rcarsey
Well Known Member
new revision of Section 38: Airframe Assembly has been released.
http://www.vansaircraft.com/public/service-rv12iS.htm
REVISION DESCRIPTION / NEW DOCUMENTATION:
http://www.vansaircraft.com/public/service-rv12iS.htm
REVISION DESCRIPTION / NEW DOCUMENTATION:
- Page 38iS/U-02 REV 1: In Figure 2 detail view, added ?NAS1149F0332P?.
Thin washer prevents premature bottoming of nut. - Page 38iS/U-05 REV 1: Step 5, ?Use shims and clamps to secure the left and right flaperons in a trailing edge down position as
shown in Figure 3. The goal is to have a 1/8 in. [3.2 mm] offset at the trailing edge.? was ?Use shims and clamps at the trailing edge
to lock both the left and right flaperons in a slightly downward position as shown in Figure 3.?
Updated Figure 3 to show smaller shims (that don?t interfere with rivet heads) and to show clamp at the trailing edge. - Page 38iS/U-09 REV 1: Added new Step 1, ?Match-Drill #30 the two holes in each F-01207C-L-1 & -R-1 Baggage Bulkhead into the
F-1284-L & -R Shear Clips. See Figure 1.?. Renumbered subsequent steps.
Shear clips are supplied without holes in forward flanges. - Page 38iS/U-17 REV 1: In Step 1, ??WD-01207-1 and WD-01208-1?? was ??WD-1207 and WD-1208??.
Updated Figure 1 to show new stabilator structure (reference SB 18-02-02). - Page 38iS/U-18 REV 1: Added new Step 8, ?Fabricate the T-01236 Fuel Overflow Sleeve by cutting a 1 in. [25.4 mm] piece of PT
1/4IDX3/8ODX4? tubing.?. Renumbered subsequent step. - Page 38iS/U-21 REV 1: In Step 2, added ?These seat cushions have been designed to suit most pilots. For adequate clearance to
the canopy, very tall pilots may need to remove foam from the seat bottom cushion or source a custom seat cushion.?.