相关题目
Absolute altitude is defined as （ ） ．
True altitude is defined as （ ） ．
（ ） is defined as pressure altitude corrected for non-standard temperature.
When the altimeter is adjusted to standard sea level atmospheric pressure of 29.92 in Hg, （ ） is displayed on the altimeter.
The altitude that the pilot reads directly from the altimeter when it is correctly adjusted to the local altimeter setting is （ ） ．
（ ） for the local flight area is essential to minimize altimeter errors.
（ ） is calibrated airspeed corrected for the compression of air at a particular altitude.
（ ） is defined as the actual speed of the airplane over the ground. It is true speed adjusted for wind.
TAS is defined as （ ） ．
The indicated airspeed corrected for installation and instrument errors is （ ） ．
