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After installation of a propeller, the engine must be ground run in order to check the propeller for correct function and operation. Aircraft propeller installations vary considerably, and no set testing procedure would be satisfactory for all aircraft. It is imperative, therefore, that any particular installation should be tested in accordance with the approved AMM procedure, which will normally include the following general requirements:
Note: If vibration was experienced during the engine run, the hub retaining nut should be re-tightened after the engine shaft has cooled down.
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Explain with the aid of sketch of zeroth law of thermodynamics
4+9/4z +z/4 divided by 1+1/4z-z/8
Convert the following reduced bearings to whole circle bearings: N.36°16’E; (b) S.28° 14’ E. (c) S.47°26’W and (d) N.58°24’W
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Centrifugal flow - Compressors in Aircraft: The centrifugal impeller is rotated at high speed by the turbine and centrifugal action causes the air between the impeller vanes to
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