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THE AIRCRAFT RULES, 1937 - Ministry of Civil Aviation

THE AIRCRAFT RULES, 1937 - Ministry of Civil Aviation

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Section WStudent Flight Engineer’s Licence1. Requirements for the issue <strong>of</strong> licence— An applicant for a Student Flight Engineer’sLicence shall satisfy the following requirements—(a) Age— He shall not be less than twenty-one years <strong>of</strong> age on the date <strong>of</strong>application.(b) Educational Qualifications— He shall have passed class ten plus two withPhysics and Mathematics or its equivalent form a recognisedBoard/University.(c) Medical Fitness— He shall produce on a prescribed pr<strong>of</strong>orma a certificate<strong>of</strong> physical fitness from an approval Medical Board after undergoing amedical examination during which he shall have established his medicalfitness on the basis <strong>of</strong> compliance with the requirements as notified by theDirector-General under Rule 39B.(d) Technical Qualification— He shall have completed a Flight Engineer’sGround Course <strong>of</strong> Instructions in the basic technical and aeronauticalknowledge required <strong>of</strong> a Flight Engineer as approved by the Director-General.(e) Knowledge— Subject to the successful completion <strong>of</strong> the coursementioned in clause (d) above, he shall pass a written examination in thefollowing subjects—(i) Regulations and procedures, including rules, in so far as duties <strong>of</strong>flight engineers are concerned;(ii) Fundamental <strong>of</strong> aerodynamics and theory <strong>of</strong> flight and navigation;(iii) General principles <strong>of</strong> constructions, maintenance and functioning<strong>of</strong> airframe, power plants, including their accessories, instruments,installed equipment and related systems;(iv) Selected elements <strong>of</strong> flight planning, including centre <strong>of</strong> gravitycomputation, fuel consumption and endurance, power plant output andcentre <strong>of</strong> power output, engine power curves and mathematicalcomputation involved;(v) Aircraft performance characteristics and limitations;(vi) Flight documentation relating to the duties <strong>of</strong> flight engineers;(vii) Procedures in the event <strong>of</strong> power plant or system malfunction oremergencies particularly in the event <strong>of</strong> fire;

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