SAE AS415-1964
Altimeter, Pressure, Compensated (Turbine Powered Subsonic Aircraft) R(1991)

Standard No.
SAE AS415-1964
Release Date
1964
Published By
Society of Automotive Engineers (SAE)
Status
 2008-02
Replace By
SAE AS415-1997
Latest
SAE AS415-2008
Scope
This Aerospace Standard establishes the essential minimum safe performance standards for Pressure Actuated Compensated Altimeters, primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in paragraph 3.3. This Aerospace Standard covers two types of compensated altimeters which indicate, by visual means, the pressure altitude compensated for the static pressure system errors of the aircraft. TYPE I - Range: - 1,000 to 30,000 feet. Barometric pressure - scale range: at least 28.1 - 30.99 in. Hg (952-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude. TYPE II - Range: - 1,000 to 60,000 feet. Barometric pressure - scale range: at least 28.1 - 30.99 in. Hg (952-1049 millibars). May include markers working in conjunction with the Barometric Pressure Scale to indicate pressure altitude.

SAE AS415-1964 Referenced Document

SAE AS415-1964 history

  • 2008 SAE AS415-2008 Altimeter, Pressure, Compensated (Turbine Powered Subsonic Aircraft)
  • 1997 SAE AS415-1997 Altimeter@ Pressure@ Compensated (Turbine Powered Subsonic Aircraft)
  • 1964 SAE AS415-1964 Altimeter, Pressure, Compensated (Turbine Powered Subsonic Aircraft) R(1991)
  • 1940 SAE AS415-5-1940 AS415 Bolt Assembly. - Attachment of Lead-Acid Accumulator



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