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SECTION 7 CESSNA AIRPLANE AND SYSTEMS DESCRIPTION MODEL 208B G1000 7-42 TYPICAL ENGINE COMPONENTS 1. Propeller Shaft 2. Propeller Governor Drive Pad 3. Second Stage Planetary Gear 4. First Stage Planetary Gear 5. Power Turbine Shaft 6. Fuel Nozzle 7. Power Turbine 8. Combustion Chamber 9. Compressor Turbine 10.Centrifugal Compressor Impeller 11. Axial-Flow Compressor Impellers (3) 12.Compressor Air Inlet U.S. Figure 7-8 13.Accessory Gearbox Drive Shaft 14.Accessory Gearbox Cover 15.Starter-Generator Drive Shaft 16.Oil Scavenge Pump 17.Number 1 Bearing 18.Compressor Bleed Valve 19.Number 2 Bearing 20.Number 3 Bearing 21.Number 4 Bearing 22.Exhaust Outlet 23.Chip Detector 24.Roller Bearing 25.Thrust Bearing 208BPHBUS-00
CESSNA SECTION 7 MODEL 208B G1000 AIRPLANE AND SYSTEMS DESCRIPTION ENGINE CONTROLS The engine is operated by four separate controls consisting of a power lever, EMERGENCY POWER Lever, PROP RPM Lever, and a FUEL CONDITION Lever. The power and FUEL CONDITION Levers are engine controls while the PROP RPM Lever controls propeller speed and feathering. POWER LEVER The power lever is connected through linkage to a cam assembly mounted in front of the fuel control unit at the rear of the engine. The power lever controls engine power through the full range from maximum takeoff power back through idle to full reverse. The lever also selects propeller pitch when in the BETA range. The power lever has MAX, IDLE, and BETA and REVERSE range positions. The range from MAX position through IDLE enables the pilot to select the desired power output from the engine. The BETA range enables the pilot to control propeller blade pitch from idle thrust back through a zero or nothrust condition to maximum reverse thrust. CAUTION The propeller reversing linkage can be damaged if the power lever is moved aft of the idle position when the propeller is feathered. 208BPHBUS-00 U.S. 7-43
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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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