SAE AS414B PDF
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TEMPERATURE INSTRUMENTS (TURBINE POWERED SUBSONIC AIRCRAFT)(NONCURRENT Nov 1996)
Description
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.
Revision History
Related Info
AS414B
2008-02-16
Latest
Reaffirmed
AS414A
1969-12-01
Historical
Revised
AS414
1961-06-01
Historical
Issued
DOI: https://doi.org/10.4271/AS414B
Issuing Committee:
A-4 Aircraft Instruments Committee
Publisher:
SAE International
Pages: 16
Related Topics:
Pressure
Aircraft instruments
Humidity
Electronic equipment
Conductivity
Identification numbers
Drag
Aircraft
Performance tests
Also known as: SAE AS 414
History
| AS414B | 2008-02-16 | Latest | Reaffirmed |
| AS414A | 1969-12-01 | Historical | Revised |
| AS414 | 1961-06-01 | Historical | Issued |
| ISSUING COMMITTEE | A-4 Aircraft Instruments Committee |
|---|---|
| DATE | 2008-02-16 |
| DOI | |
| ISCURRENT | Current |
| PAGE | 16 |
| PUBLISHER | SAE International |
| REVISED | REAF. NONC. |
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