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
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Status: WithdrawnPublication date: 1990-02Stage: Withdrawal of International Standard [95.99]
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Edition: 1Number of pages: 18
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Technical Committee :ISO/TC 20/SC 10ICS :49.080
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Life cycle
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Now
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Revised by
WithdrawnISO 9206:2016