# Airworthiness Directives; BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ Airplanes
> **Rule** · Final rule. · Published 2009-06-19 · Effective 2009-07-24 · 74 FR 29123
## Document
- **Document number:** E9-13567
- **Category:** airworthiness
- **Manufacturer:** BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 74 FR 29123
- **Publication date:** 2009-06-19
- **Effective date:** 2009-07-24
- **FAA docket:** Docket No. FAA-2009-0133
## Abstract

The FAA is superseding an existing airworthiness directive (AD), which applies to all BAE Systems (Operations) Limited Model BAe 146 and Avro 146-RJ airplanes. That AD currently requires repetitive inspections for corrosion of frames 15, 18, 41, and 43 and applicable related investigative and corrective actions. The existing AD also provides an optional action that would extend the repetitive inspection interval. This new AD also requires a high frequency eddy current inspection for corrosion of the outer frame flanges and door hinge bosses of frames 15, 18, 41, and 43. This AD results from a report indicating that corrosion has been detected in the outer frame flanges and door hinge bosses during scheduled maintenance. We are issuing this AD to prevent reduced structural integrity of the airplane.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2009/06/19/E9-13567/airworthiness-directives-bae-systems-operations-limited-model-bae-146-and-avro-146-rj-airplanes)
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