 28997
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Aerospace Technologies of Australia Pty Ltd. (Formerly Government
Publication date
1997-05-29
Effective date
1997-07-11
FAA docket
Docket No. 95-CE-98-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that applies to Aerospace Technologies of Australia Pty Ltd. (ASTA) Models N22B, N22S, and N24A airplanes. This action requires repetitively inspecting the stub wing upper front spar cap flanges for cracks, and repairing any cracked part. This AD results from fatigue tests that show that the stub wing upper front spar cap flanges could fail over time because of fatigue. The actions specified by this AD are intended to prevent structural failure of the front spar caused by cracks in the stub wing upper front spar cap flanges, which could result in loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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