Increased load factors are a characteristic of all banked turns. Load factors become significant both to flight performance and to the load on wing structure as the bank increases beyond approximately 45°.
The yield factor of the average light plane is reached at a bank of approximately 70° to 75°, and approximately one-half at a bank of approximately 63° increases the stalling speed.
Brief and clear explanations of Aircraft Weight Control. This article describes about Aircraft Weight Control as a part of Aeronautical Knowledge Handbook.
AIRCRAFT SYSTEMS - OUTSIDE AIR TEMPERATURE GAUGE AND FUEL INJECTION SYSTEMS
OUTSIDE AIR TEMPERATURE GAUGE Most airplanes also are equipped with an outside air temperature (OAT) gauge calibrated in both degrees Celsi...
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The correct name for the tail section of an airplane is empennage. The empennage includes the entire tail group, consisting of fixed su...
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The control forces may be excessively high in some airplanes, and in order to decrease them, the manufacturer may use balance tabs. They loo...
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The fuselage includes the cabin and/or cockpit, which contains seats for the occupants and the controls for the airplane. In addition,...