# Airworthiness Directives; The Boeing Company Airplanes
> **Rule** · Final rule. · Published 2019-12-09 · Effective 2020-01-13 · 84 FR 67179
## Document
- **Document number:** 2019-26400
- **Category:** airworthiness
- **Manufacturer:** The Boeing Company
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 84 FR 67179
- **Publication date:** 2019-12-09
- **Effective date:** 2020-01-13
- **FAA docket:** Docket No. FAA-2019-0437
## Abstract

The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 757-200, -200CB, and -300 series airplanes. This AD was prompted by reports of cracks initiating in the fuselage frame web at body station (STA) 1640. This AD requires, depending on configuration, a general visual inspection for any previous repair, such as any reinforcing repair or local frame replacement repair, repetitive open hole high frequency eddy current (HFEC) inspections for any crack of the fuselage frame web fastener holes, on the left and right side of the airplane, and applicable on- condition actions. The FAA is issuing this AD to address the unsafe condition on these products.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2019/12/09/2019-26400/airworthiness-directives-the-boeing-company-airplanes)
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