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SECTION 7 CESSNA
f=
AIRPLANE AND SYSTEMS DESCRIPTION MODEL 2088 (675 SHP)
WING
FLAP
SYSTEM
(Continued)
A standby system can be used to operate the flaps in the event the
..
primary system should malfunction. On earlier airplanes, the standby
system consists of a standby motor, a guarded standby flap motor
,
..
switch and an unguarded standby flap motor upldown switch located
on the overhead panel. On later airplanes, both switches have guards
which are
safetied in the closed position, with breakable copper wire.
The guarded standby flap motor switch has NORM and
STBY
positions. The guarded NORM position of the switch permits operation
of the flaps using the control pedestal mounted selector; the
STBY
position is used to disable the dynamic braking of the primary flap
motor when the standby flap motor system is operated.
Figure
7-8.
Wing Flap System
(Continued Next Page)
1
7-28
U.S.
Revision
23
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