CESSNA
SECTION 4
MODEL 208B 867 SHP
NORMAL PROCEDURES
GARMIN G1000
U.S.
FAA APPROVED
BEFORE TAKEOFF
1. PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SET
(depress brake pedals and pull handle out)
2. Seats, Seat Belts and
Shoulder Harnesses . . . . . . . . . . . . . . . . .
CHECK SECURE
WARNING
Failure to correctly use seat belts and shoulder
harnesses can result in serious or fatal injury in the
event of an accident.
3. Flight Controls. . . . . . . . . . . . . . . . . . . . .
FREE and CORRECT
4. Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
5. Altimeters:
a. PFD 1 and PFD 2 (BARO) . . . . . . . . . . . . . . . . . . . . . .
SET
b. Standby Altimeter . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SET
6. ALT SEL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
SET
7. Standby Flight Instruments . . . . . . . . . . . . . . . . . . . . . .
CHECK
8. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . .
NORM
9. FUEL TANK SELECTORS . . . . . . . . . . . . . . . . . . . .
BOTH ON
10. FUEL QTY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
11. FUEL/OIL SHUTOFF Knob . . . . . . . . . . . . . . . . . . . . .
CHECK
(verify FULL in)
12. ELEVATOR, AILERON, and RUD TRIM Controls . . . . . .
3
SET
(for takeoff)
13. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
400 FT-LB
a. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
CHECK
(verify 28.5 volts minimum)
b. INERTIAL SEPARATOR. . . . . . . . . . . . . . . . . . . . .
CHECK
Turn control counterclockwise, pull to BYPASS position and
check torque drop; move control back to NORMAL position
and check that original torque is regained.
c. Engine Indicating System. . . . . . . . . . . . . . . . . . . .
CHECK
(verify oil temp 32 - 99
°
C for takeoff)
(Continued Next Page)
208BPHCUS-00
4-29
Summary of Contents for Cessna Grand Caravan Ex 208B
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