PA.VIII.B.S2
SkillClimb at a constant airspeed to specific altitudes in straight flight and turns.
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 8: Helicopter Attitude Instrument Flying › Straight Climbs (Constant Airspeed and Constant Rate) › Entry
Entry To enter a constant airspeed climb from cruise airspeed when the climb speed is lower than cruise speed, simultaneously increase power to the climb power setting and adjust pitch attitude to the approximate climb attitude. A helicopter ... have an exact “climb attitude.” To slow down to climb (versus cruise) airspeed, the nose must be raised. Depending on power and horizontal stabilizer configuration and effectiveness, the nose may be level during an established climb or slightly nose high…