CA.V.C.K4
KnowledgeProper pitch control required for continuously decreasing airspeed.
From the FAA library
- Chapter 10: Performance Maneuvers › Chandelle
angle of bank is fixed during the first 90°, recall that as airspeed decreases, the overbanking tendency increases. [Figure 10-3C] As a result, proper use of the ailerons allows the bank to remain at a fixed angle until ... vertical component of lift increases. However, as speed continues to decrease, a slight increase of elevator back pressure is required to keep the pitch attitude from decreasing. When the airspeed is slowest, near the completion of the chandelle, right rudder…
- Chapter 3: Basic Flight Maneuvers › Effect and Use of Flight Controls
With the pilot’s hand: ⦁ When pulling the elevator pitch control toward the pilot, which is an aft movement of the control wheel, yoke, control stick, or side stick controller (referred to as adding back pressure), the airplane’s nose ... will rotate backwards relative to the pilot around the pitch (lateral) axis of the airplane. Think of this movement from the pilot’s feet to the pilot’s head. ⦁ When pushing elevator pitch control toward the instrument panel, (referred…
- Chapter 3: Basic Flight Maneuvers › Trim Control
then hold the wings level with aileron flight control pressure while rudder control pressure is trimmed out. Finally, aileron trim should be adjusted to relieve any aileron flight control pressure. A properly trimmed airplane is an indication of good piloting ... skills. Any control forces that the pilot feels should be a result of deliberate flight control pressure inputs during a planned change in airplane attitude, not a result of forces being applied by the airplane. A common trim control error…
- Chapter 6: Takeoffs and Departure Climbs › Normal Takeoff › Initial Climb
pilot should also consider flying at a lower pitch for cruise climb since flying at VY requires much quicker pilot response in the event of a powerplant failure to preclude a stall. Since the power on the initial climb ... takeoff power setting, the airspeed should be controlled by making slight pitch adjustments using the elevators. However, the pilot should not fixate on the airspeed indicator when making these pitch changes, but should continue to scan outside to adjust…
- Chapter 7, Section II: Airplane Basic Flight Maneuvers › Common Errors › Steep Turns
allowed to continue to decrease, a pronounced loss of altitude is indicated on the altimeter along with the VSI tape, as well as the altitude trend indicator. Additionally, the airspeed begins to increase due to the lowered pitch attitude ... loss of altitude, the pilot begins to slowly increase back pressure on the control yoke in order to increase the pitch attitude. The pitch change required is usually no more than 3 degrees to 5 degrees, depending on the type…
- Chapter 7, Section II: Airplane Basic Flight Maneuvers › Straight-and-Level Flight › Pitch
already decreased below the speed desired, which will require additional adjustment in the power setting. 4. Fixation on airspeed tape or manifold pressure indications during airspeed changes, resulting in erratic control of airspeed, power, as well as pitch and bank ... being trimmed for airspeed, not a pitch attitude. 4. Faulty sequence in trim techniques. Trim should be utilized to relieve control pressures, not to change pitch attitudes. The proper trim technique has the pilot holding the control wheel first…