Textron Cessna Skyhawk SP - Crosswind Component

SECTION 5 CESSNA
PERFORMANCE MODEL 172S NAV III
GFC 700 AFCS
U.S.
CROSSWIND COMPONENT
MAXIMUM DEMONSTRATED CROSSWIND VELOCITY
Takeoff, Flaps UP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 KNOTS
Takeoff, Flaps 10° . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 KNOTS
Landing, Flaps 10°. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 KNOTS
Landing, Flaps FULL . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15 KNOTS
Figure 5-4
172SPHBUS-02
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