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SECTION 5 CESSNA PERFORMANCE MODEL 208B G1000 MAXIMUM ENGINE TORQUE FOR CLIMB CONDITIONS: 1900 RPM V y KIAS INERTIAL SEPARATOR NORMAL 5-18 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. Figure 5-9 U.S. FAA APPROVED 208BPHBUS-00
CESSNA SECTION 5 MODEL 208B G1000 PERFORMANCE FAA APPROVED 208BPHBUS-00 Figure 5-10 (Sheet 1 of 5) U.S. 5-19
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CESSNA INTRODUCTION MODEL 208B G100
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CESSNA SECTION 1 MODEL 208B G1000 G
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CESSNA SECTION 2 MODEL 208B G1000 L
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SECTION 3 CESSNA EMERGENCY PROCEDUR
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SECTION 3 CESSNA ABNORMAL PROCEDURE
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CESSNA SECTION 3 MODEL 208B G1000 A
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CESSNA SECTION 4 MODEL 208B G1000 N
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CESSNA SECTION 5 MODEL 208B G1000 P
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CESSNA SECTION 6 MODEL 208B G1000 W
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SECTION 7 CESSNA AIRPLANE AND SYSTE
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CESSNA SECTION 8 MODEL 208B G1000 H
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