# Airworthiness Directives; Cessna Aircraft Company Model 525A Airplanes
> **Rule** · Final rule; request for comments. · Published 2009-11-30 · Effective 2009-12-15 · 74 FR 62479
## Document
- **Document number:** E9-28234
- **Category:** airworthiness
- **Manufacturer:** Cessna
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 74 FR 62479
- **Publication date:** 2009-11-30
- **Effective date:** 2009-12-15
- **FAA docket:** Docket No. FAA-2009-1096
## Abstract

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Model 525A airplanes. This AD requires you to repetitively inspect the thrust attenuator paddle assemblies for loose and damaged fasteners and for cracks. This AD also requires you to replace loose or damaged fasteners and replace cracked thrust attenuator paddles found during any inspection. This AD results from reports of fatigue cracks found in thrust attenuator paddles. We are issuing this AD to detect and correct loose and damaged fasteners and cracks in the thrust attenuator paddles, which could result in in- flight departure of the thrust attenuator paddles. This failure could lead to rudder and elevator damage and result in loss of control.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2009/11/30/E9-28234/airworthiness-directives-cessna-aircraft-company-model-525a-airplanes)
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