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this document is unlimited with the following exceptions: (1)
redistribution is allowed only if full attribution to the original
author(s) is preserved, and all changes are approved by the author(s);
(2) this document MAY NOT be reproduced in any form for profit of any
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This document provides informal advice. Use of the information
is at the owner's discretion only. In no way do the authors of this
document warrant, implicitly or otherwise, any information contained
herein. Always follow
manufacturer's recommendations when installing or removing, or
authorizing a certified mechanic to install or remove, any part from
In no way do the author(s) of this document support any
deviation from published documentation from Raytheon/Beechcraft, the
Federal Aviation Administration, or any manufacturer of airframe parts,
avionics, instruments, or any other part used in the manufacture or repair of an aircraft.