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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.

Source

Authoritative
Federal Register document
Machine
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