111.111
••••••
GO AROUND
When the
fuel
quantity gage indicates
600
pounds or
less
remaining in either
wing
tank, prolonged nose-up
attitude of
100
or tnore
may
cause
fuel
to be trapped
in
the aft area of the wing tank outboard of the wheel
well.
Fuel
starvation and engine flameout may
occur.
For go-around conditions with low
fuel,
on
first
steady
indication
by the
LOW
FUEL warning
light,
reduce
climb
attitude and thrust to a minimum required.
1. Autopilot - Disengaged.
2. Thrust Levers - Set to takeoff power or
as
required.
3. SPOll..ER Switch - Check
RET.
I
4. Raps - 20°. I
5.
LANDING
GEAR
Switch - UP after positive rate of climb
is
established.
6. Climb
at
Approach
Climb
Speed.
7. When clear of obstacles, accelerate to
VREF
+30
and retract
flaps.
1. SPOll..ER Switch -
EXT
after touchdown.
~
If,
upon touchdown, one or more
ANTI-SKID
GEN
ICAU110N
I,
lights
come on, anti-skid protection for the associated
wheel
is inoperative and has reverted to manual brake
control.
2. Brakes -
As
required.
~
If
not already operating,
do
not
tum
on
cooling
system
ICAUTION
"
during
landing with
anti-skid
system operating.
Initial
voltage
drop
may
cause
false
signals in the anti-skid sys-
tem and dump brake pressure for 2 to 3 seconds.
3. Thrust Reversers or Drag Chute
(if
installed)
-
As
desired.
I
4. Nose Wheel Steering -
As
required
below
45
knots.
During
moderate to
heavy
braking action on patchy
snow or ice,
avoid
use of nose wheel steering above
10
knots.
FAA
APPROVED
4-30-76
REISSUED
2-25-81,
CHANGE
10
2-35
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