SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
BEFORE TAKEOFF (Continued)
14. Overspeed Governor. . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(first flight of the day and after maintenance)
a. PROP RPM Lever. . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAX
(full forward)
b. OVERSPEED GOVERNOR
TEST Button . . . . . . . . . . . . . . . . . . . PRESS and HOLD
c. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . ADVANCE
(propeller RPM stabilize at 1750 ±60 RPM)
Smoothly advance the POWER lever to allow propeller
RPM to stabilize. Rapid movement of the POWER lever will
cause the propeller to surge.
d. POWER Lever . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDLE
e. OVERSPEED GOVERNOR TEST Button . . . . . RELEASE
15. Quadrant Friction Lock . . . . . . . . . . . . . . . . . . . . . . . . ADJUST
16. Standby Power . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(first flight of the day)
a. ENGINE Softkey. . . . . . . . . . . . . . . . . . . SELECT SYSTEM
b. STBY ALT PWR Switch . . . . . . . . . . . . . . . . . . . . . . . . . ON
c. GEN AMPS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . LOAD
(to approximately 30 amps)
Generator load can be increased by turning the TAXI/
RECOG Lights ON. Do not exceed 60 amps total load.
d. ALT AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(alternator output near zero)
e. GENERATOR Switch . . . . . . . . . . . . . . . . . . . . . . . . . TRIP
f. ALT AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify load)
(Continued Next Page)
208BPHCUS-004-30