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Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

airworthiness · Rule · Final rule. · Published 2006-03-30 · Effective 2006-05-11 · 71 FR 16027

Document

Document number
06-2982
Federal Register citation
71 FR 16027
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cirrus Design Corporation Models SR20 and SR22
Publication date
2006-03-30
Effective date
2006-05-11
FAA docket
Docket No. FAA-2005-23023

Abstract

The FAA adopts a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to inspect the fuel line and wire bundles for any chafing damage; replace any damaged fuel line and repair any damaged wires or sheathing of the wire harness if any chafing damage is found; and install (to prevent any chafing damage to the fuel line and wire bundles) the forward loop clamp, fuel line shield, aft loop clamp, and anti-chafe tubing. This AD results from reports of fuel line leaks resulting from wire chafing on the fuel lines. We are issuing this AD to detect, correct, and prevent damage to the fuel line and wire bundles, which could result in fuel leaks. This failure could lead to unsafe fuel vapor within the cockpit and possible fire.

Source

Authoritative
Federal Register document
Machine
JSON-LD · Markdown