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This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist.

To specify minimum requirements for Fuel Flowmeters for use primarily in reciprocating engine powered civil transport aircraft, the operation of which may subject the instruments to the environmental conditions specified in Section 3.3. This Aeronautical Standard covers two basic types of instruments, or combinations thereof, intended for use in indicating fuel consumption of aircraft engines as follows: TYPE I - Measure rate of flow of fuel used. TYPE II - Totalize amount of fuel consumed or remaining.
 

Document History

  1. SAE AS407E


    Fuel Flow Rate Measurement System

    • Most Recent
  2. SAE AS407D

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    viewing


    Fuel Flowmeters (Stabilized: Aug 2012)

    • Historical Version
  3. SAE AS 407C


    Fuel Flowmeters ( Reaffirmed: Feb 2008 )

    • Historical Version
  4. SAE AS 4075/1


    Optical Implementation Relating to the High Speed Ring Bus (HSRB) Standard

    • Historical Version