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Helicopter Section
HOVERING PITCH (PHV)
This function trims the pitch near the hovering
point. By setting a range, adjustment is possible
without changing the high and low points. This
Hovering pitch setting can be made for each flight
condition,
but
is
commonly
used
for
Normal
flight
condition.
At initial definition, the left sliding lever con-
trols hovering pitch volume.
Activation of command
In the Condition Menu, press the
PHV
key to get the
PIT HOVER menu shown below. Use the A key to
activate mode setting, then press the ACT or INH
keys ( F and G) to activate or inhibit the function.
Mode setting
Hovering Throttle
trim volume setting
Return to
Condition
screen
Trim deflection
setting
Range setting
Rate setting
Mode selection
Hovering Pitch Trim Deflection Setting
Press the
B
key to allow input to this setting, and
input the rate with the numeric keys F to M . The
deflection may be set from 0 to 100% (the initial value of
this parameter is defined to be 100%).
Setting of Range
Now you will set the Range of travel over which
HIGH/LOW
sides
do
not
change.
Press
the
Ckey
and
set
the
rate
with
the numeric
keys F to M
.
The
Range
may
be set from 0 to 100% (when activated, the initial value of
this parameter is defined to be 100%).
Offset Rate Setting
The offset amount is entered by pressing the D key,
and
input
with
the numeric
keys E to M
.
This may be
input from -100 to +100%, and the initial value is
programmed to 0%.
Hovering Pitch Trim Selection and Operation Direction
Setting
Call up the volume setting screen by pressing the
VOL O
key. Set the volume control as desired (the
left-side slider is set as the pitch trim volume control
initially). For a description of the volume setting method,
see page 37).
Precautions
When the range is set to 100%. the rate changes be-
tween points 1 and 13. When the range is set to 0%, the
rate changes only between points 6 and 8. When you use
this function, set up the numbers so that when the range
is small, the trim deflection is also small, and make sure
that the preceding and following points are not exceeded
when the range is moved to its maximum position.
Helicopter Section, Page 105
29


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