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
