Problem $(50$ Points$)$

A static pressure port and a Pitot tube are used to estimate the flight speed of

a subsonic aircraft. The static pressure port reports that the aircraft is flying at an

altitude corresponding to a static pressure of $8\mathrm{.}30l\frac{b}{i}{n}^2.$

What are the pressure altitude $($ ft $),$ static temperature $,$ and static density

slug$/($:$f{t}^3$