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Full Description

This Aerospace Standard covers one type of maximum-allowable-airspeed instrument which gives a continuous indication of both indicated airspeed and maximum allowable airspeed not exceeding 650 knots.

This Aerospace Standard establishes the essential minimum safe performance standards for pitot-static type of maximum-allowable-airspeed instruments primarily for use with turbine powered subsonic transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3.
 

Document History

  1. SAE AS437B


    Maximum-Allowable-Airspeed Instruments (Turbine Powered Subsonic Aircraft) (Stabilized: Dec 2020)

    • Most Recent
  2. SAE AS4372C


    Performance Requirements for Wire, Electric, Insulated Copper or Copper Alloy

    • Historical Version
  3. SAE AS437A

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    MAXIMUM-ALLOWABLE-AIRSPEED INSTRUMENTS (TURBINE POWERED SUBSONIC AIRCRAFT)

    • Historical Version