Airworthiness Directives; Air Tractor, Inc. Airplanes
airworthiness · Rule · Final rule. · Published 2014-08-25 · Effective 2014-09-29 · 79 FR 50542
Document
Document number
2014-20098
Federal Register citation
79 FR 50542
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2014-08-25
Effective date
2014-09-29
FAA docket
Docket No. FAA-2014-0077
Abstract
We are superseding Airworthiness Directive (AD) 2010-17-18 R1, which applies to certain Air Tractor, Inc. Models AT-802 and AT-802A airplanes. AD 2010-17-18 R1 required repetitively inspecting (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; repairing or replacing any cracked spar; changing the safe life for certain serial number ranges; and sending the inspection results, only if cracks are found, to the FAA. This new AD retains all actions of AD 2010-17-18 R1 and expands the applicability to include all serial numbers regardless of configuration or operational use. This AD was prompted by our determination that the safe life for the wing main spar lower caps should apply to all Models AT-802 and AT-802A airplanes regardless of configuration or operational use. We are issuing this AD to correct the unsafe condition on these products.