Airworthiness Directives; Cirrus Design Corporation Models SR20 and SR22 Airplanes
airworthiness · Rule · Final rule. · Published 2006-09-19 · Effective 2006-10-24 · 71 FR 54755
Document
Document number
E6-15432
Federal Register citation
71 FR 54755
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Cirrus Design Corporation Models SR20 and SR22
Publication date
2006-09-19
Effective date
2006-10-24
FAA docket
Docket No. FAA-2006-24254
Abstract
We are adopting a new airworthiness directive (AD) that supersedes AD 2005-17-19, which applies to certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. AD 2005-17-19 currently requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats. Since we issued AD 2005-17-19, CDC developed new crew seat break-over pins to replace the old crew seat break-over bolts. Consequently, this AD retains the action from AD 2005-17-19 of replacing the crew seat recline locks on both seats and adds the action of replacing the crew seat break-over bolts with the new crew seat break-over pins on both seats. We are issuing this AD to prevent the crew seats from folding forward during emergency landing dynamic loads with consequent occupant injury.