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  • Chapter 9: Basic Flight Maneuvers › Hovering—Rearward Flight › Technique

    Common Errors 1. Exaggerated movement of the cyclic, resulting in overcontrolling and erratic movement over the surface. 2. Failure to use proper antitorque pedal control, resulting in excessive heading change. 3. Failure to maintain desired hovering height. 4. Failure ... maintain proper rpm. 5. Failure to make sure the area is clear prior to starting the maneuver. Hovering—Rearward Flight Rearward hovering flight may be necessary to move the helicopter to a specific area when the situation is such that…

  • Chapter 9: Basic Flight Maneuvers › The Four Fundamentals › Guidelines

    Guidelines Good practices to follow during maneuvering flight include: 1. Move the cyclic only as fast as trim, torque, and rotor speed can be maintained. When entering a maneuver and the trim, rotor, or torque reacts quicker than anticipated, pilot ... limitations have been exceeded. If continued, an aircraft limitation will be exceeded. Perform the maneuver with less intensity until all aspects of the machine can be controlled. The pilot must be aware of the sensitivity of the flight controls…

  • Chapter 9: Basic Flight Maneuvers › Hovering—Sideward Flight › Technique

    straight ground track, use two reference points in line and at some distance in front of the helicopter. Failure to use proper antitorque pedal control, resulting in excessive heading change. 3. Failure to maintain desired hovering height. 4. Failure ... maintain proper rpm. 5. Failure to maintain alignment with direction of travel. Hovering—Sideward Flight Sideward hovering flight may be necessary to move the helicopter to a specific area when conditions make it impossible to use forward flight. During…

  • Chapter 11: Helicopter Emergencies and Hazards › Recovery Technique (Uncontrolled Right Yaw) › Main Drive Shaft or Clutch Failure

    Main Drive Shaft or Clutch Failure The main drive shaft, located between the engine and the main rotor transmission, provides engine power to the main rotor transmission. In some helicopters, particularly those with piston engines, a drive belt is used ... instead of a drive shaft. A failure of the drive shaft clutch or belt has the same effect as an engine failure because power is no longer provided to the main rotor and an autorotation must be initiated. There…

  • Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Antitorque System Failure

    antitorque failure with a high-power setting at a low airspeed results in a severe spinning to the right. At low power settings and high airspeeds, the spin is less severe. High airspeeds tend to streamline the helicopter and keep ... from spinning. If a tail rotor failure occurs, power must be reduced in order to reduce main rotor torque. The techniques differ depending on whether the helicopter is in flight or in a hover, but ultimately require an autorotation…

  • 14 CFR Part 121, Appendix E to Part 121—Flight Training Requirements

    gusts if practicable under the existing meteorological, airport, and traffic conditions | I, T, U, C (e) Maneuvering to a landing with simulated powerplant failure, as follows: (1) For 3-engine airplanes, maneuvering to a landing with an approved procedure that ... outboard engine) | I, C | T, U (2) For other multiengine airplanes, maneuvering to a landing with a simulated failure of 50 percent of available powerplants with the simulated loss of power on one side of the airplane…