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Cessna 402C - Page 44

Cessna 402C
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MODEL
402C
AIRSTART
(ABBREVIATED
PROCEDURES)
...........
'''''''
..
0.1
EMERGENCY
PROCEDURES
---./
Airplane Without Optional Propeller
Unleatt1ering
System:
1. Auxiliary Fuel
Pump
- CHECK OFF.
lION
or LOW,
purge
engine by turning OFF
auxiliary
fuel
pump,
mixture
to
IDLE
CUT-OFF.
throttle
full
open,
magneto
switches
OFF,
and
rotating
engine
15
revolutions
with
starter.
2.
Magneto Switches - ON.
3.
Fuel
Selector - MAIN TANK (Feel For Detent).
4.
Throttle
- FORWARD approximately·
one
and
one-half
inches.
5.
Mixture
-
FULL
RICH
then
retard
approximately
two
inches.
6.
Propeller - FORWARD
01
detent
7.
Starter Button - PRESS.
8.
Primer Switch - ACTIVATE.
9.
Starter
and
Primer
Switch
-
RELEASE
when
engine
fires.
,
O.
Auxiliary
Fuel
Pump
- LOW.
,
1.
Mixture
- ADJUST
for
smooth
engine
operation.
12.
Power
- INCREASE
after
cylinder
head
temperature
reaches
200°F
with
gradual
mixture
enrichment
as
power
increases.
13. Cowl Flap -
AS
REQUIRED.
14. Alternator
- ON.
Airplane With Optional Propeller Unleathering System:
1.
Auxiliary Fuel pump - CHECK OFF.
lION
or LOW, purge engine by turning OFF
auxiliary
fuel
pump,
mixture
to
IDLE
CUT-OFF,
throttle
full
open,
magneto
switches
OFF,
and
rotating
engine
15
revolutions
with
starter.
2.
Magneto Switches - ON.
3.
Fuel
Selector - MAIN TANK (Feel
For
Detent).
4.
Throttle
- FORWARD
approximately
one
and
one-half
inches.
5.
Mixture
,.
FULL RICH
then
retard
approximately
two
inches.
6.
Propeller - FULL FORWARD.
7.
Propeller - RETARD to detent
when
propeller reaches 1000 RPM.
8.
Auxiliary
Fuel
Pump
- LOW.
9.
Mixture - ADJUST lor smooth engine operation.
10. Power - INCREASE after cylinder
head
temperature reaches 200°F with gradual
mixture
enrichment
as
power
increases.
11. Cowl Flap -
AS
REQUIRED.
12. Alternator - ON.
BOTH ENGINES FAILURE DURING CRUISE FLIGHT
1.
Wing Flaps - UP.
2.
Landing
Gear -
UP.
3.
Propellers - FEATHER.
4. Cowl Flaps - CLOSE.
5.
Airspeed - 117 KIAS (See Figure 3-3).
6.
Landing - ReIer to FORCED LANDING (Complete Power Loss)
in
this section.
1 November 1979
3-5

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