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AD FAA-2007-28246

Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes

Summary

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.

Directive Details

AD Number

FAA-2007-28246

Document Number

E8-2044

Type

Rule

Publication Date

February 5, 2008

Effective Date

March 11, 2008

Affected Manufacturer

Cirrus Design Corporation Models SR20 and SR22

Criticality

routine

Emergency

No

Docket ID

Docket No. FAA-2007-28246

Topics

Air transportationAircraftAviation safetyIncorporation by referenceSafety

Official Documents

View all ADs for Cirrus Design Corporation Models SR20 and SR22 →

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