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AD FAA-2007-28956

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

Summary

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.

Directive Details

AD Number

FAA-2007-28956

Document Number

E8-1821

Type

Rule

Publication Date

February 5, 2008

Effective Date

March 11, 2008

Affected Manufacturer

Cessna Aircraft Company Models 525, 525A, and 525B

Criticality

important

Emergency

No

Docket ID

Docket No. FAA-2007-28956

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

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