Cessna 402B 1973 - Page 48

NOTE
If start
is
unsuccessfuI,
turn
inoperative engine
magneto
s\ryitches
OFF,
retard
mixfure
to
IDLE
CUT-OFF,
open
throttle
fully,
and
engage starter
for several
revolutions.
Then
repeat air-start
procedures,
AI R CRAFI
WITH
OPTION
A!
PROPEttER U NFEATHERING
SYSTE'I1
INSTAI.TED
(1)
Magneto
Switches -
ON.
(2)
Throttle -
FORWARD approximately
one
inch.
(3)
Mixture
- FULL
RICH.
(4)
Propeller
-
FULL
FORWARD.
NOTE
The
propeller
will automatically
windmill
when
the
propeller
lever is moved out of the FEATH-
ER
position.
(5)
Propeller -
RETARD
to
detent. when
propeller
reaches 1000
RPM.
(6)
Power
- INCREASE
after
cylinder head temperature
reaches
200'F.
SINGI.E
-
ENGINE APPROACH AND TANDING
(1)
Mixture
-
FULL
RICH.
(2)
Propeller - FULL FORWARD.
(3)
Approach
at 120 MPH IAS with
excessive
altitude.
(4)
Landing
Gear - DOWN
when
witNn
gliding
distance of field.
(5)
Wing Flaps
-
DOrffN
when
landing
is assured,
(6)
Decrease
speed
below
110
MPH IAS
only if landing
is assured.
(7)
Minimum
Single-Engine
Control Speed - 95 MPH
IAS.
MAXIMUM
GLIDE
In
the
event
of
a double-engine failure
condition,
maximum
gliding
dis-
tance
can
be
obtained
by
feathering
both
propellers,
and maintaining ap-
proximately
133
MPH
IAS with
landing
gear
and
wing flaps
up.
Refer
to
the Maximum
Glide Diagram,
Figure 3-4,
for maximum
glide
data.
3-8