If a blade requires more than a 15-degree tab bend from
0 in either direction, refer to the manufacturers
procedure for isolation of a defective blade.
i. If any adjustments have been made, perform the flight test again and verify the corrections.
j. Remove the AVA equipment from the aircraft.
k. Inventory AVA kit and adapter kit to ensure all parts are removed from the aircraft.
Figure 13. FLIGHT Flow Chart
Exit Vibration Analysis
Use Edit Adjustables to turn on trim
tab for hub with >12 mark pitch link