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SAE AS414 Rev B

Temperature Instruments (Turbine Powered Subsonic Aircraft)
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SAE AS414 Rev B

Temperature Instruments (Turbine Powered Subsonic Aircraft)

PUBLISH DATE 1996
PAGES 16
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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.
SDO SAE: SAE International
Document Number AS414
Publication Date Sept. 1, 1996
Language en - English
Page Count 16
Revision Level B
Supercedes
Committee
Publish Date Document Id Type View
Sept. 1, 1996 AS414B Revision
Nov. 30, 1970 AS414-7 Revision
Dec. 1, 1969 AS414A Revision
June 1, 1961 AS414 Revision