AI.V.F.S5

From the FAA library

• Airplane Flying Handbookp. 16-12
  Chapter 16: Transition to Jet-Powered Airplanes › Jet Airplane Takeoff and Climb › Takeoff Roll

  speed used during certification at which the critical engine is assumed to fail. ⦁ VR —rotation speed, or speed at which the rotation of the airplane is initiated to takeoff attitude. This speed cannot be less than V1 or less than ... VMCA (minimum control speed in the air). On a single-engine takeoff, it also allows for the acceleration to V2 at the 35-foot height at the end of the runway. ⦁ VLOF —lift-off speed, or speed at which…

• Airplane Flying Handbookp. 16-12
  Chapter 16: Transition to Jet-Powered Airplanes › Jet Airplane Takeoff and Climb › V-Speeds

  Airplane Takeoff and Climb The following information is generic in nature and, since most civilian jet airplanes require a minimum flight crew of two pilots, assumes a two-pilot crew. If any of the following information conflicts with FAA-approved ... procedures for a particular airplane, the AFM procedures take precedence. Also, if any of the following procedures differ from the FAA-approved procedures developed for use by a specific air operator and/or for use in an FAA-approved training center…

• Airplane Flying Handbookp. 2-21
  Chapter 2: Ground Operations › Before-Takeoff Check

  airplane is properly positioned for the run-up, it should be allowed to roll forward slightly to ensure that the nosewheel or tailwheel is in alignment with the longitudinal axis of the airplane. While performing the before-takeoff check ... accordance with the airplane’s AFM/POH, the pilot divides attention between the inside and outside of the airplane. If the parking brake slips, or if application of the toe brakes is inadequate for the amount of power applied, the airplane…

• Airplane Flying Handbookp. 13-11
  Chapter 13: Transition to Multiengine Airplanes › Performance and Limitations

  highest altitude at which the airplane can maintain a steady rate of climb of 100 fpm with both engines operating. The airplane has reached its absolute ceiling when climb is no longer possible. ⦁ The single-engine service ceiling is reached ... when the multiengine airplane can no longer maintain a 50 fpm rate of climb with OEI, and its single-engine absolute ceiling when climb is no longer possible. The takeoff in a multiengine airplane should be planned in sufficient detail…

• Airplane Flying Handbookp. 15-12
  Chapter 15: Transition to Turbopropeller-Powered Airplanes › Operational Considerations

  preceded by unusually high initial fuel flow, which may be the first indication the pilot has that the engine start is not proceeding normally. Serious engine damage occurs if the hot start is allowed to continue. A condition where ... engine is accelerating more slowly than normal is termed a hung start or false start. During a hung start/false start, the engine may stabilize at an engine rpm that is not high enough for the engine to continue…

• Airplane Flying Handbookp. 6-3
  Chapter 6: Takeoffs and Departure Climbs › Normal Takeoff › Takeoff Roll

  pilot should also ensure that the takeoff surfaces are firm and of sufficient length to permit the airplane to gradually accelerate to normal lift-off and climb-out speed, and there are no obstructions along the takeoff path. There ... reasons for making a takeoff as nearly into the wind as possible. First, since the airplane depends on airspeed, a headwind provides some of that airspeed even before the airplane begins to accelerate into the wind. Second, a headwind decreases…