Figure 23. Effect of Pitch Link Change on vertical 1/REV (AH-64D)

Figure 20. Lateral Effect for WEIGHT Changes (AH-64A)

Figure 24. Effect of Tab 4-10 Change on vertical 1/REV (AH-64D)

TM-1-6625-724-13P Aviation Vibration Analyzer Manual
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TM 1-6625-724-13&P 0071 00 0071 00-43 Figure 22. Effect of Pitch Link Change on Lateral 1/REV (AH-64D) Figure 23. Effect of Pitch Link Change on vertical 1/REV (AH-64D) 140 Knots

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