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Airworthiness Directives; Boeing Model 747-100, -200B, -200C, and -200F Series Airplanes

airworthiness · Rule · Final rule. · Published 2007-08-28 · Effective 2007-10-02 · 72 FR 49161

Document

Document number
E7-16420
Federal Register citation
72 FR 49161
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2007-08-28
Effective date
2007-10-02
FAA docket
Docket No. FAA-2007-28257

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100, -200B, -200C, and -200F series airplanes. This AD requires performing repetitive inspections for cracks in the fuselage skin at the cutout of the bulk cargo door light, and corrective actions if necessary. This AD also provides terminating action for airplanes with a certain type of damage. This AD results from a report of a 2-inch crack through the fuselage skin and internal bonded doubler at the cutout of the bulk cargo door light. We are issuing this AD to detect and correct cracks in the fuselage skin at the cutout of the bulk cargo door light, which could result in reduced structural integrity of the fuselage at the bulk cargo door and consequent rapid decompression of the fuselage.

Source

Authoritative
Federal Register document
Machine
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