Eurocopter AS 350 83 Flight Manual page 64

FLIGHT MANUAL'
2.1 Red 1iQhts (Cont'd)
LIGHT FAILURE PILOT ACTION 4It
MANU mode engaged -Store the flight data.
GOV or
Governing failure: the fuel f10~ -Unlock the "FLIGHT" notch, the
is frozen at the value prior to fuel flow can be increased or
failure. decreased by turning the
twist grip.
-Only apply small amplitude
adjustments, synchronized
with the collective pitch
control in order to maintain
.
NR in the green range.
-Fly the approach at 40 kt and
adjust the fuel flow rate to
maintain NR within the upper
section of the green range.
Slowly reduce the speed if
necessary adjust the fuel flow
rate slightly on the twist
grip to maintain NR within the
green range.
On final approach, when the
collective pitch is increased
on reaching the hover, let the
NR drop for touchdown. After
touchdown, reduce the fuel
flow rate before lowering the
collective pitch.
NOTE: This failure can also
result in loss of ~Ng
and torque parameters on '
.
the VEMD. Refer to
paragraph 3.3 for
compliance with
limitations.
Return from MANU mode to AUTO -The AUTO/MANU selector can be
mode. replaced in the AUTO position
irrespective of the NR value.
Then return the control to the
FLIGHT notch (red and amber
GOV and TWT GRP warning lights
should be extinguished).
.
DGAC Approved: 350 83 ~.~
I A I 8 I C I D I FIG I 97-40 Page 4