This Volume contains plotted trim data obtained from the Boeing Vertol Tandem Rotor Trim and Stability Analysis Program (A-97) for the CH-46E helicopter. Data for the following flight regimes are presented: Level flight; Maximum power climb and autorotation; Constant altitude sideslips; and Sideward flight. For each flight regime considered, the four cockpit control positions, plus helicopter pitch and roll attitudes, are plotted vs. airspeed or sideslip angle.


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