# Airworthiness Directives; Cessna Aircraft Company Models 525, 525A, and 525B Airplanes
> **Rule** · Final rule. · Published 2008-02-05 · Effective 2008-03-11 · 73 FR 6582
## Document
- **Document number:** E8-1821
- **Category:** airworthiness
- **Manufacturer:** Cessna
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 73 FR 6582
- **Publication date:** 2008-02-05
- **Effective date:** 2008-03-11
- **FAA docket:** Docket No. FAA-2007-28956
## Abstract

We are adopting a new airworthiness directive (AD) for certain Cessna Aircraft Company (Cessna) Models 525, 525A, and 525B airplanes. This AD requires you to inspect the lower wing skin structure, forward wing spar, lower fuselage skin, fairings, and the external fairing frames for corrosion; repair any damage found; apply a corrosion inhibitive sealant to the fuselage fairings before reinstalling; and disable the cockpit mounted pilot relief tube. This AD results from leaking of the cockpit mounted pilot relief tube, which caused corrosion of the airplane structure. We are issuing this AD to detect and correct any damage from corrosion of the airplane structure. Corrosion of the airplane structure could cause structural degradation and lead to structural failure of the airplane with consequent loss of control.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2008/02/05/E8-1821/airworthiness-directives-cessna-aircraft-company-models-525-525a-and-525b-airplanes)
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