# Airworthiness Directives; Boeing Model 727 Airplanes
> **Rule** · Final rule. · Published 2005-03-11 · Effective 2005-04-15 · 70 FR 12120
## Document
- **Document number:** 05-4826
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 727
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 70 FR 12120
- **Publication date:** 2005-03-11
- **Effective date:** 2005-04-15
- **FAA docket:** Docket No. FAA-2004-19530
## Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to certain Boeing Model 727 airplanes. That AD currently requires repetitive detailed inspections to detect cracking, corrosion, and existing stop-drilled repairs of cracking in the upper chord of the rear spar of the wing; and repair if necessary. This new AD requires new repetitive inspections to detect cracks, corrosion, minor surface defects, and existing stop-drilled repairs of cracks in the upper and lower chords of the front and rear spars of the wing; and repair if necessary. This AD is prompted by our determination that further rulemaking action is necessary to require additional actions specified in the referenced service bulletin. We are issuing this AD to prevent structural failure of the wing and fuel leaks in the airplane due to stress corrosion cracking of the wing spar chords.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2005/03/11/05-4826/airworthiness-directives-boeing-model-727-airplanes)
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