Washout Angle - Cub Crafters CARBON CUB SS CC11-160 Maintenance Manual

attachment fittings as illustrated in Figure 6.3.4.2. The bubble should be
approximately centered. Check the opposite wing panel in the same manner.
(e) If the dihedral angle is not equal for both wing panels, adjust the threaded fork on
the lower end of the front strut until the dihedral angle is the same. Recheck the
total dihedral and readjust as necessary.
(f) Record the actual results in the aircraft logbook.

(3) WASHOUT ANGLE

(a) Check the washout of each wing by holding a straightedge on the end of a 30-
inch level so that one end of the straightedge protrudes 0.38 (3/8) inches above
the level (See Figure 6.3.4.2
of the full rib next to the outboard end of the aileron. The level end with
straightedge space should fit to the rear of the rib while the other end of the level
should be placed under the front spar.
(b) To obtain the proper washout, adjust the threaded fork at the lower end of the
rear strut at the fuselage end until the bubble is centered.
(c) Repeat on the opposite wing if needed.
(d) Record the actual results in the aircraft logbook.
There should not be more than 15 threads exposed on the lift strut forks.
6.3.4
Page: 8
CUB CRAFTERS, INC.
CC11-160 MAINTENANCE MANUAL
Place this combination along the bottom surface
).
CAUTION
Manual number SSC10000AMM
Date: 09/03/2010