NACA oil scoop was reinforced with 2-ply BID top and bottom of scoop. Additional strengtheners glassed to area of gear bulkhead around the gear pulley openings.
Rudder cable see-saw installed on canard bulkhead, and battery shelf positioned and clecoed in place. NLG actuator bolted into place on fuselage centerline.
Heat duct (pre-fab part) sawed in half and internal flange fabricated by using waxed Al tape on one half and bonding 2-ply BID across seam.
Iteratively cut lower cowling along cut line aft of firewall, holding it in place with hot glue and wooden sticks. Added a 2-ply BID layup to strengthen joint between firewall and fuselage in region of cowl flange.
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