2005-17-19
FR doc 05-16980 · 70 FR 51999AD 2005-17-19Published 2005-09-01Effective 2005-10-13
Superseded by 2006-19-10
Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.
Requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats.
Full official abstract
The FAA adopts a new airworthiness directive (AD) for certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD requires you to measure and adjust the crew seat break-over bolts and to replace the crew seat recline locks on both crew seats. This AD results from CDC discovering that the crew seats, under emergency landing dynamic loads, may fold forward at less than the 26 g required by the regulations. We are issuing this AD to prevent the crew seats from folding forward during emergency landing dynamic loads with consequent occupant injury.