SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
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
(verify no red X’s)
5. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(24 volts minimum)
6. EMERGENCY POWER Lever. . . . . . . . . . . . . . . . . . . NORMAL
(full aft position)
7. Red EMERG PWR LVR Annunciator . . . . . . . . . . . . . . CHECK
(verify annunciator is not shown)
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
(verify annunciator is shown)
b. Amber FUEL PRESS LOW Annunciator . . . . . . . . CHECK
(verify annunciator is not shown)
c. FFLOW PPH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify 0 fuel flow PPH indicated)
10. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . START
a. White IGNITION ON Annunciator. . . . . . . . . . . . . . CHECK
(verify annunciator is shown)
b. OIL PSI . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify oil pressure indicated)
c. N
g
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STABLE
(12% minimum)
(Continued Next Page)
208BPHCUS-004-24