22-02. (H) MEASURMENT OF AIR DATA PARAMETERS
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1. With EAS and density altitude, we can deduce:
2. The advantages provided by an air data computer to indicate the altitude are:
1) Position/pressure error correction.
2) Density error correction.
3) Remote data transmission capability.
4) Capability of operating as a conventional altimeter in the event of a failure.
The combination of correct statements is:
3. The total air temperature (TAT) is always:
4. With a pitot probe blocked due to ice buildup, the aircraft airspeed indicator will indicate in descent a:
5. Assume non-pressurized aircraft. A leak in the pressure line from the pitot tube will affect the airspeed indicator in the following way: