# Airworthiness Directives; Boeing Model 747-400 Series Airplanes Equipped With General Electric Model CF6-80C2 Series Engines
> **Rule** · Final rule. · Published 2003-08-27 · Effective 2003-10-01 · 68 FR 51439
## Document
- **Document number:** 03-21151
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 747-400 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 68 FR 51439
- **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.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2003/08/27/03-21151/airworthiness-directives-boeing-model-747-400-series-airplanes-equipped-with-general-electric-model)
---
*AI Analytics · CC0 1.0*