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Airworthiness Directives; Boeing Model 747 Series Airplanes

airworthiness · Rule · Final rule. · Published 2003-01-03 · Effective 2003-02-07 · 68 FR 257

Document

Document number
03-27
Federal Register citation
68 FR 257
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747 Series
Publication date
2003-01-03
Effective date
2003-02-07
FAA docket
Docket No. 2002-NM-84-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that currently requires a one-time inspection to identify all alloy steel bolts on the body station 1480 bulkhead splice, and corrective action if necessary; and provides for optional terminating action for certain requirements of that AD. This amendment requires accomplishment of the previously optional terminating action. The actions specified by this AD are intended to prevent cracked or broken bolts, which could result in structural damage and rapid depressurization of the airplane. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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