Quickie Q2 Lite Construction Manual - page 145

Q2 Plans - Chapter 9 - Page 9-05

GLASSING THE AILERON SLOT FOAM CORE SLOTS

.....

The aileron slot foam core inside slots are glass ed with 2 BID 

at 45 degrees to the spanwise direction. (i.e. T.E.). Knife trim to 

the edge of the foam core, as shown on the sketch.

SHOULDER HARNESS INSTALLATION

.....

 Remember those 20 BID plies that you laminated over the two 

SH1's when you performed the "BOTTOM" skin and spar cap lamination? 

Now is the time to drill and tap each SH1 with a 1 x 28 tap for a AN4 

bolt later. The sketch shows the complete assembly. We don't 

recommend actually attaching the shoulder harnesses until after the 

main wing is mounted to the fuselage. Note that both shoulder harness 

straps of each shoulder harness assembly are attached to one bolt, in 

a Y fashion. Also, the 4130 Steel Bushing should be as short as 

possible, to reduce bending loads on the bolt.