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10.
In crosswind conditions, directional control can be enhanced by using the single wheel brakes. Note that using the brakes for directional control increases the take-off roll distance. 12.
FOR THE SHORTEST POSSIBLE TAKE-OFF DISTANCE TO CLEAR A 15 M (50 FT) OBSTACLE: 4.4.8. Climb For aircraft without the altitude compensating fuel pump, at full throttle settings with power less than 75%, it is necessary to lean the engine with the mixture control. It should be noted that with the engine set to full throttle, it can produce less than 75% power, depending on pressure altitude. Refer to the Section 5.3.2., Performance to determine the engine performance as a function of altitude and temperature. Expect engines without altitude compensating fuel pump to require leaning at full throttle above 5000 ft pressure altitude. 3. 4. 5. 6.
2. 3. 4. 5. 6.
2. 3. 4.
CHT NOT BELOW 300o F FOR MORE THAN 5 MINUTES. 240o F MIN. To achieve a fast descent: 4.4.11. Landing Approach 2. 3. 4. 5. 6. 7. 8. 9. 10. 11. 12.
FOR STRONG HEADWIND, CROSSWIND, DANGER OF WIND-SHEAR OR TURBULENCE, A HIGHER APPROACH SPEED SHOULD BE SELECTED. 4.4.12. Balked Landing 2. |