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This Standard applies to all temperature instruments used in aircraft applications and environments. The word "instrument" as used in this Standard encompasses only the display device and does not include the temperature sensors. Examples of the types of instruments covered are as follows:

This Aerospace Standard covers two basic types of temperature instruments as follows:

This Aerospace Recommended Practice covers the design and installation requirements for pitot-static systems.

This Aerospace Standard covers a direct reading magnetic compass.

This Aeronautical Standard covers two basic types of temperature instruments as follows:

This document is limited to units meeting the definitions of para. 1.3 and covers the following general class of synchros:

This Aeronautical Standard covers two basic types of temperature indicators as follows: TYPE I - Ratiometer type actuated by changes of electrical resistance of a temperature sensing electrical resistance element; the resistance changes being obtained by temperature changes of the temperature sensing resistance element. TYPE II - Millivoltmeter type, operated and actuated by varying e.m.f. output of a thermocouple, the varying e.m.f. input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.

This specification covers two types of instruments. These instruments are for the purpose of measuring temperature, such as those of oil coolant, carburetor air, free air and cylinder head.

This specification covers minimum requirements for gyroscopically stabilized (or integrated) magnetic direction indicators for use in aircraft.

This specification covers two basic types as follows: Type I - Direct Reading Type II - Remote Indicating