Temperature Instruments (Reciprocating Engine Powered Aircraft)
- Aerospace Standard
- Reaf. Nonc.
|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 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.|
|Aerospace Standard||Pressure Instruments - Fuel, Oil and Hydraulic (Reciprocating Engine Powered Aircraft)|
|Aerospace Standard||AIRSPEED INDICATOR (PITOT STATIC) (RECIPROCATING ENGINE POWERED AIRCRAFT)|
|Aerospace Standard||ALTIMETER, PRESSURE ACTUATED SENSITIVE TYPE|
Data Sets - Support Documents
|Unnamed Dataset 1|
|TABLE I||TEMPERATURE VS RESISTANCE CHARACTERISTICS - AIRCRAFT THERMOMETER BULBS|
The A-4 Committee is responsible for mechanical, electromechanical and electronic cockpit instrumentation standards applicable to all civil aircraft, with emphasis on minimum performance standards intended for reference in the Federal Aviation Administration (FAA) Technical Standard Orders (TSO).A list of the technical reports developed by the A-4 Committee can be obtained by searching on 'aircraft instruments' and selecting 'standards', from the SAE Home Page. A-4 Standards For additional information about the A-4 Committee or SAE, contact Maureen Lemankiewicz email@example.com Let us contact you about suitable committee participation opportunities. Advise us of an industry issue for an SAE Technical Committee.