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ASSIGNMENT 4-Cont. - 14014_96
ASSIGNMENT 4-Cont. - 14014_98

Airman - Aviation theories and other practices
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4-29. The spars are designed with extra strength to combat which of the following forces? 1. Torsion 2. Bending 3. Tension 4. Compression 4-30. What parts of an aircraft wing transmit the load from the skin covering to the spars? 1. Formers 2. Stringers 3. False spars 4. Ribs 4-31. What is the purpose of the false spar in some aircraft wings? 1. To support the ailerons and flaps 2. To give the wings bending strength 3. To help transmit the air load from the wing 4. To help carry the load 4-32. The term   wet wing   is used to describe what construction feature? 1. How water drains from the surface 2. Fuel cells installed in the wing 3. How water is used to balance the wing 4. Oil tanks installed in the wing 4-33. The flight control surfaces on a simple wing include what controls? 1. Edge flaps and ailerons 2. Trailing and leading edge flaps 3. Ailerons and leading edge flaps 4. Ailerons and trailing edge flaps 4-34. The empennage of the aircraft consists of which of the following sections? 1. Wings and tail 2. Speed brakes, spoilers, and flaps 3. Vertical and horizontal stabilizers, rudder, and elevators 4. Ribs, spars, and skin 4-35. What is the primary function of the stabilizers? 1. To provide drag for the aircraft 2. To control the direction of flight 3. To balance the weight of the wings 4. To keep the aircraft flying straight and level 4-36. What surfaces maintain directional stability in an aircraft? 1. The rudder 2. The elevators 3. The vertical stabilizer 4. The horizontal stabilizer 4-37. What are the three groups of flight control surfaces? 1. Main, ancillary, and optional 2. Primary, secondary, and optional 3. Primary, secondary, and auxiliary 4. Primary, secondary, and tertiary 4-38. Ailerons, elevators, and rudders make up what group of aircraft control surfaces? 1. Primary 2. Auxiliary 3. Optional 4. Secondary 4-39. The ailerons control what motion of the aircraft? 1. Pitch 2. Roll 3. Yaw 4. Skid 4-40. Elevators are used to control what aspects of flight? 1. Motion about the vertical axis 2. Motion about the lateral axis 3. Forward flight 4. Landing or takeoff 4-41. Where  are  the  elevator  control  surfaces located? 1. Trailing edge of the wings 2. Horizontal stabilizer 3. Lower surface of the fuselage 4. Vertical stabilizer 4-42. Where are the rudder control surfaces located? 1. Trailing edge of the wings 2. Horizontal stabilizer 3. Lower surfaces of the fuselage 4. Vertical stabilizer 4-43. What assembly operates the ailerons and elevators on a multiengine fixed–wing aircraft? 1. Yoke and wheel assembly 2. Control stick assembly 3. Stock and shaft assembly 4. Steering and shaft assembly 4-25







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