ACES SYSTEMS Cobra II, Руководство пользователя

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Gen II
User Manual
8-4 – Tail Rotor Balance Chapter 8 Revision 3.00, April 2020

Press the [

] key and select the chart type by pressing the [

] key. The type of chart
for this example is “Irregular”. See paragraph 8.8.1 for more information on chart
type “Regular” and paragraph 8.8.2 for chart type “Irregular”.

Press the [

] key and enter the number of weight positions using the keypad. This
example uses 4 weight positions.

Press the [

] key and enter the first weight position name as “TARGET”. Using the
[

] key to change fields, enter the influence co-efficient for this location as “0.60”
grams adjustment per “1.0” IPS vibration, and the move line of “5:45” using the
keypad.

Press the [

] key and enter the second weight position name of “A”. Using the [

]
key to change fields, enter the influence co-efficient for this location as “5.0” grams
adjustment per “1.0” IPS vibration, and the move line of “10:00” using the keypad.

Press the [

] key and enter the third weight position name of “BLANK”. Using the
[

] key to change fields, enter the influence co-efficient for this location as “0.60”
grams adjustment per “1.0” IPS vibration, and the move line of “11:45” using the
keypad.

Press the [

] key and enter the fourth weight position name of “B”. Using the [

] key
to change fields, enter the influence co-efficient for this location as “5.0” grams
adjustment per “1.0” IPS vibration, and the move line of “4:00” using the keypad.
When completed, press [OK] to save the setup.
8.2. – Multiple Condition Setups
The following paragraphs will describe the process for building multiple condition setups for
tail rotor balance. Multiple condition setups are used for aircraft that require balancing at
more than one speed and may have more than one balance chart.
Follow the steps below to complete the tail rotor setup screen for “Multiple Conditions” as
shown.