Assembly and Rigging Unit 3 exam

8212. The auxiliary (tail) rotor of a helicopter permits the pilot to compensate for and/or accomplish which of the following?

8213. The vertical flight of a helicopter is controlled by

8214. A reduction in ani-torque thrust will cause the

8215. In rotorcraft external-loading, the ideal location of the cargo release is where the line of action passes

8216. The acute angle formed by the chord line of a wing and the relative wind is known as the

8217. A helicopter in forward flight, cruise configuration, changes direction by

8218. The purpose in checking main rotor blade tracking is to determine the

8219. In a hovering helicopter equipped with a tail rotor, directional controls is maintained by

8220. if a single-rotor helicopter is in foward horizontal flight, the angle of attack of the advancing blade is

8221. Main rotor blades that do not cone by the same amount during rotaiton are said to be out of

8222. One purpose of the freewhelling unit required between the engine and the helicopter transmission is to

8223. Which statement is correct concerning torque effect on helicpoters?

8224. What is the pupose of the free-wheeling unit in a helicopter drive system?

8225. Movement about the longitudinal axis (roll) in a helicopter is effected by movement of the

8226. Movemetn about the lateral axis (pitch) in a helicopter is effected by movement of the