Results
Q1. The pressure measured at the forward facing orifice of a pitot tube is the:
total pressure.
Q2. If the pitot tube is clogged, which instrument(s) is/are affected?
Airspeed indicator only.
Q3. A pitot blockage of both the ram air input and the drain hole with the static port open causes the airspeed indicator to:
react like an altimeter.
Q4. When the OAT is +25°C, the deviation from standard temperature for aerodynamic computations is:
+10°C
Q5. Total air pressure consists of static pressure plus:
Dynamic pressure.
Q6. A pitot tube covered by ice which blocks the ram air inlet will affect the following instrument (s):
airspeed indicator only.
Q7. Which instrument does not connect to the static system?
Vacuum gauge.
Q8. In a standard atmosphere and at the sea level, the calibrated airspeed (CAS) is:
equal to the true airspeed (TAS).
Q9. A pitot tube covered by ice which blocks the ram air inlet will affect the following instrument (s):
airspeed indicator only.
Q10. The pitot tube supplies:
Impact pressure.
Q11. In a non-pressurized aircraft, if one or several static pressure ports are damaged, there is an ultimate emergency means for restoring a practically correct static pressure intake:
breaking the rate-of-climb indicator glass window
Q12. The atmospheric pressure at FL 70 in a “standard +10” atmosphere is:
781.85 hPa.
Q13. What corrections must be applied to indicated airspeed to produce true airspeed?
Correction for altitude and temperature.
Q14. A pitot blockage of both the ram air input and the drain hole with the static port open causes the airspeed indicator to:
react like an altimeter.
Q15. If the alternate static source is used, the resulting reading will be:
Too high reading of altitude.
