Step 1:
The acceleration of the aircraft can be determined using the equation of motion for polar coordinates, which is given by:
\[a = \sqrt{\ddot{r}^2 + (r\ddot{\theta})^2 + 2r\dot{r}\dot{\theta}}\]
Given that $\ddot{r}=14 \mathrm{ft} / \mathrm{sec}^{2}$, we
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