ocr: DDD vectored thrust tilting arm from pivot (ft, jets equipped point to prop hub DD enter 0) TILT-ROTOR BLADE UEFLECTIUNS OR THRUST DECTOR DECTOR UEFLELTIUNS cyclic pitch change with full pitch detiection (degrees, always (prop planes only) enter positive) cyclic pitch change with full roll detlection (degrees, always (prop planes only) enter positive) PUFFERS with full pitch pitch moment detiection B00DD B0DDDD enter (ft-Ib, positive) always roll moment BDDDDD (ft-lb, always with full roll deflection B0DDDD enter positive) with full yaw yaw moment detiection a00DDD F00DDD enter (ft-lb, positiv ...
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