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FLIGHT MANUAL
.'
I RR 2F I
2.1
Red lights
(Cont'
d)
tt
The text
of paragraph
(VOYANT GOV) ,is
to be replaced
by the following
text:
LIGHT
FAILURE
PILOT ACTION
-Check
Flight
parameters.
MANU mode engaged
GOV
-Maintain
NR in green arc.
Or
-unlock
the
"FLIGHT"
detent,the
Governing
failure:
the
fuel
fuel
flow
can
be
increased
or
flow is
frozen
at the value
decreased
by turning
the
prior
to
failure.
twist
grip.
-Only
apply
small
amplitude
tt
adjustments,
synchronized
with
the
collective
pitch
I
con~rol
in order
to maintainI
NR ln 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
tt
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
-The
AUTO/MANU selector
can be
AUTO mode.
set
back
to
the
AUTO position
irrespective
of
the
NR value.
Then return
the control
to the
FLIGHT detent
(red and amber
GOV and TWT GRP warning
lights
should
be extinguished).
.
DGAC Approved:
350 83
3.3
IAI
ICICI
IFIG1
02-14
Page
4
11'\1
\'-'\U
I
\r
I~I
'RR'
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