SECTION 4
NORMAL PROCEDURES
STARTING ENGINE (With External Power)
21. STARTER Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
22. Amber STARTER ON Annunciator . . . . . . . . . . . . . . . . CHECK
23. Engine Indicating System . . . . . . . . . . CHECK PARAMETERS
24. EXTERNAL POWER Switch . . . . . . . . . . . . . . . . . . . . . . . . OFF
25. External Power Unit. . . . . . . . . . . . . . . OFF, then DISENGAGE
26. GEN AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK LOAD
27. Amber GENERATOR Off Annunciator . . . . . . . . . . . . . CHECK
28. BAT AMPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
29. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
30. Amber FUEL BOOST ON Annunciator . . . . . . . . . . . . . CHECK
31. AVIONICS No. 2 Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
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
Propeller BETA range can be used during taxi with
minimum blade erosion up to the point where N
(against beta range spring) to control taxi speed and
improve brake life.
2. Flight Instruments . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
4-28
(verify all parameters in normal range)
NOTE
NOTE
U.S.
MODEL 208B 867 SHP
GARMIN G1000
(verify annunciator is not shown)
(verify annunciator is not shown)
(verify charge shown (positive))
(verify annunciator is not shown)
increases
g
FAA APPROVED
208BPHCUS-00
CESSNA
(Continued)