SECTION 4
NORMAL PROCEDURES
STARTING ENGINE (With Battery)
1. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2. BCN Light Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3. AVIONICS No. 1 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
4. Engine Indicating System . . . . . . . . . . CHECK PARAMETERS
5. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
6. EMERGENCY POWER Lever. . . . . . . . . . . . . . . . . . . NORMAL
7. Red EMERG PWR LVR Annunciator . . . . . . . . . . . . . . CHECK
Make sure that the EMERGENCY POWER lever is in
the NORMAL (full aft) position or an over-temperature
condition will result during engine start.
8. Propeller Area . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CLEAR
(verify that all people and equipment are at a safe distance from
the propeller)
9. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
a. Amber FUEL BOOST ON Annunciator. . . . . . . . . . CHECK
b. Amber FUEL PRESS LOW Annunciator . . . . . . . . CHECK
c. FFLOW PPH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
10. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START
a. White IGNITION ON Annunciator . . . . . . . . . . . . . . CHECK
b. OIL PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
c. N
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STABLE
g
4-24
CAUTION
(Continued Next Page)
U.S.
MODEL 208B 867 SHP
GARMIN G1000
(verify no red X's)
(24 volts minimum)
(full aft position)
(verify annunciator is not shown)
(verify annunciator is shown)
(verify annunciator is not shown)
(verify 0 fuel flow PPH indicated)
(verify annunciator is shown)
(verify oil pressure indicated)
(12% minimum)
FAA APPROVED
208BPHCUS-00
CESSNA