FH.VII.E.S11

From the FAA library

• Helicopter Flying Handbookp. 10-8
  Chapter 10: Advanced Flight Maneuvers › Slope Operations › Technique

  Technique Refer to Figure 10-6. At the termination of the approach, if necessary, move the helicopter slowly toward the slope, being careful not to turn the tail upslope. Position the helicopter across the slope at a stabilized hover headed ... touches the ground, hesitate momentarily in a level attitude, then apply slight lateral cyclic in the direction of the slope (frame 2). This holds the skid against the slope while the pilot continues lowering the downslope skid with the collective…

• Helicopter Flying Handbookp. 10-7
  Chapter 10: Advanced Flight Maneuvers › Slope Operations

  Slope Operations Prior to conducting any slope operations, be thoroughly familiar with the characteristics of dynamic rollover and mast bumping, which are discussed in Chapter 11, Helicopter Emergencies and Hazards. The approach to a slope is similar to the approach ... other landing area. During slope operations, make allowances for wind, barriers, and forced landing sites in case of engine failure. Since the slope may constitute an obstruction to wind passage, anticipate turbulence and downdrafts. Slope Landing A pilot usually lands…

• 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…

• Pilot's Handbook of Aeronautical Knowledgep. 6-8
  Chapter 6: Flight Controls › Flight Control Systems › V-Tail

  horizontal force is exerted in the opposite direction. [Figure 6-15] By pushing the left pedal, the rudder moves left. This alters the airflow around the vertical stabilizer/rudder and creates a sideward lift that moves the tail to the right ... movable surfaces, which are usually called ruddervators, are connected through a special linkage that allows the control wheel to move both surfaces simultaneously. On the other hand, displacement of the rudder pedals moves the surfaces differentially, thereby providing directional control…