CESSNA AIRCRAFT
COMPANY
SINGLE ENGINE
STRUCTURAL REPA
IR MANUAL
(2) At WS 100.00:
(a) Hold straightedge parallel to wing station.
(b) Place bolt "A" o
n mark, set protractor head against lower edge of straightedge and verify
bubble in protractor head indicates level.
(3) At WS 207.00:
(a) Remove bolt "A"
from straightedge. Grind another bolt "A" to a dimension of 0.66 inch.
Place this bolt 20.00 inches from bolt "B" and secure to straightedge.
(b) Hold straightedge parallel to wing station and place bolt "A" on mark.
(c) Check to assure
that protractor bubble is still centered. If proper twist is present, the
protractor readings will be the same (parallel).
NOTE: Forward or aft b
olt may be lowered from wing 0.10 inch (maximum) to attain
level indication.
57-22-00 Page 605
© Cessna Aircraft Company Jun 1/2005
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