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SECTION 4 CESSNA NORMAL PROCEDURES MODEL 208B G1000 TAKEOFF POWER SETTING Refer to the Maximum Engine Torque for Takeoff chart in Section 5 to determine the torque corresponding to the surface altitude and OAT conditions. This torque should be obtainable without exceeding 805°C ITT or 101.6% N g . Takeoff roll is most smoothly initiated by gradually advancing the POWER Lever until propeller RPM nears 1900. Smoothly release the brakes and continue advancing the POWER Lever until the takeoff torque is reached. NOTE As airspeed increases during takeoff, an increase in torque at a fixed POWER Lever position is normal and need not be reduced provided the torque limit (1865 foot-pounds) is not exceeded. WING FLAP SETTINGS A flap setting of 20° is recommended for all takeoffs unless a strong crosswind exists at which time 10° flaps may be preferred. Use of 20° flaps provides for a lower liftoff speed, as well as a reduction in ground roll and total distance over an obstacle compared to takeoff with flaps up. Flap settings greater than 20° are not approved for takeoff. SHORT FIELD TAKEOFF If an obstruction dictates the use of a steep climb angle after liftoff, accelerate to and climb at an obstacle clearance speed of 83 KIAS with 20° flaps. Takeoff performance data is shown in Section 5 based on this speed and configuration. 4-44 NOTE The 83 KIAS obstacle clearance speed is a recommended safe speed under all conditions, including turbulence and complete engine failure. The actual VX speed with flaps 20° is 70 KIAS at maximum takeoff weight as noted in the Climb Gradient - Takeoff Flap Setting - Flaps 20 chart in Section 5. U.S. (Continued Next Page) FAA APPROVED 208BPHBUS-00
CESSNA SECTION 4 MODEL 208B G1000 NORMAL PROCEDURES SHORT FIELD TAKEOFF (Continued) After clearing the obstacle, and reaching a safe altitude, the flaps can be retracted slowly as the airplane accelerates to the normal climb airspeed. Minimum ground roll takeoffs are accomplished by using 20° flaps, lifting the nose wheel off the ground as soon as practical and leaving the ground in a slightly tail-low attitude. However, after liftoff the airplane should be leveled immediately to accelerate to a safe climb airspeed. TYPE II, TYPE III OR TYPE IV ANTI-ICE FLUID TAKEOFF When Type II, Type III or Type IV anti-ice fluid is applied to the airplane, a rotation speed of 89 KIAS with flaps UP is required. Use of flaps UP allows the airplane to accelerate to a higher rotation speed without any liftoff tendencies, which is required for the Type II, Type III or Type IV anti-ice fluid to be effective. Takeoff performance data shown in Section 5 is based on this speed and configuration. CROSSWIND TAKEOFF Takeoffs into strong crosswinds normally are performed with FLAPS 10° or 20°. With the ailerons partially deflected into the wind, the airplane is accelerated to a speed higher than normal, and then rotated to prevent settling back to the runway. When clear of the ground, make a coordinated turn into the wind to correct for drift. The use of flaps 10° will improve directional control, but will also increase the takeoff distance. Increase the flaps 20° short field takeoff lift off and 50 feet obstacle speeds by 7 knots, if flaps 10° is used for takeoff. ENROUTE CLIMB Normally, maximum climb power is maintained during the climb to cruise altitude. Adjust the POWER Lever as required to prevent exceeding maximum climb torque, maximum climb ITT of 765°C, or maximum climb N g of 101.6%, whichever occurs first. NOTE Engine operations which exceed 740°C ITT can reduce engine life. (Continued Next Page) FAA APPROVED 208BPHBUS-00 U.S. 4-45
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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 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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