# Airworthiness Directives; the Boeing Company Airplanes
> **Rule** · Final rule. · Published 2013-09-30 · Effective 2013-11-04 · 78 FR 59801
## Document
- **Document number:** 2013-22676
- **Category:** airworthiness
- **Manufacturer:** the Boeing Company
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 78 FR 59801
- **Publication date:** 2013-09-30
- **Effective date:** 2013-11-04
- **FAA docket:** Docket No. FAA-2012-0723
## Abstract

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes. This AD was prompted by a report of cracks found in the skin at body station (STA) 540 just below stringer S-22L on a Model 737-700 series airplane. This AD requires repetitive detailed and high frequency eddy current inspections for cracking of the skin around the eight fasteners common to the ends of the STA 540 bulkhead chords between stringers S-22 and S-23, left and right sides; and corrective actions and preventive modification if necessary. We are issuing this AD to detect and correct fatigue cracking in the skin, which can result in rapid decompression of the cabin.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2013/09/30/2013-22676/airworthiness-directives-the-boeing-company-airplanes)
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