← FAA Federal Register actions

Airworthiness Directives; Cessna Aircraft Company Models 525, 525A, and 525B Airplanes

airworthiness · Rule · Final rule. · Published 2008-02-05 · Effective 2008-03-11 · 73 FR 6582

Document

Document number
E8-1821
Federal Register citation
73 FR 6582
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cessna
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

Authoritative
Federal Register document
Machine
JSON-LD · Markdown