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.
Status: WithdrawnPublication date: 1990-02
Edition: 1Number of pages: 18
Technical Committee: ISO/TC 20/SC 10 Aerospace fluid systems and components
- ICS :
- 49.080 Aerospace fluid systems and components
ISO 9206:1990Stage: 95.99
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