Due to an unequal distribution of fuel in the wing tanks, the centers of gravity for the airplane fuselage $A$ and wings $B$ and $C$ are located as shown. If these components have weights $W_{A}=45000 \mathrm{lb}, \quad W_{B}=8000 \mathrm{lb}, \quad$ and
$W_{C}=6000 \mathrm{lb},$ determine the normal reactions of the wheels $D, E,$ and $F$ on the ground.