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Airworthiness Directives; Air Tractor, Inc. Model AT-602 Airplanes

airworthiness · Rule · Final rule. · Published 2006-11-09 · Effective 2006-12-14 · 71 FR 65719

Document

Document number
E6-18688
Federal Register citation
71 FR 65719
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2006-11-09
Effective date
2006-12-14
FAA docket
Docket No. FAA-2004-20007

Abstract

The FAA adopts a new airworthiness directive (AD) for all Air Tractor, Inc. (Air Tractor) Model AT-602 airplanes. This AD requires you to repetitively inspect (using the eddy current method) the wing center splice joint two outboard fastener holes on both of the wing main spar lower caps for fatigue cracking; repair or replace any wing main spar lower cap where fatigue cracking is found; and report any fatigue cracking found. This AD results from fatigue cracking at the wing center splice joint outboard fastener hole in one of the wing main spar lower caps. We are issuing this AD to detect and correct cracks in the wing main spar lower cap, which could result in failure of the spar cap and lead to wing separation and loss of control of the airplane.

Source

Authoritative
Federal Register document
Machine
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