# Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
> **Rule** · Final rule. · Published 2002-12-10 · Effective 2003-01-24 · 67 FR 75809
## Document
- **Document number:** 02-30685
- **Category:** airworthiness
- **Manufacturer:** Cirrus Design Corporation Models SR20 and SR22
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 67 FR 75809
- **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
- [Federal Register document](https://www.federalregister.gov/documents/2002/12/10/02-30685/airworthiness-directives-cirrus-design-corporation-models-sr20-and-sr22-airplanes)
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