SAE AS413B-1969
Temperature Instruments (Reciprocating Engine Powered Aircraft)
- Standard No.
- SAE AS413B-1969
- Release Date
- 1969
- Published By
- Society of Automotive Engineers (SAE)
- Status
- Replace By
- SAE AS413B-2008
- Latest
- SAE AS413B-2008
- 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.
SAE AS413B-1969 Referenced Document
- SAE ARP582 Lighting, Integral, for Aircraft Instruments; Criteria for Design
- SAE ARP798-1965 Design Criteria for White Incandescent Lighted Aerospace Instruments
- SAE AS425 AS425 Bottom Bracket - Parachute Stowage
SAE AS413B-1969 history
- 2008 SAE AS413B-2008 Temperature Instruments (Reciprocating Engine Powered Aircraft)
- 1969 SAE AS413B-1969 Temperature Instruments (Reciprocating Engine Powered Aircraft)
- 1954 SAE AS413A-1954 TEMPERATURE INDICATOR
- 1948 SAE AS413-1948 TEMPERATURE INDICATOR
- 1940 SAE AS413-4-1940 AS413 Valve Lifter for Fuel Drain Valve
