Cessna 402C - Page 58

(AMPLIFIED PROCEDURES)
SECTION 3
EMERGENCY PROCEDURES
AIRSTART (Afte, Feathedng)
Airplane Without Optional Propeller Unfeathering System:
I. Auxiliary Fuel Pump - CHECK OFF. If ON 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 revolu-
tions 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 - FDRWARD of detent.
7. Starter Button - PRESS.
8. Primer Switch - ACTIVATE.
9. Starter and Primer Switch - RELEASE when engine fires.
10. Auxiliary Fuel Pump - LOW.
11. Mixture - ADJUST for smooth engine operation.
12. Power - INCREASE after cylinder head temperature reaches 200
0
F with
gradual mixture enrichment as power increases.
13. Cowl Flap - AS REQUIRED.
14. Alternator - ON.
Airplane With Optional Propeller Unfeathering System:
I. Auxiliary Fuel Pump - CHECK OFF. If DN 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 revolu-
tions 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.
r-------- NOTE ----------,
The propeller will automatically windmill when the
propeller lever
is moved out of the FEATHER
position.
7. Propeller - RETARD to detent when propeller reaches 1000 RPM.
8. Auxiliary Fuel Pump - LOW.
9. Mixture ~ ADJUST for smooth engine operation.
10. Power - INCREASE after cylinder head temperature reaches 200
0
F with
gradual mixture enrichment as power increases.
II. Cowl Flap - AS REQUIRED.
12. Alternator - ON.
I November 1979
3-19