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Airworthiness Directives; Boeing Model 747-100, -100B, -100B SUD, -200B, -200C, -200F, -300, 747SR, and 747SP Series Airplanes Equipped With Pratt & Whitney JT9D-3, -7, -7Q, and -7R4G2 Series Engines

airworthiness · Rule · Final rule. · Published 2004-04-06 · Effective 2004-05-11 · 69 FR 17918

Document

Document number
04-7299
Federal Register citation
69 FR 17918
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-04-06
Effective date
2004-05-11
FAA docket
Docket No. 2002-NM-207-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747-100, -100B, -100B SUD, -200B, - 200C, -200F, -300, 747SR, and 747SP series airplanes equipped with Pratt & Whitney JT9D-3, -7, -7Q, and -7R4G2 series engines. This amendment requires drilling witness holes through the cowl skin at the cowl latch locations in the left-hand side of the cowl panel assembly of each engine. This action is necessary to prevent improper connection of the latch, which could result in separation of a cowl panel from the airplane. Such separation could cause damage to the airplane, consequent rapid depressurization, and hazards to persons or property on the ground. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
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