111.11,
••••••
EXTERIOR PREFUGHT (CON'l}
g. Right Pitot-Static Drain
Va1ves
(2)
- Drain.
Required
only
if
Ei~
moisture in the pitot-static system is known or suspected.
H pitot-static
drain
valves
are opened, ensure that
va1ve
stem returns to the
closed
position.
h.
Oxygen
Discharge
Disc
(if
applicable) - Condition.
e
a.
Copilot's
Windshield
Defog
Outlet
- Clear of obstructions.
b.
Wmg
Inspection Ught
and
Lens
(if
installed) - Condition.
I
c.
Lower
Fuselage Antennas, Rotating Beacon
Light
and
Lens
- Condition.
e
a.
Emergency
Exit
- Secure.
b.
Upper Fuselage Antennas, Rotating Beacon Ught
and
Lens
(on vertical
fin)
- Condition.
•
c.
Right Engine
Inlet
and
Fan - Clear of obstructions and con-
dition.
•
If
fan
is
windmiDing,
stop by pressing on
fan
spinner.
I
Do not attempt to stop
windmilling
by
grabbing
blades.
• The wing,
flight
control surfaces,
and
engine inlet
must be
free
of
frost,
snow,
and
ice.
d.
Fuel Crossover,
Left
Wmg
Stunp, Left Engine
Fuel,
Right
Wmg
Swnp,
and
Right
Engine
Fuel
Drain
Va1ves
- Drain.
"e.
Right
Main
Gear
and
Wheel
WeB
- Hydraulic/fuel leakage
and"
condition;
f.
Right
Main
Gear Landing Ught - Condition.
•
g.
Right
Main
Gear Wheels, Brakes and Ttres - Condition .
e
a.
Aircraft 35-279
and
subsequent, 36-045 and subsequent
and
prior aircraft incorporating
AAK
79-10
or
AMK 83-5,
Stall Ship
(wing
leading
edge)
and Stall Fence - Condition.
b.
Right
Wmg
Access Panels
(Wlderside
of
wing)
- Check for
fuel
leakage.
c.
Right
Fuel
Vent
(Wlderside
of
wing)
-
Plug
removed, clear of
obstructions.
e
a.
•
Aircraft 35-279
and
subsequent, 36-045 and subsequent
and
prior aircraft incorporating
AAK
79-10
or
AMK 83-5,
BOWldary
Layer Energizers - Condition.
• Other aircraft, Vortex Generators - Condition.
b.
Right
Wing
Heat
Scupper
(underside of
wing
forward)
-
Clear
of
obstructions.
FAA
APPROVED
4-30-76 2-3
REISSUED
2-25-81,
CHANGE
10
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