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The Sioux is a single-engine single-rotor three-seat observation and basic training helicopter. In 1953 the Bell 47G design was introduced. In 1953 the Bell 47G design was introduced. It can be recognized by the full "soap bubble" canopy (as its designer Arthur M. Young termed it), [ 7 ] exposed welded-tube tail boom, saddle fuel tanks and skid ...
The helicopter was unveiled at the 2013 Paris Airshow on June 17, 2013, as the Bell SLS (Short Light Single). The model designation was later announced at HAI Heli-Expo 2014 in Anaheim, California on February 25, 2014. [2] [3] [4] The Bell 505 is a "clean sheet" design, but uses some dynamic components, such as the rotor system, [5] of the Bell ...
Parachute Riggers/Packers in training attend the 15-day Basic Parachute qualification course at CFB Trenton, and then for approximately 2.5–3 years undertake three different 45-day courses that cover maintaining parachutes, packing parachutes, and quality control of parachutes.
Helicopter Training Squadron EIGHT (HT-8) is a United States Navy helicopter training squadron based at Naval Air Station Whiting Field in Milton, FL. [1] The squadron's mission is helicopter pilot training for U. S. Navy, U. S. Marine Corps and U. S. Coast Guard Student Naval Aviators and for selected foreign military flight students from basic helicopter flight training through winging.
Location of flight controls in a helicopter. Helicopter flight controls are used to achieve and maintain controlled aerodynamic helicopter flight. [1] Changes to the aircraft flight control system transmit mechanically to the rotor, producing aerodynamic effects on the rotor blades that make the helicopter move in a desired way.
A Bell XH-40, a prototype of the UH-1 and Bell 204. Bell designed its Model 204 in response to a 1955 United States Army requirement for a utility helicopter. The 204 was a giant step forward in helicopter design, being one of the first to be powered by a turboshaft.
The following table includes a list of helicopter models that are designed to carry underslung loads. [3] Cargo capacities provided reflect the airframe manufacturer's specifications; when put into practice the actual maximum load capacities may be less, depending on the rating of the cargo hook equipment.
This category is intended for equipment that is associated specifically with the operation of helicopters but is not a component of the helicopter required for the function of flight (e.g. rotors, engines, controls).