# Airworthiness Directives; Boeing Model 747 Series Airplanes
> **Rule** · Final rule. · Published 2000-12-04 · Effective 2001-01-08 · 65 FR 75582
## Document
- **Document number:** 00-30399
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 747 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 75582
- **Publication date:** 2000-12-04
- **Effective date:** 2001-01-08
- **FAA docket:** Docket No. 99-NM-377-AD
## Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that requires inspections to detect cracking of the frame web, doubler, and inner chord of the forward edge frame of main entry door number 1, and various follow-on actions. This amendment is prompted by reports of cracking in the frame web, doubler, inner chord, and strap of the forward edge frame of main entry door number 1. The actions specified by this AD are intended to prevent cracks in the frame web and doubler of the forward edge frame of main entry door number 1, which could result in inability of the edge frame to react door stop loads, and consequent rapid depressurization of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/12/04/00-30399/airworthiness-directives-boeing-model-747-series-airplanes)
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