CESSNA
MODEL 208B 867 SHP
GARMIN G1000
AFTER LANDING
1. WING FLAPS Handle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP
2. Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
a. PITOT/STATIC HEAT Switch . . . . . . . . . . . . . . . . . . . . OFF
b. STALL HEAT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
4. Amber STBY PWR INOP Annunciator . . . . . . . . . . . . . CHECK
5. STROBE Lights Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
6. LDG and TAXI/RECOG Lights Switches . . . . . . . . . . . . . . SET
7. FUEL CONDITION Lever . . . . . . . . . . . . . . . . . . . . . LOW IDLE
If the FUEL CONDITION lever is moved past the LOW
IDLE position and the engine N
moving the lever back to the LOW IDLE position can
cause an ITT over-temperature condition. If the engine
has started to shutdown in this situation, allow the
engine to complete its shutdown sequence, and
proceed to do a normal engine start using the
STARTING ENGINE checklist.
FAA APPROVED
208BPHCUS-00
NORMAL PROCEDURES
(verify annunciator is shown)
(when clear of the runway)
CAUTION
falls below 55%,
g
SECTION 4
U.S.
4-41