SECTION 4 CESSNA
NORMAL PROCEDURES MODEL 208B 867 SHP
GARMIN G1000
U.S.
FAA APPROVED
ENROUTE CLIMB (Continued)
If climb requirements do not necessitate a maximum performance
climb, a POWER lever setting that will result in an ITT of 785 °C
throughout the climb may be desirable over setting the POWER lever
per Figure 5-9 Maximum Engine Torque For Climb chart located in
Section 5 of the POH.
For improved visibility over the nose, a cruise climb airspeed of 115 -
125 KIAS may be desirable at altitudes up to approximately 12,000
feet. Adjust the POWER lever per Figure 5-9, Maximum Engine Torque
for Climb chart located in Section 5 of the POH with the PROP RPM set
at 1900 to prevent exceeding the maximum allowable shaft horsepower
for the ambient conditions. After Climb Torque is set, PROP RPM can
be reduced in accordance with the following table for improved
passenger comfort.
Under no circumstances should the following limitations be exceeded:
1. The MAX TORQUE for the corresponding PROP RPM
2. A maximum climb ITT of 825°C
3. A maximum N
g
of 103.7%
To achieve maximum flat rated horsepower, PROP RPM
lever must be set at 1900 RPM.
If an obstruction dictates the use of a steep climb angle, climb with
FLAPS UP and maximum continuous power at 85 KIAS.
PROP RPM MAX TORQUE
1900 2397 FT-LB
1800 2397 FT-LB
1700 2397 FT-LB
1600 2397 FT-LB
208BPHCUS-004-60
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