SECTION 3 CESSNA
EMERGENCY PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
AIRSTART
STARTER ASSIST
1. BATTERY Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
2. AVIONICS No. 1 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
3. Electrical Load. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE
a. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
b. AVIONICS No. 2 Switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
With AVIONICS No. 2 switch in the OFF position, the
dynamic redline will become fixed at 2397 FT-LB regardless
of temperature or altitude changes. The cruise torque bug
will become inoperative and will not be shown on the EIS
torque indicator.
c. IGNITION Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
d. Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . . . CLOSE
(push in)
e. Left LIGHTS Panel Switches (9 total) . . . . . . . . . . . . . . OFF
f. POWER OUTLET Switch(es) . . . . . . . . . . . . . . . . . . . . OFF
g. VENT AIR FANS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
h. AIR CONDITIONING (if installed). . . . . . . . . . . . . . . . . OFF
i. TEMP Control Knob . . . . . . . . . . . . . . . . . . . . . . . CLOSED
(rotate FULL counterclockwise)
j. BLEED AIR HEAT Switch. . . . . . . . . . . . . . . . . . . . . . . OFF
4. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . . . NORMAL
(push in)
5. EMERGENCY POWER Lever. . . . . . . . . . . . . . . . . . . NORMAL
6. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
7. PROP RPM Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MIN
8. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . . CUTOFF
9. FUEL/OIL SHUTOFF Knob. . . . . . . . . . . . . . . . . . . . . . . . . . ON
(push in)
10. FUEL TANK SELECTORS . . . . . . . . . . . . . . . . . . . . BOTH ON
(Continued Next Page)
208BPHCUS-00
3-12
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