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Cessna 208B - Page 184

Cessna 208B
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CESSNA SECTION 5
MODEL
2088 (675 SHP) PERFORMANCE
MAXIMUM ENGINE TORQUE FOR CLIMB
CONDITIONS:
1900 RPM
V,
KlAS
Inertial Separator
-
Normal
NOTE
1. Torque on this chart shall be achieved without exceeding
765°C ITT or 101.6 percent
Ng.
2. With the inertial separator in BYPASS, decrease torque setting
by 100 Ft-Lbs.
3.
With the cabin heater ON, decrease torque setting by 80 Ft-
Lbs.
-60
-50
40
-30
-20
-10
0
10
20
30
40
50
60
Outside
Air
Temperalure
-
"C
Figure 5-8A'. Maximum Engine Torque for Climb
1
Revis~on 23 U.S. 5-21
-,

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