← FAA Federal Register actions

Airworthiness Directives; Boeing Model 747 Airplanes

airworthiness · Rule · Final rule. · Published 2009-06-11 · Effective 2009-07-16 · 74 FR 27693

Document

Document number
E9-13406
Federal Register citation
74 FR 27693
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747
Publication date
2009-06-11
Effective date
2009-07-16
FAA docket
Docket No. FAA-2008-0612

Abstract

The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 747 airplanes. This AD requires inspecting for cracks in the left- and right-side Stringer 11 longeron adjacent to the horizontal stabilizer pivot bulkhead, and related investigative and corrective actions if necessary. This AD results from a report of a crack found in the right-side Stringer 11 longeron horizontal flange, adjacent to the horizontal stabilizer pivot bulkhead, during a routine maintenance inspection. We are issuing this AD to detect and correct fatigue cracking of the longeron, which can propagate and cause damage to the adjacent horizontal stabilizer pivot bulkhead. This damage could result in loss of structural integrity and consequent inability of the bulkhead to carry flight loads, which could adversely affect controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown