Tutor Platform

AI.XI.B.S2

Skill

Climb at a constant airspeed to specific altitudes in straight flight and turns.

Study note

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.

Sign in to generate a study note

From the FAA library

  • Chapter 8: Helicopter Attitude Instrument Flying › Turn Indicator › Power Control During Straight-and-Level Flight

    Common Errors During Straight-and-Level Flight Failure to maintain altitude 2…

  • Chapter 10: Performance Maneuvers › Chandelle

    that begins from approximately straight-and-level flight and concludes with the airplane in a wings-level, nose-high attitude just above stall speed. [Figure 10-3] The goal is to gain the most altitude possible for a given bank ... specific phases: the first 90° of turn and the second 90° of turn. The first 90° of turn is described as constant bank and continuously increasing pitch; and the second 90° as constant pitch and continuously decreasing bank. During…

  • Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns › Climbing Turns

    pitch attitude should be decreased smoothly and slowly to allow for the airspeed to increase. A loss of altitude may result if the pitch attitude is changed too rapidly without allowing the airspeed to increase proportionately. After the airplane ... established in level flight at a constant altitude, climb power should be retained temporarily so that the airplane accelerates to the cruise airspeed. When the airspeed reaches the desired cruise airspeed, the throttle setting and the propeller control, if equipped…

  • Chapter 7, Section I: Airplane Basic Flight Maneuvers › Straight Climbs and Descents › Entry

    upward, continues to move slowly, and then stops at a rate appropriate to the stabilized airspeed and attitude. (Primary and supporting instruments for the climb entry are shown in Figure 7-25.) Figure 7-25. Climb entry for constant airspeed ... climb. Once the airplane stabilizes at a constant airspeed and attitude, the ASI is primary for pitch and the heading indicator remains primary for bank. [Figure 7-26] Monitor the tachometer or manifold pressure gauge as the primary power instrument…

  • Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns

    Normal climb speed is generally higher than the airplane’s best rate of climb. The additional airspeed provides for better engine cooling, greater control authority, and better visibility over the nose of the airplane. Normal climb is sometimes referred ... cruise climb. ⦁ Best rate of climb (VY)—produces the most altitude gained over a given amount of time. This airspeed is typically used when initially departing a runway without obstructions until it is safe to transition to a normal…

  • Chapter 7, Section II: Airplane Basic Flight Maneuvers › Straight Climbs and Descents › Constant Rate Climbs

    Constant Airspeed Climb from Established Airspeed In order to enter a constant airspeed climb, first complete the airspeed reduction from cruise airspeed to climb airspeed. Maintain straight-and-level flight as the airspeed is reduced. The entry to the climb ... similar to the entry from cruise airspeed with the exception that the power must be increased when the pitch attitude is raised. [Figure 7-64] Power added after the pitch change shows a decrease in airspeed due to the increased…