Textron Cessna Grand Caravan Ex 208B - Taxiing

SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
STARTING ENGINE (With External Power) (Continued)
21. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
22. Amber STARTER ON Annunciator . . . . . . . . . . . . . . . . CHECK
(verify annunciator is not shown)
23. Engine Indicating System . . . . . . . . . . CHECK PARAMETERS
(verify all parameters in normal range)
24. EXTERNAL POWER Switch. . . . . . . . . . . . . . . . . . . . . . . . OFF
25. External Power Unit. . . . . . . . . . . . . . . OFF, then DISENGAGE
26. GEN AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK LOAD
27. Amber GENERATOR Off Annunciator . . . . . . . . . . . . . CHECK
(verify annunciator is not shown)
28. BAT AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
(verify charge shown (positive))
29. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
30. Amber FUEL BOOST ON Annunciator . . . . . . . . . . . . . CHECK
(verify annunciator is not shown)
31. AVIONICS No. 2 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
NOTE
With AVIONICS No. 2 Switch ON, verify white TORQUE
GAGE annunciator is not shown and the dynamic redline
agrees with the values listed in Figure 5-8, Maximum
Engine Torque For Takeoff, for current altitude and
temperature.
32. NAV Lights Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
33. Cabin Heating, Ventilating
and Defrosting Controls . . . . . . . . . . . . . . . . . . . AS DESIRED
TAXIING
1. Brakes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
NOTE
Propeller BETA range can be used during taxi with
minimum blade erosion up to the point where N
g
increases
(against beta range spring) to control taxi speed and
improve brake life.
2. Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
208BPHCUS-004-28