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The auxiliary gear is in the form of a nose or tail wheel installation, almost invariably the former, especially in large aircraft. 2. The advantages of tricycle landing gear during ground operation are: (i) No risk of the aircraft ‘nosing over’ during hard braking. (ii) Better visibility for the pilot during taxiing. (iii) Less likelihood of ground looping during take-off or landing in cross-wind conditions. 3. The landing gear contains shock absorbers to withstand the landing forces and the effects of taxiing over uneven surfaces, and brakes to stop and assist in controlling the aircraft on the ground.

3. The landing gear contains shock absorbers to withstand the landing forces and the effects of taxiing over uneven surfaces, and brakes to stop and assist in controlling the aircraft on the ground. Most modern aircraft with tricycle (nose-wheel) layouts are equipped with nose-wheel steering for ground manoeuvring, some very large aircraft also have main wheel steering (known as body steering). In aircraft designed for flight at high speeds/altitudes the landing gear is retracted into the fuselage or wings in flight, to reduce profile drag.

FIGURE 1-23 Internal Balance Chapter 1 Page 39 © G LONGHURST 1999 All Rights Reserved Worldwide Airframe and Systems Balance Tab 80. Like the inset hinge and the horn balance the balance tab serves the purpose of reducing the stick forces involved in moving a primary control surface, at a given airspeed. A balance tab is shown at Figure 1-24. As the primary control surface moves one way, so the balance tab moves the other. Since the tab is a considerable distance from the hinge line of the primary control, the moment produced by it is large.

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Airframe & Systems Tutorial - PPSC


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