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© 2007 Stevens AeroModel.
Page 19 of 35
Wing
General Construction Notes: This wing is of typical I-Beam construction with additional torsional strength derived from the
trussed sub ribs. Each component precisely interlocks using the interlocking I-beam construction method developed by
Stevens AeroModel. Throughout construction, we suggest dry-fitting all components, and using minimal amounts of glue
at tab and notch locations only to hold parts together. By dry fitting the wing, each successive component will assist with
pulling the wing square and straight. It is not required to pin the wing to your building surface. In-fact, most of your
building will be done above the board. You will, however, require a flat surface to set the wing on top of for final gluing of
the assembly.
One interesting feature of the SHAFT 25e kit is our incorporation of provisions for quad / split aileron / flaps. In this case
the ailerons are split into two units. This is a popular setup with pilots of “stick” type planes. Just so there is no confusion
we have built in provisions to assist the builder with mounting and rigging this setup beyond showing you where the parts
assemble the builder is on their own with implementing the quad / split aileron / system at the time of publication Stevens
AeroModel does not offer technical assistance for implementing this setup.
1.
Begin construction by assembling major parts from sub assemblies: W1a and W1b to create W1 turbulator with
jig. W2a and W2b to create two (2) W2 turbulators. S1a and two (2) each S1b to create S1 spar webbing, S2a
and S2b to create two (2) spar web caps. T1a, T1b, and T1c to create T1 trailing edge. Assemblies are joined
along the pre-cut scarf and finger joints. Reference parts along a straight edge and bond at the scarf joints
using medium CA glue. See illustration below for parts reference.
2.
Complete the S1 spar web assembly. Locate the previously assembled 3/32” balsa S1 spar web and the 1/16”
plywood S1c spar web doubler. Align S1c on top of the S1 assembly, centering S1c on top of S1 at the wing
center section. Apply liberal amounts of medium CA glue between the parts to laminate the ply spar web
doubler to the spar web assembly. Note: S1c should not cover any of the rib (and sub-rib) notches in S1 and
should end right at the inside edge of the notches for sub rib R2a. See illustrations below.