2002-05-05
FR doc 02-5703 · 67 FR 11220AD 2002-05-05Published 2002-03-13Effective 2002-03-19
Superseded by 2002-24-08
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 incorporate temporary operating limitations into the Limitation Section of the airplane flight manual (AFM) for certain affected airplanes and install a cable clamp external to the cone adapter on the Cirrus…
Full official abstract
This amendment adopts a new airworthiness directive (AD) that applies to certain Cirrus Design Corporation (Cirrus) Models SR20 and SR22 airplanes. This AD requires you to incorporate temporary operating limitations into the Limitation Section of the airplane flight manual (AFM) for certain affected airplanes and install a cable clamp external to the cone adapter on the Cirrus Aircraft Parachute System (CAPS) activation cable for all affected airplanes. The operating limitations will reduce the need to use the CAPS system in a loss of aircraft control emergency situation. The installation will prevent the cable housing from going into the rocket cone and will allow the rocket to fire correctly. This AD is the result of a report from the manufacturer that certain CAPS may not activate in an emergency situation. The actions specified by this AD are intended to initially limit the chance of failure of the CAPS activation system in an emergency situation and eventually eliminate this potential failure. Failure of this system would result in occupant injury and/or loss of life and loss of aircraft.