Most of this chapter was done as part of our Fast Build Fuselage. In fact, the bolt hole in the nose that is referenced in this chapter for all of the measurements was already removed and the nose closed up prior to taking delivery. Of note, the canard bulkhead is 39 1/2″ aft, the instrument panel is mounted 59″ aft, and the firewall is 157 1/2″ aft. The gear bulkhead is then 7 1/4″ forward of the firewall.
The only thing referenced in this section that was not completed was the mounting of some bubble levels along an across the fuselage to verify that level is maintained while working in it.
Posted By: Brett FerrellMonday June 10th, 2002 at 7:30 PM