Beechcraft C23 SUNDOWNER 180 Pilot Operating Handbook page 222

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2. R/GHT
FUSENGE:
a.
Static
Pressure
Button
-
UNOBSTRUCTED
b.
Emergency
Locator
Transmitter
-
ARMED
3.
EMPENNAGE:
a.
Control Surfaces
-
CHECK
b. Tie
Down
-
REMOVE
c.
Position
Light
-
CHECK
4. LEFT
FUSELAGE:
a.
Static
Pressure
Button
-
UNOBSTRUCTED
b. All Antennas
-
CHECK
c.
Baggage
Door
-
CHECK
5. LEFT WING
TRAILING
EDGE:
a.
Flap
-
CHECK
b.
Fuel
Vent
Line
-
UNOBSTRUCTED
c.
Aileron
-
CHECK
d.
Wing Tip
-
CHECK
e.
Position
Light
-
CHECK
6. LEFT
WING
LEADING
EDGE:
a.
Pitot
Tube
-
CHECK,
(Remove Cover)
b.
Landing
Light
-
CHECK
c.
Tie
Down
and Chocks
-
REMOVE
d.
Stall Warning
-
CHECK
for
movement
of
vane
e.
Fuel
Tank
-
CHECK O.UANTITY;
Filler
Cap
SECURE.
7. LEFT
LANDING
GEAR:
a. Tire and Nose Gear
-
CHECK
b.
-
Fuel
Sump
-
DRAIN
8.
NOSE SECTION:
a.
Left
Cowl
-
SECURE
b.
Induction
Air
Intake
-
CLEAR
c.
Propeller
-
CHECK,
General
Condition,
Nicks,
etc.
d.
Tire
and
Nose Gear
-
CHECK
FAA Approved
Revised:
February
1979
2 of 4
P/N 169-590008-19

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