HI.VIII.E.S6

From the FAA library

• Pilot's Handbook of Aeronautical Knowledgep. 11-14
  Chapter 11: Aircraft Performance › Takeoff and Landing Performance › Takeoff Performance

  margin above stall and provides satisfactory control and initial ROC. Generally, the lift-off speed is some fixed percentage of the stall speed or minimum control speed for the aircraft in the takeoff configuration. As such, the lift ... stall speed or minimum control speed. To obtain minimum takeoff distance at the specific lift-off speed, the forces that act on the aircraft must provide the maximum acceleration during the takeoff roll. The various forces acting on the aircraft…

• Helicopter Flying Handbookp. 11-14
  Chapter 11: Helicopter Emergencies and Hazards › Low-G Conditions and Mast Bumping

  control of fuselage attitude but may not immediately realize it. Tail rotor thrust or other aerodynamic factors will often induce a roll. The pilot still has control of the rotor disk, and may instinctively try to correct the roll ... been the cause of numerous military and civilian fatal accidents. It was initially encountered during nap-of-the-earth flying, a very low-altitude tactical flight technique used by the military where the aircraft flies following the contours…

• Pilot's Handbook of Aeronautical Knowledgep. 6-2
  Chapter 6: Flight Controls › Flight Control Systems › Primary Flight Controls

  Flight Control Systems Flight Controls Aircraft flight control systems consist of primary and secondary systems. The ailerons, elevator (or stabilator), and rudder constitute the primary control system and are required to control an aircraft safely during flight. Wing flaps, leading ... edge devices, spoilers, and trim systems constitute the secondary control system and improve the performance characteristics of the airplane or relieve the pilot of excessive control forces. Primary Flight Controls Aircraft control systems are carefully designed to provide adequate responsiveness…

• Helicopter Flying Handbookp. 11-13
  Chapter 11: Helicopter Emergencies and Hazards › Dynamic Rollover › Slope Takeoffs and Landings

  Slope Takeoffs and Landings During slope operations, excessive application of cyclic control into the slope, together with excessive collective pitch control, can result in the downslope skid or landing wheel rising sufficiently to exceed lateral cyclic control limits ... upslope rolling motion can occur. [Figure 11-6] When performing slope takeoff and landing maneuvers, follow the published procedures and keep the roll rates small. Slowly raise the downslope skid or wheel to bring the helicopter level, and then lift…

• Airplane Flying Handbookp. 6-9
  Chapter 6: Takeoffs and Departure Climbs › Crosswind Takeoff › Initial Climb

  taxiing onto the active runway. ⦁ Using less than full aileron pressure into the wind initially on the takeoff roll. ⦁ Mechanical use of aileron control rather than judging lateral position of airplane on runway from visual clues and applying sufficient aileron ... runway. ⦁ Side-skipping due to improper aileron application. ⦁ Inadequate rudder control to maintain airplane parallel to centerline and pointed straight ahead in alignment with visual references. ⦁ Excessive aileron input in the latter stage of the takeoff roll resulting…

• Airplane Flying Handbookp. 13-31
  Chapter 13: Transition to Multiengine Airplanes › Low Altitude Engine Failure Scenarios › Control

  Landing gear up—adequate climb performance. Control The first consideration following engine failure during takeoff is to maintain control of the airplane. Maintaining directional control with prompt and often aggressive rudder application and STOPPING THE YAW is critical ... maximum of 10° of bank toward the operative engine should be used initially to stop the yaw and maintain directional control. This initial bank input is held only momentarily, just long enough to establish or ensure directional control. Climb performance…