Washout Angle - Cub Crafters CC18-180 Maintenance Manual

illustrated in Figure 57-00-2. 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 log book.

(3) WASHOUT ANGLE

(a) Check the washout of each wing by holding a straight-edge on the end of a 30-inch
level so that one end of the straight-edge protrudes 0.38 (3/8) inches above the
level (See Figure 57-00-2
full rib next to the outboard end of the aileron. The level end with straight-edge
space should be 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 log book.
There should not be more than 15 threads exposed on the lift strut forks.
Manual number TC10000AMM
Date: 04/15/05
CUB CRAFTERS, INC.
CC18-180 MAINTENANCE MANUAL
Place this combination along the bottom surface of the
).
CAUTION
57-00
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