SECTION 7 CESSNA
AIRPLANE AND SYSTEM DESCRIPTION MODEL 172S NAV III
GFC 700 AFCS
U.S.
WING FLAP SYSTEM
The single slot type wing flaps, refer to Figure 7-3, are extended or
retracted by positioning the wing flap control lever on the instrument
panel to the desired flap deflection position. The wing flap control lever
is moved up or down in a slotted panel that provides mechanical stops
at the 10°, 20° and FULL positions. To change flap setting, the wing flap
control lever is moved to the right to clear mechanical stops at the 10°
and 20° positions. A scale and pointer to the left of the wing flap control
lever indicates flap travel in degrees. The wing flap system circuit is
protected by a 10-ampere circuit breaker, labeled FLAP, on the left side
of the circuit breaker panel.
Figure 7-3*
172SPHBUS-02
7-22
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