The airplane is traveling in a straight line with a speed of $300 \mathrm{~km} / \mathrm{h}$, when the engines $A$ and $B$ produce a thrust of $T_{A}=40 \mathrm{kN}$ and $T_{B}=20 \mathrm{kN}$, respectively. Determine the angular velocity of the airplane in $t=5 \mathrm{~s}$. The plane has a mass of $200 \mathrm{Mg}$, its center of mass is located at $G$, and its radius of gyration about $G$ is $k_{G}=15 \mathrm{~m}$.