Abstract

Establishes informations for motors to be installed in aircraft, which transform hydraulic power into mechanical energy in the form of a rotational torque. Primary and secondary function motors are covered. Actuators with internal rotation angle limits and low-speed motors are not covered. Shall be used in conjunction with the detail specification particular to each application.


General information 

  • Status
     :  Withdrawn
    Publication date
     : 1990-02
  • Edition
     : 1
    Number of pages
     : 18
  • Technical Committee
     : ISO/TC 20/SC 10 Aerospace fluid systems and components
  • ICS
     :
    49.080 Aerospace fluid systems and components

Life cycle


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