# Airworthiness Directives; Boeing Model 747-200B, 747-200C, 747-200F, 747-300, and 747SR Series Airplanes Equipped With General Electric (GE) CF6-45 or -50 Series Engines
> **Rule** · Final rule. · Published 2005-03-21 · Effective 2005-04-25 · 70 FR 13347
## Document
- **Document number:** 05-5298
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 70 FR 13347
- **Publication date:** 2005-03-21
- **Effective date:** 2005-04-25
- **FAA docket:** Docket No. FAA-2004-19945
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-200B, 747-200C, 747-200F, 747-300, and 747SR series airplanes, equipped with GE CF6-45 or -50 series engines. This AD requires modifying the side cowl assemblies on the engines by replacing existing wear plates with new extended wear plates and installing new stop fittings. This AD is prompted by reports of a gap at the interface of the lower portion of the side cowl and the aft flange of the thrust reverser. We are issuing this AD to prevent an excessive quantity of air from entering the fire zone that surrounds the engine, which, in the event of an engine fire, could result in an inability to control or extinguish the fire.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/03/21/05-5298/airworthiness-directives-boeing-model-747-200b-747-200c-747-200f-747-300-and-747sr-series-airplanes)
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