Table of Contents
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CESSNA
MODEL 208B 867 SHP
GARMIN G1000
BEFORE TAKEOFF
1. PARKING BRAKE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SET
2. Seats, Seat Belts and
Shoulder Harnesses . . . . . . . . . . . . . . . . . CHECK SECURE
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
12. ELEVATOR, AILERON, and RUD TRIM Controls . . . . . . 3 SET
13. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 400 FT-LB
a. BUS VOLTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
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
FAA APPROVED
208BPHCUS-00
(depress brake pedals and pull handle out)
WARNING
(verify oil temp 32 - 99
(Continued Next Page)
SECTION 4
NORMAL PROCEDURES
(verify FULL in)
(for takeoff)
(verify 28.5 volts minimum)
°
C for takeoff)
U.S.
4-29
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