# Airworthiness Directives; Boeing Model 727 Series Airplanes
> **Rule** · Final rule. · Published 2000-07-13 · Effective 2000-08-17 · 65 FR 43228
## Document
- **Document number:** 00-17296
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 727 Series
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 65 FR 43228
- **Publication date:** 2000-07-13
- **Effective date:** 2000-08-17
- **FAA docket:** Docket No. 99-NM-75-AD
## Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 727 series airplanes, that currently requires repetitive inspections to detect cracking of the rear spar web or fuel leakage of the wing center section, and repair, if necessary. That action also provides for an optional modification of the rear spar web that constitutes terminating action for the repetitive inspections. This amendment requires accomplishment of the previously optional terminating action. The actions specified by this AD are intended to prevent cracking of the rear spar web, which could permit fuel leakage into the airflow multiplier, and could result in an electrical short that could cause a fire.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2000/07/13/00-17296/airworthiness-directives-boeing-model-727-series-airplanes)
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