$26$ A large transport aircraf is making a level landing, as shown in Fig. P$2\mathrm{.}6.$ The gross weight of the aircrall is $150,000lb,$ and its pitching mass moment of inertia is $50{11}^{N}lb*$ in $*s^2$ about the center of gravity. The landing rear$-$wheel reaction is $350,000$ tb at an angle of $15$ with the vertical. Determine whether passenger $A$ or $B$ will receive the most load. Assume that each passenger weights $170$ lb and neglect the airplane lif.

Figure P$2\mathrm{.}6$