ACES SYSTEMS Cobra II - Main Rotor Adjustment Symbol and Solution Logic Screen

Gen II User Manual
7-8 – Main Rotor Track & Balance Chapter 7 Revision 3.00, Apr 2020
The last example shows one lateral chart and two track adjustment ID entries. The lateral
measurements for both Ground and Hover will be averaged, with the solution based on this
average. The recorded track split for Ground and Hover will be averaged with one solution based
on this average. The recorded track split for FLT 80 and FLT 120 will also be averaged with a
second solution based on this average. This is an example of a setup for use on an aircraft that
requires pitch change link adjustment for ground and hover visual track, then trim tab adjustment
based on visual track in forward flight.
When you have completed the conditions setup screen, press [OK] to accept and continue.
Proceed to paragraph 7.1.4 below for the next main rotor setup screen.
7.1.4. – Main Rotor Adjustment Symbol and Solution Logic Setup Screen