Browse Standards AS414B
Current Reaffirmed 2008-02-16

Temperature Instruments (Turbine Powered Subsonic Aircraft)(NONCURRENT Nov 1996) AS414B

This SAE Aerospace Standard (AS) covers two basic types of temperature instruments as follows: type I: ratiometer type, actuated by changes in 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 EMF output of a thermocouple; the varying EMF input to the instrument being obtained by temperature changes of the temperature sensing thermocouple.

This document establishes the essential minimum safe performance standards for electrical type temperature instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4.

AS414B
2008-02-16
Latest
Reaffirmed
AS414A
1969-12-01
Historical
Revised
AS414
1961-06-01
Historical
Issued

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