SAE AS413A

Temperature Instruments (Reciprocating Engine Powered Aircraft).

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Standard:
  • AS413
  • Revision: A
Revised:
  • 1954-12-01
Revision:
  • Historical. Access the latest revision: AS413B
Issuing:
  • A-4 Aircraft Instruments Committee
Scope:

This Aerospace Standard establishes the minimum sage performance standards for electrical type temperature instruments primarily for use with reciprocating engine powered transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.4. This Aerospace Standard covers two basic types of temperature instruments as follows: TYPE I Radiometer 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 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.

History:
StandardPublishedRevisionStatus
AS413B1969-12-01LatestReaffirmed
AS413A1954-12-01HistoricalRevised
AS4131948-11-01HistoricalIssued
AKA:
  • SAE AS 413
Sector:
  • Aerospace
Topic:
  • Avionics
  • Aircraft instruments
  • Aircraft displays
  • Flight control systems
  • Flight management systems
  • Displays
  • Smoke detection
  • Instrument panels
  • Parts
  • Safety
  • Fire detection
  • Tests and Testing

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