SECTION 4
CESSNA
NORMAL PROCEDURES
MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
ENROUTE CLIMB
(Continued)
MAXIMUM PERFORMANCE CLIMB
1. Ice Protection . . . . . . . . . . . . . . . . . . . . . . . . . .
AS REQUIRED
a. PITOT/STATIC HEAT Switch . . . . . . . . . . . . . . . . . . . . .
ON
(when OAT is below 5°C (41°F) and in visible moisture)
b. STALL HEAT Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . .
ON
(when OAT is below 5°C (41°F) and in visible moisture)
2. INERTIAL SEPARATOR . . . . . . . . . . . . . . . . . . . . . . . . . . .
SET
(position INERTIAL SEPARATOR to NORMAL or BYPASS as
conditions warrant)
3. Airspeed . . . . . . . . . . . .
108 KIAS
(from sea level to 3000 feet)
decreasing to
92 KIAS
(at 20,000 feet)
4. PROP RPM Lever . . . . . . . . . . . . . . . . . . . . . . . . . . .
1900 RPM
5. POWER Lever. . . . . . . . . . . . . . . . . . . . . . . . .
SET
FOR CLIMB
(observe Maximum Climb Torque, ITT and N
g
limits)
Refer to Section 5, Performance, Figure 5-9, Maximum Engine
Torque for Climb for approved engine power settings.
CAUTION
For every 10°C (18°F) below -30°C (-22°F) ambient
temperature, reduce maximum allowable N
g
by 2.2%.
The Garmin G1000 incorporates a temperature
compensating N
g
redline.
208BPHCUS-00
4-36
Summary of Contents for Cessna Grand Caravan Ex 208B
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