Cessna 402C Pilot Operating Handbook page 219

SECTION 7
AIRPLANE & SYSTEMS DESCRIPTIONS
The minimum turning distance is presented in Figure 7-11. Always use as.
large a radius of turn as is practical. Turning tighter than necessary
requires excessive braking on the inboard wheel which decreases the tire
1
ife.
...--------NOTE-------.....,
Minimum turning dtstance is effected with inboard
wheel brake locked, full rudder and differential
power.
MINIMUM TURNING DISTANCE
' "
L_'-='- "'-
I
I
52104008
-
Figure 7-11
WING FLAPS SYSTEM
The wing flaps, see Figure 7-12, are of the split flap design. Each
wing flap (two per side) is attached to the rear wing main spar lower
._~ su rface and is actua ted by two pus h-pu 11 rods attached to bell cranks in the
wing. The be11cranks in each wing are ganged together with push-pull rods.
Each inboard push-pull rod is attached to a cable which is actuated by an
electric motor with reduction gear in the fuselage center section.
The electric flap motor is controlled by the wing flap position switch,
see Figure 7-1, in the cockpit. This switch incorporates a preselect
1 November 1979
Revision 2 - 3 Aug 1981
7-15