While designing pitot/static system, I notice that the Dynon AoA/Pitot probe does not have a static port. Most other probes come with Pitot and static pressures. Is it a common practice to put the static ports at the sides of a fuselage? What are the advantages/disadvantages of the two different approaches ( [Pitot/static in a single probe] vs [Pitot probe + static port at fuselage sides] ) ?