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Learjet 35A - After Takeoff

Learjet 35A
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AFTER
TAKEOff
When
the
fuel quantity gage indicates
600
potmds
or
less remaining in either wing tank, prolonged
nose
up
attitude of 10"
or"
more 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. Reduc-
ing pitch attitude
and
thrust
to
a minimum required
will
prevent
this
situation.
JET
PUMP
Switches should always
be
in
the
ON
po-
sition. However,
at
any time during flight,
if
either
or
both switches are noted
to
be
in
the
Off position, re-
set
to
ON
during steady engine operation
at
80%
Fan
Speed
(Nl),
or
above.
If
taxi
and/or
takeoff were
on
ice, snow,
or
slush,
al-
low
the
wheels
to
spin down for approximately
one
minute prior
to
gear
retraction
to
throw off as
much
slush as possible.
1.
LANDING GEAR Switch -
UP.
Landing
gear
should
be
fully
retracted prior
to
retracting flaps.
2.
Yaw Damper
PHI
or
SEC
ENG Button - Depress.
3.
Flaps -
UP
prior
to
VFE.
4. Anti-Ice Systems - As required.
Even
small
accumulations
of
ice
on
the
wing leading
edge
can cause aerodynamic
stall
prior
to
activation
of
the
stick
shaker
and/or
pusher.
These
ice accumulations
can also cause angle-of-attack indicator information
to
be
tmreliable.
Anti-ice systems should
be
turned
on
prior
to
flight into
visible
moisture
and
Ram
Air Temperature of
lOOC
or
below.
5.
AIR
IGN Switches -
OFF
tmless ambient conditions require igni-
tion
to
remain On.
:5~
During
periods
of heavy precipitation, set AIR IGN
Switches
On
to
prevent possible engine flameout
due
to
large quantities
of
water entering
the
engine.
FAA APPROVED 4-30-76
REISSUED
2-25-81,
CHANGE
10
2-29

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