The mass of a CRT is not more than 600 g. The sensitivity to deviation along the X axis is 17.6-18.5 mm / A, and along the Y axis it is 17.0-17.8 mm / A. The inductance of the deflecting coils in the X and Y axes is not more than 80 μH. The resonant frequency of the coil deviations of at least 3 MHz.

The tubes work in harsh climatic conditions with high mechanical loads. Operating temperature range from -600 to + 850C.

A CRT as part of an optoelectronic aviation indicator forms a collimated luminous image of symbolic navigation and flight information and special information against the background of the cabin space.