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Airworthiness Directives; Boeing Model 747 Series Airplanes

airworthiness · Rule · Final rule. · Published 2000-05-01 · Effective 2000-06-05 · 65 FR 25281

Document

Document number
00-10285
Federal Register citation
65 FR 25281
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747 Series
Publication date
2000-05-01
Effective date
2000-06-05
FAA docket
Docket No. 99-NM-231-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 747 series airplanes, that requires repetitive inspections to detect cracking of the forward and aft inner chords and the splice fitting of the forward inner chord of the station 2598 bulkhead, and repair, if necessary. This amendment is prompted by reports of fatigue cracking found in those areas. The actions specified by this AD are intended to detect and correct such cracking, which could result in reduced structural capability of the bulkhead and the inability of the structure to carry horizontal stabilizer flight loads.

Source

Authoritative
Federal Register document
Machine
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