AE50R, AE50RA
AE50RAB
Engine Manual
Doc. No. E1.01.0-E
Rev. 6 10-March-2011
Page 18-7
18.3.5 Temperature
Sensor
Air Temperature sensor
Supplied by Austro Engine GmbH and should be installed with its probe in the induction
airflow.
Rotor cooling air out temperature sensor
Supplied by Austro Engine GmbH and should be mounted in the rotor cooling air flow within
100mm or less downstream from outlet.
18.4 Fuel
System
18.4.1 Fuel
Specification
Refer to chapter 5.2.7
18.4.2 Fuel
delivery
No fuel pumps are provided by Austro Engine GmbH. Therefore electric pumps each capable
of delivering 45 liters an hour at working pressure.
18.4.3 Fuel
filters
No fuel filters are provided by Austro Engine GmbH. Therefore a filter of 40 microns or better
with a flow capacity of least 50 liters per hour at 0.1 bar pressure drop must be fitted in the fuel
delivery line after the pumps.
18.4.4 Pressure
Regulator
No fuel pressure regulator is supplied with this engine. It is the responsibility of the aircraft
manufacturer / installer to provide the engine with fuel regulated at working pressure.
18.4.5 Water in Fuel
The fuel system shall incorporate suitable means of isolating, removing, and checking for the
presence of water in the fuel system before each flight.
Summary of Contents for AE50R
Page 49: ......
