PA.IV.I.S9

From the FAA library

• Airplane Flying Handbookp. 3-17
  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…

• Airplane Flying Handbookp. 3-19
  Chapter 3: Basic Flight Maneuvers › Climbs and Climbing Turns › Establishing a Climb

  Establishing a Climb A straight climb is entered by gently increasing back pressure on the elevator flight control to the pitch attitude referencing the airplane’s nose to the natural horizon while simultaneously increasing engine power to the climb power ... setting. The wingtips should be referenced in maintaining the climb attitude while cross-checking the flight instruments to verify performance. In many airplanes, as power is increased, an increase in slipstream over the horizontal stabilizer causes the airplane’s pitch…

• Airplane Flying Handbookp. 6-13
  Chapter 6: Takeoffs and Departure Climbs › Soft/Rough-Field Takeoff and Climb › Initial Climb

  Initial Climb After a positive rate of climb is established, and the airplane has accelerated to VY, the pilot should retract the landing gear and flaps, if equipped. If departing from an airstrip with wet snow or slush ... event an obstacle needs to be cleared after a soft-field takeoff, the pilot should perform the climb-out at VX until the obstacle has been cleared. The pilot should then adjust the pitch attitude to VY and retract…

• Airplane Flying Handbookp. 3-20
  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…

• Instrument Flying Handbookp. 8-10
  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…

• Instrument Flying Handbookp. 7-14
  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…