AP.III.C.R3
Risk managementDirectional control following a rejected takeoff.
From the FAA library
- Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Takeoff Performance
Figure 11-19 illustrates the general effect of wind by the percent change in takeoff or landing distance as a function of the ratio of wind velocity to takeoff or landing speed. The effect of proper takeoff speed is especially ... important when runway lengths and takeoff distances are critical. The takeoff speeds specified in the AFM/POH are generally the minimum safe speeds at which the aircraft can become airborne. Any attempt to take off below the recommended speed means that…
- Chapter 11: Aircraft Performance › Takeoff and Landing Performance
Takeoff and Landing Performance The majority of pilot-caused aircraft accidents occur during the takeoff and landing phase of flight. Because of this fact, the pilot must be familiar with all the variables that influence the takeoff and landing performance ... aircraft and must strive for exacting, professional procedures of operation during these phases of flight. Takeoff and landing performance is a condition of accelerated and decelerated motion. For instance, during takeoff an aircraft starts at zero speed and accelerates…
- Chapter 16: Transition to Jet-Powered Airplanes › Jet Airplane Takeoff and Climb › Rejected Takeoff
shown that the initial tendency of a flight crew is to use normal after-landing braking during a rejected takeoff. Delaying the intervention of the primary deceleration force during an RTO maneuver, when every second counts, increases stopping distance. Instead ... braking immediately while simultaneously retarding the throttles, with spoiler extension and thrust reverser deployment following in short sequence. Differential braking applied to maintain directional control also diminishes the effectiveness of the brakes. A blown tire will eliminate any kind…
- Chapter 6: Takeoffs and Departure Climbs › Rejected Takeoff/Engine Failure
event a takeoff is rejected, the power is reduced to idle and maximum braking applied while maintaining directional control. If it is necessary to shut down the engine due to a fire, the mixture control should be brought ... idle cutoff position and the magnetos turned off. In all cases, the manufacturer’s emergency procedure should be followed. Urgency characterizes all power loss or engine failure occurrences after lift-off. In most instances, the pilot has only…
- 14 CFR § 91.1705 Required pilot training.
following flight training maneuver profiles applicable to the MU-2B model being trained: (i) Normal takeoff with 5- and 20- degrees flaps; (ii) Takeoff engine failure with 5- and 20- degrees flaps; (iii) Takeoff engine failure on runway or rejected ... takeoff; (iv) Takeoff engine failure after liftoff—unable to climb (may be completed in classroom or flight training device only); (v) Steep turns; (vi) Slow flight maneuvers; (vii) One engine inoperative maneuvering with loss of directional control; (viii) Approach…