# Airworthiness Directives; Boeing Model 767 Airplanes
> **Rule** · Final rule. · Published 2006-05-03 · Effective 2006-06-07 · 71 FR 25928
## Document
- **Document number:** 06-4055
- **Category:** airworthiness
- **Manufacturer:** Boeing Model 767
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 71 FR 25928
- **Publication date:** 2006-05-03
- **Effective date:** 2006-06-07
- **FAA docket:** Docket No. FAA-2006-23762
## Abstract

The FAA is adopting a new airworthiness directive (AD) for all Boeing Model 767 airplanes. This AD requires repetitive inspections for cracking in the skin, the bulkhead outer chord, and the strap of the bulkhead outer chord at station (STA) 1725.5; and repair if necessary. This AD also provides for repairs, which are optional for airplanes on which no cracking is found, that terminate certain inspections. This AD results from reports of cracking in the skin panel common to stringer 7R and aft of the STA 1725.5 butt splice, and in the strap of the bulkhead outer chord at STA 1725.5. We are issuing this AD to detect and correct cracking in the skin, the bulkhead outer chord, or the strap of the bulkhead outer chord in this area, which could progress into surrounding areas and result in reduced structural integrity of the support structure for the vertical or horizontal stabilizer and subsequent loss of control of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2006/05/03/06-4055/airworthiness-directives-boeing-model-767-airplanes)
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