FH.II.D.K13

From the FAA library

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

  collective to manipulate rotor pitch and anti-torque pedals to control yaw. [Figure 6-3] For additional information on flight control systems, refer to the appropriate handbook for information related to the flight control systems and characteristics of specific types…

• Helicopter Flying Handbookp. 11-18
  Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Loss of Tail Rotor Effectiveness (LTE)

  There are no extra parts in helicopters. The respect and discipline pilots…

• Helicopter Flying Handbookp. 4-8
  Chapter 4: Helicopter Components, Sections, and Systems › Antitorque System › NOTAR®

  likely to come into contact with people or objects. [Figure 4-14] NOTAR® Using the natural characteristics of helicopter aerodynamics, the NOTAR® antitorque system provides safe, quiet, responsive, foreign object damage (FOD) resistant directional control. The enclosed variable-pitch composite ... called the Coanda effect. The result is that the tailboom becomes a “wing,” flying in the downwash of the rotor system, producing up to 60 percent of the antitorque required in a hover. The balance of the directional control…

• Helicopter Flying Handbookp. 11-20
  Chapter 11: Helicopter Emergencies and Hazards › System Malfunctions › Tail Rotor Vortex Ring State (210–330°)

  Weathercock Stability (120–240°) In this region, the helicopter attempts to weathervane…

• Pilot's Handbook of Aeronautical Knowledge Addendum (MOSAIC)p. 4
  A Note About Light Sport Category Aircraft

  attitude. It should be noted that flight control systems and characteristics can vary greatly depending on the type of aircraft flown. The most basic flight control system designs are mechanical and date back to early aircraft. They operate with ... variety of flight control systems. For example, some aircraft utilized by sport pilots rely on shifting weight while hot-air balloons use a standard burn technique. Helicopters utilize a cyclic to tilt the rotor in the desired direction, along with…

• 14 CFR Part 135 — Operating Requirements: Commuter and on Demand Operations and Rules Governing Persons on Board Such AircraftOpen
  14 CFR Part 135, Appendix C to Part 135—Helicopter Flight Recorder Specifications

  Resolution 250 fpm below 12,000 ft. indicated | 1 | 250 fpm below 12,000. Engine Power, Each Engine Main rotor speed | Maximum range | ±5% | 1 | 1% 2 Free or power turbine | Maximum range | + 5% | 1 | 1% 2 Engine torque | Maximum ... sources are aircraft instruments (except altimeters) of acceptable quality to fly the aircraft the recording system excluding these sensors (but including all other characteristics of the recording system) shall contribute no more than half of the values in this column…