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Cessna 402C - Page 54

Cessna 402C
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(AMPLIFIED
PROCEDURES)
SECTION
3
EMERGENCY
PROCEDURES
ADJUST
bank toward
operative
engine with
approxi-
mately
1/2
ball
slip
indicated
on
the
turn
and bank
indicator.
Cowl
Flap
-
CLOSE
(Inoperative
Engine).
Inoperative
Engine -
SECURE
as
follows:
a.
Fuel
Selector
-
OFF
(Feel
For
Detent).
b.
Auxiliary
Fuel
Pump
-
OFF.
c.
Magneto Switches -
OFF.
d.
Alternator
Switch
-
OFF.
As
Soon
as
Practical
-
LAND.
Cl
imb
at
One
Engine
Inoperative
Best Rate-of-Cl
imb
Speed - 104
KIAS.
9.
Trim Tabs
8.
10.
II.
12.
Upon
engine
failure
after
reaching
95
KIAS
on
takeoff,
the
multi-engine
pilot
has a
significant
advantage
over
a
single-engine
pilot,
for
he
has a
choice
of
stopping
or
continuing
the
takeoff.
This
would
be
similar
to
the
choice
facing
a
single-engine
pilot
who
has suddenly
lost
slightly
more
than
half
of
his
takeoff
power.
In
this
situation,
the
single·engine
pilot
would
be
extremely
reluctant
to
continue
the
takeoff
if
he
had
to cl
imb
over
obstructions.
However,
if
the
failure
occurred
at
an
altitude
as
high
or
higher
than
surrounding
obstructions,
he
would
feel
free
to
maneuver
for
a
landing
back
at
the
airport.
Fortunately,
the
airplane
accelerates
through
this
"area
of
decision"
in
just
a
few
seconds. However,
to
make
an
intelligent
decision
in
this
type
of
emergency, one must
consider
the
field
length,
obstruction
height,
field
elevation,
air
temperature,
headwind, and
takeoff
weight.
The
flight
paths
illustrated
in
Figure
3-2
indicate
that
the
"go no-go
area
of
decision"
is
bounded by:
(1)
the
point
at
which
95
KIAS
is
reached
and
(2)
the
point
where
the
obstruction
altitude
is
reached.
An
engine
failure
in
this
area
reqUires
an
immediate
decision.
Beyond
this
area,
the
airplane,
within
the
limitations
of
one engine
inoperative
climb performance
shown
in
Section
5
••
may
be
maneuvered
to
a
landing
back
at
the
airport.
ENGINE FAILURE DURING TAKEOFF
GO
NO-GO
DECISION
,."~-'
J
GO
NO-GO
95
KtAS
.•
,AREA
OF
,,,DECISION
NORMAL
TAKEOFF
.,
Fi9ure
3-2
I November 1979
Revision
4 - 1 December 1983
3-15

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