Final answer:
The critical Angle of Attack (AOA) remains constant at different altitudes, so at 5000', the critical AOA would still be 15 degrees.
Step-by-step explanation:
The critical Angle of Attack (AOA) is not directly affected by altitude. It is a characteristic of the wing's aerodynamic properties. However, the air density decreases with altitude, which means that an aircraft must fly at a higher true airspeed to generate the same amount of lift at higher altitudes. A higher true airspeed would mean that the indicated angle of attack where the airflow separates from the wing (resulting in a stall) remains the same. Therefore, the critical AOA at 5000' would be the same as at 1000', which is 15 degrees.