Airworthiness Directives; Air Tractor, Inc. Models AT-802 and AT-802A Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2006-04-19 · Effective 2006-04-21 · 71 FR 19994
Document
Document number
06-3613
Federal Register citation
71 FR 19994
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2006-04-19
Effective date
2006-04-21
FAA docket
Docket No. FAA-2005-20591
Abstract
The FAA is adopting a new airworthiness directive (AD) for all Air Tractor, Inc. (Air Tractor) Models AT-802 and AT-802A airplanes. This AD requires you to repetitively inspect (using the eddy current method) the two outboard fastener holes in both of the wing main spar lower caps at the center splice joint for cracks and repair or replace any cracked spar cap. This AD results from in-service fatigue cracking of the wing main spar lower cap at the center splice joint outboard fastener hole at hours time-in-service below the safe life limit established for these airplanes in AD 2002-11-05. We are issuing this AD to detect and correct cracks in the wing main spar lower cap at the center splice joint, which could result in failure of the spar cap and lead to wing separation and loss of control of the airplane.