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AI.IX.B.S4

Skill

Apply wind-drift correction to track a constant radius circle around selected reference point with bank not to exceed 60° a steepest point in turn.

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Get a short, cited explanation of this element written from the FAA handbooks: the core idea, the numbers that matter, common test traps, and a quick self-check.

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From the FAA library

  • Chapter 10: Performance Maneuvers › Steep Spiral

    clearing the airspace for air traffic and hazards. In general, the throttle is closed to idle, carburetor heat is applied if equipped, and gliding speed is established. Once the proper airspeed is attained, the pitch should be lowered ... airplane rolled to the desired bank angle as the reference point is reached. The pilot should consider the distance from the reference point since that establishes the turning radius, and the steepest bank should not exceed 60°. The gliding spiral…

  • Chapter 3: Basic Flight Maneuvers › Level Turns

    throttle provides thrust, which may be used for airspeed control and to vary the radius of the turn. ⦁ The pilot uses the rudder to offset any adverse yaw developed by wing’s differential lift and the engine/propeller. The rudder does ... turn the airplane. The rudder is used to maintain coordinated flight. For purposes of this discussion, turns are divided into three classes: shallow, medium, and steep. ⦁ Shallow turns—bank angle is approximately 20° or less. This shallow bank is such…

  • Chapter 3: Basic Flight Maneuvers › Straight-and-Level Flight › Straight Flight

    Straight Flight Maintaining a constant direction or heading is accomplished by visually checking the relationship of the airplane’s wingtips to the natural horizon. Depending on whether the airplane is a high wing or low wing, both wingtips should ... level and equally above or below the natural horizon. Any necessary bank corrections are made with the pilot’s coordinated use of ailerons and rudder. [Figure 3-7] The pilot should understand that anytime the wings are banked, the airplane…

  • Chapter 5: Aerodynamics of Flight › Load Factors › Load Factors in Steep Turns

    Load Factors in Steep Turns At a constant altitude, during a coordinated turn in any aircraft, the load factor is the result of two forces: centrifugal force and weight. [Figure 5-52] For any given bank angle, the ROT varies ... centrifugal force, allowing the load factor to remain the same. Figure 5-52. Two forces cause load factor during turns. Figure 5-53 reveals an important fact about turns—the load factor increases at a terrific rate after a bank…

  • Chapter 3: Basic Flight Maneuvers › Level Turns › Establishing a Turn

    steeper turns, additional power may be required to maintain airspeed. If altitude is not being maintained during the turn, the pitch attitude should be corrected in relation to the natural horizon and cross-checked with the flight instruments to verify ... performance. Steep turns require accurate, smooth, and timely flight control inputs. Minor corrections for pitch attitude are accomplished with proportional elevator back pressure while the bank angle is held constant with the ailerons. However, during steep turns…

  • Chapter 7, Section I: Airplane Basic Flight Maneuvers › Turns › Steep Turns

    When turning to an east or west heading from a southerly direction, start the rollout approximately 5 degrees before the east or west indication is reached. When turning to other headings, the lead or lag must be interpolated. Abrupt changes ... resulting erratic movements of the compass card make accurate interpretations of the instrument very difficult. Proficiency in compass turns depends on knowledge of compass characteristics, smooth control technique, and accurate bank-and-pitch control. Figure 7-35. North and south…