The potential exists for the front pilot and co-pilot window heat wires to arc to ground if improperly installed during the re-installation of the overhead panel.
The landing gear is very susceptible to corrosion and even though steps may have been taken to lessen the effects, some corrosion still forms.
If you operate TFE731-3, -3A, -3AR, -3R, -3B, and -3BR engines installed on one of the following aircraft models, AD 2005-05-15 applies to you.
The Customer Bulletin (CB) requires the Securaplane Service Bulletin (SB) 100-0302-24-139 be complied with at the next internal battery change (a 48-month requirement).
This Airworthiness Directive (AD) requires that Service Bulletin (SB) 100-31-284 be complied with, within 250 hours of the effective date of the AD.
Ever given much thought to your avionics / customized wiring prints? Probably not, unless something is broke or during an upgrade of some sort.