Eurocopter AS 350 83 Flight Manual page 178

FLIGHT MANUAL
.1~
The power takeoff on the MG8 permits a hydraulic p~ to be driven at
6000 rpm for a rotor speed of 386 rpm.
The drive is taken from the MGB spiral beve) gear wheel.
When the hydraulic pump runs dry the power taken must be less than 3 kW
so that the aircraft's performance data is not affected.
2 LIMITATIONS
The limitations laid down in the basic Flight Manual remain applicable
except for special limitations below:
.
-The maximum permissible power is 32 kW.
-When the hydraulic pump runs dry the power taken must be less than
3 kW so that the aircraft's performance data is not affected.
--Operation of the hydraulic pump (under load) is prohibited:
.in hover
.in climb
.in level flight at airspeeds below 30 knots (56 kmfh) and above
80 knots (148 kmfh).
3 EMERGENCY PROCEDURES
The emergency procedures laid down in the basic Flight Manual remain
applicable.
In the event of an engine failure, immediately shut down the power-driven
system.
4 NORMAL PROCEDURES
The normal procedures given in the basic Flight Manual remain applicable.
5 PERFORMANCE
.:-;:= data given in the basic Flight Manual remain applicable.
.
DGAC Approved: 35083 SUP.20
I A I B I C I F I 97-40 Page 1
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