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1
ENGINE
FAILURE
(CONT)
IN
FUGHT
1. Control Wheel Master Switch
(MSW)
- Depress
and
release.
Yaw
damper
and autopilot
will
disengage.
2. Rudder and Ailerons -
As
required, for directional control.
3.
Thrust Lever (operative engine) - Increase
as
required.
4.
ENG SYNC Switch - OFF.
5.
Rudder Trim -
As
required.
6.
Yaw
Damper
- Engage.
7. Autopilot - As desired.
8.
Refer
to
ENGINE SHUTDOWN
IN
FUGHT procedure, Section
IV.
DURING
APPROACH
,~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~~f
,
1.
Control Wheel Master Switch
(MSW)
-
Depress
and'
, release.
Yaw
damper
and
autopilot will disengage. :
:
2.
Thrust
Lever (operative engine) - Increase
as
required. ,
:
3.
Flaps - 20° maximum. :
,
-~
H aircraft
is
configured with landing flaps
(ON):
:
~r
when engine failure occurs,
thrust
increase
(on.
, operative engine)
and
flap retraction
to
20°:
: should be
near
simultaneous actions. ,
:
4.
Airspeed -
VREF
+
10
minimum. :
.~~~~~~~~~~-~----------.---------------~
5.
Rudder Trim -
As
required.
-_NOTE
~
During a coupled approach,
full
rudder trim may
be
re-
r quired with
an
actual engine failure. Use rudder pedal
force
as
necessary
to
maintain slip indicator ball
centered.
6.
Yaw
Damper
- Engage.
7. Autopilot - As desired.
8.
Refer
to
either of the
foUowing
procedures as applicable:
3-12
• SINGLE-ENGINE LANDING. Section
IV.
•
GO
AROUND, Section
II,
and ENGINE SHUTDOWN
IN
FUGHT,
Section
IV.
FAA
APPROVED
4-30-76
REISSUED
2-25-81,
CHANGE
12
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