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[Cites 0, Cited by 0] [Section 58(2)] [Section 58] [Entire Act]

Union of India - Subsection

Section 58(2)(b) in Aircraft Rules, 1937

(b)The load of an aircraft throughout a flight including take-off and landing shall be so distributed that the centre of gravity position of the aircraft falls within the limitations specified or approved by the Director-General: