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Extra resources for Airplane Flying Handbook: FAA-H-8083-3A
Qxd 7/13/04 11:08 AM Page 3-15 becomes greater as the angle of bank is increased. So shallow turns should be used to maintain an efficient rate of climb. Figure 3-16. Climb indications. All the factors that affect the airplane during level (constant altitude) turns will affect it during climbing turns or any other training maneuver. It will be noted that because of the low airspeed, aileron drag (adverse yaw) will have a more prominent effect than it did in straight-and-level flight and more rudder pressure will have to be blended with aileron pressure to keep the airplane in coordinated flight during changes in bank angle.
These forces need not be strong, only perceptible by the pilot to be useful. An accomplished pilot who has excellent “feel” for the airplane will be able to detect even the minutest change. The response of the aileron and rudder controls to the pilot’s touch is another element of “feel,” and is one 3-2 that provides direct information concerning airspeed. As previously stated, control surfaces move in the airstream and meet resistance proportional to the speed of the airstream. When the airstream is fast, the controls are stiff and hard to move.
In any turn, the loss of vertical lift and increased induced drag, due to increased angle of attack, Common errors in the performance of climbs and climbing turns are: DESCENTS AND DESCENDING TURNS When an airplane enters a descent, it changes its flightpath from level to an inclined plane. qxd 7/13/04 11:08 AM Page 3-16 the pilot know the power settings and pitch attitudes that will produce the following conditions of descent. PARTIAL POWER DESCENT—The normal method of losing altitude is to descend with partial power.
Airplane Flying Handbook: FAA-H-8083-3A by Federal Aviation Administration