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  • Status :  Withdrawn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
  • :
    ISO/TC 20/SC 10
    Aerospace fluid systems and components
  • 49.080
    Aerospace fluid systems and components

Got a question?

Check out our FAQs

Customer care
+41 22 749 08 88

Opening hours:
Monday to Friday - 09:00-12:00, 14:00-17:00 (UTC+1)

Keep up to date with ISO

Sign up to our newsletter for the latest news, views and product information.