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Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

airworthiness · Rule · Final rule. · Published 2002-12-10 · Effective 2003-01-24 · 67 FR 75809

Document

Document number
02-30685
Federal Register citation
67 FR 75809
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cirrus Design Corporation Models SR20 and SR22
Publication date
2002-12-10
Effective date
2003-01-24
FAA docket
Docket No. 2002-CE-31-AD

Abstract

This amendment supersedes Airworthiness Directive (AD) 2002- 05-05, which currently applies to certain Cirrus Design Corporation (Cirrus) Models SR20 and SR22 airplanes. AD 2002-05-05 currently requires you to incorporate temporary operating limitations into the Limitation Section of the airplane flight manual (AFM) for certain affected airplanes and install a cable clamp external to the cone adapter on the Cirrus Airplane Parachute System (CAPS) activation cable for all affected airplanes. AD 2002-05-05 resulted from a report from the manufacturer that certain CAPS may not activate in an emergency situation. This AD is the result of the manufacturer redesigning the CAPS activation system. This AD requires you to modify the CAPS activation system. The actions specified by this AD are intended to prevent failure of the CAPS activation system in an emergency situation. Failure of this system could result in occupant injury and/ or loss of life and loss of aircraft.

Source

Authoritative
Federal Register document
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