← FAA Federal Register actions

Airworthiness Directives; Boeing Model 747 Airplanes

airworthiness · Rule · Final rule. · Published 2006-09-28 · Effective 2006-11-02 · 71 FR 56861

Document

Document number
06-8227
Federal Register citation
71 FR 56861
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747
Publication date
2006-09-28
Effective date
2006-11-02
FAA docket
Docket No. FAA-2006-24865

Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 747 airplanes. That AD currently requires inspections to detect disbonding, corrosion, and cracking at the longitudinal rows of fasteners in the bonded skin panels in section 41 of the fuselage, and repair, if necessary. This new AD adds airplanes to the applicability, and requires new inspections of airplanes that may have Alodine-coated rivets installed. This AD results from a report of cracking discovered in a skin lap joint that was previously inspected using the eddy current method. We are issuing this AD to prevent rapid decompression of the airplane due to disbonding and subsequent cracking of the skin panels.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown