ENGINE
FAILURE
DURING TAKEOFF
BELOW
VI
SPEED
,------~-------------------------------i
I
1.
Thrust
Levers
-IDLE.
I
:
2.
Wheel
Brakes
- Apply. :
I
3.
Spoilers -
EXT.
I
~--------------------------------------~
4.
Drag Chute or Thrust Reversers
(if
installed) - Deploy,
if
necessary.
ABOVE
VI
SPEED
----------------------------------------,
:
1.
Rudder
and
Ailerons - As
required,
for
directional I
,
control.
:
:
2.
Accelerate
to
VR.
,
:
NOTE~
Directional
control
is
improved
if
the
nose
wheel:
:
-'f
is
kept
on
the
runway
until
VR.
:
,
3.
Rotate
at
VR; Climb
at
V2. :
:
4.
GEAR -
UP,
when positive
rate
of
c6mb
is
established.
,
I
5.
When
clear
of
obstacles,
accelerate
to
V2 +
30
and
retract
:
:
flaps. I
----------------------.----------------~
Lateral control
is
improved with tip tanks empty. If time
permits, it
is recommended that tip
tank
fuel
be
jettisoned.
6.
FUEL
JTSN Switch - ON
Oights
on); Off prior
to
touchdown.
Time
to
reduce aircraft weight from maximum takeoff weight
to
maximum landing weight
is
approximately 40 minutes. Time
to
jet-
tison fuel from tip tanks
is
approximately 5 minutes.
7. Refer
to
ENGINE SHUTDOWN
IN
AJGHT
procedure, Section N,
or
ENGINE ARE - SHUTDOWN procedure, this section.
FAA APPROVED 4-30-76
REISSUED
2-25-81,
CHANGE
12
3-11
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