AE50R, AE50RA
AE50RAB
Engine Manual
Doc. No. E1.01.01-E Rev. 6 10-March-2011 Page 6-3
6.3.3 Liquid Coolant Temperature Limits
Maximum for Take–off 90 °C
Minimum for Take–off 60 °C
Maximum continuous 100 °C
6.3.4 Rotor Cooling Air Outlet Temperature Limits
Maximum for Take–off (3 minutes) 120 °C
Maximum Continuous 110 °C
6.3.5 Exhaust Gas Temperature (EGT)
Maximum Exhaust Gas Temperature 950 °C
6.3.6 Fuel Pressure
min 0.276 bar (4 psi)
max 0.414 bar (6 psi)
6.3.7 Altitude
The engine has been tested for use up to 14.000 ft pressure altitude
6.4 Manuals
Operation / Maintenance / Installation Doc. No. E1.01.01–E
Overhaul Manual Doc. No. E1.04.01–E