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Airworthiness Directives; Boeing Model 747 Airplanes

airworthiness · Rule · Final rule. · Published 2005-07-11 · Effective 2005-08-15 · 70 FR 39644

Document

Document number
05-13432
Federal Register citation
70 FR 39644
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747
Publication date
2005-07-11
Effective date
2005-08-15
FAA docket
Docket No. FAA-2005-20243

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747-100, -200, -300, and 747SP series airplanes. That AD currently requires certain inspections to find missing or alloy-steel taperlock fasteners (bolts) in the diagonal brace underwing fittings, and corrective actions if necessary. For airplanes with missing or alloy-steel fasteners, that AD also mandates replacement of certain fasteners with new fasteners, which constitutes terminating action for certain inspections. This new AD expands the applicability to include additional airplane models and requires a new inspection to determine fastener material and to find missing or broken fasteners, and related investigative/corrective actions if necessary. This AD is prompted by reports indicating that cracked fasteners made of A286 material were found on airplanes that had only fasteners made of A286 material installed in the area common to the diagonal brace underwing fittings. We are issuing this AD to prevent loss of the underwing fitting load path due to missing or damaged alloy-steel or A286 taperlock fasteners, which could result in separation of the engine and strut from the airplane.

Source

Authoritative
Federal Register document
Machine
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