Airworthiness Directives; Boeing Model 747-400 Series Airplanes Equipped With General Electric Model CF6-80C2 Series Engines
airworthiness · Rule · Final rule. · Published 2003-08-27 · Effective 2003-10-01 · 68 FR 51439
Document
Document number
03-21151
Federal Register citation
68 FR 51439
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747-400 Series
Publication date
2003-08-27
Effective date
2003-10-01
FAA docket
Docket No. 2002-NM-128-AD
Abstract
This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 747-400 series airplanes, that currently requires repetitive tests of the cone brake of the central drive unit (CDU) of the thrust reversers, and corrective actions if necessary. This amendment requires installation of a thrust reverser actuation system (TRAS) lock and various related modifications and installations. Following installation of the TRAS lock, this action also requires repetitive functional tests of the TRAS lock, and corrective action if necessary. These actions are intended to prevent an inadvertent deployment of a thrust reverser during flight, which could result in loss of control of the airplane.