Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2001-12-11 · Effective 2001-12-17 · 66 FR 63913
Document
Document number
01-30423
Federal Register citation
66 FR 63913
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Cirrus Design Corporation Models SR20 and SR22
Publication date
2001-12-11
Effective date
2001-12-17
FAA docket
Docket No. 2001-CE-46-AD
Abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to inspect one time for understrength rivets on the elevator torque tube and rudder hinge and replace any understrength rivets. This AD is the result of CDC notifying FAA that understrength rivets were mixed in production supplies. The actions specified by this AD are intended to detect and replace understrength rivets in the elevator and rudder, which could result in failure of the control surfaces. Such failure could lead to a loss of control of the airplane in flight.