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About This Item

 

Full Description

To establish an orientation standard for aircraft gas turbine engines and their component parts. Orientation of the engine, engine axis and coordinate system referred to herein shall be the conventional terminology used in all references to aircraft gas turbine engines. Numbering as provided herein is intended for convenience in locating a particular unit in a group of like or similar units.
 

Document History

  1. SAE ARP2C


    Horsepower Correction Formulae (Stabilized: Aug 2018)

    • Most Recent
  2. SAE ARP2B


    Horsepower Correction Formulae

    • Historical Version
  3. SAE ARP246C

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    Orientation of Engine Axis, Coordinate and Numbering Systems for Aircraft Gas Turbine Engines

    • Historical Version
  4. SAE ARP210


    Definition of Commonly Used Day Types (Atmospheric Ambient Temperature Characteristics Versus Pressure Altitude)

    • Historical Version
  5. SAE ARP24D


    Determination of Hydraulic Pressure Drop

    • Historical Version