188 PUBLICATIONS AND DOCUMENTATION 1. Publications . The various publications issued for AN 32 aircraft are grouped in three categories, namely. (a).Publications issued by manufacturer. (b) Publications issued by Air Head Quarter.
32 OIL SYSTEM 1. Introduction. The engines have independent, self contained, short, closed loop oil lubrication system, which enables a continuous positive supply of oil under pressure for lubrication & heat dissipation at the heavy duty friction (e.g. Rotor
42 FUEL SYSTEM 1 Introduction. One of the prime concern of the designer in the aviation industry is to design a safe and reliable fuel system which can efficiently cater for the fuel requirements of the power plants at different power ratings on ground and under
143 ENGINE CONTROL. 1. Functions. AI20D series 5 engine control system are (a)Engine power rating control. (b)Engine shut down control. (c)Propeller feathering & un-feathering control. (d)Propeller pitch stop system control.