0075 00TM 1-6625-724-13&P0075 00-20NOTEIf a blade requires more than a 15-degree tab bend from0 in either direction, refer to the manufacturer’sprocedure 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 ChartFLIGHT MEASUREMENTSWithinLimits?YESExit Vibration AnalysisNOMake AVA-recommendedadjustmentsUse Edit Adjustables to turn on trimtab for hub with >12 mark pitch linkadjustmentYESNOAVA Defaultsolution >12marks forpitch link?
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