Q. What are the tubes in the aircraft that carry the air pressure to the instruments is called as?

View solution

Q. What is the difference between the static pressure and the stagnation pressure when the aircraft is stationary?

View solution

Q. The impact pressure and the dynamic pressure are the same.

View solution

Q. At supersonic speeds, a normal pitot tube cannot be used for speed measurements.

View solution

Q. Which of the following instruments use the pitot-static probe for its input?

View solution

Q. What is the temperature of the air surrounding the aircraft called as?

View solution

Q. What is the temperature measured by a probe on the exterior of a moving aircraft?

View solution

Q. Why is a hole required at the rear end of the temperature probe?

View solution

Q. Which is the optimum place for a temperature probe?

View solution

Q. The recovery factor for computing the static temperature does not account for _____

View solution

Q. The temperature is probe is actually an electric coil whose resistance varies with temperature.

View solution

Q. What error will a 10°C error in temperature shown in true airspeed?

View solution

Q. The angle between the relative wind and the longitudinal datum line on the fuselage is called as?

View solution

Q. Which flight critical system is the angle of attack indicator a part of?

View solution

Q. Sideslip sensors are only used in experimental aircraft and not in general aviation or commercial aircraft.

View solution

Q. Which of the following is used to obtain the altitude from the static pressure?

View solution

Q. What is the height called when the standard temperatures are used?

View solution

Q. Which of the following altitude is measured by the pitot-static tube?

View solution

Q. Why is it dangerous to fly over hilly areas with pressure altitude?

View solution

Q. What does the altitude rate essentially tell us?

View solution