# Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
> **Rule** · Final rule. · Published 2008-02-05 · Effective 2008-03-11 · 73 FR 6598
## Document
- **Document number:** E8-2044
- **Category:** airworthiness
- **Manufacturer:** Cirrus Design Corporation Models SR20 and SR22
- **Type:** Rule
- **Action:** Final rule.
- **Citation:** 73 FR 6598
- **Publication date:** 2008-02-05
- **Effective date:** 2008-03-11
- **FAA docket:** Docket No. FAA-2007-28246
## Abstract

We are adopting a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to inspect the rudder, aileron, and rudder-aileron interconnect rigging; correct any out-of-rig condition; replace the attaching hardware for the rudder-aileron interconnect arm; and report any out-of-rig condition found. This AD results from a jamming of the aileron and rudder controls on a Model SR20 airplane, which resulted in loss of rudder and aileron flight controls. We are issuing this AD to prevent the possibility of jamming of the rudder-aileron interconnect system, which may result in loss of rudder and aileron flight controls.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2008/02/05/E8-2044/airworthiness-directives-cirrus-design-corporation-models-sr20-and-sr22-airplanes)
---
*AI Analytics · CC0 1.0*