Aerospace. Linear hydraulic utility actuator. General specifications seo-ignore and tested in accordance with

and tested in accordance with the component manufacturer’s

The test shall be carried out within a temperature range of 10 °C to 35 °C

inlet valve

– the limits of the voltages due to the electromagnetic interference

Why should you use ISO 8102‑6 - Electrical requirements for lifts

Aerospace. Linear hydraulic utility actuator. General specifications seo-ignore and tested in accordance withWhat is ISO 18387 Linear hydraulic utility actuator about ? ISO 18387 establishes the general requirements for a linear hydraulic utility actuator, herein referred to as a "utility actuator", for use in flight vehicle hydraulic systems at pressures up to 35000 kPa (5000 psi). These requirements include: Design requirements Test requirements. ISO 18387 is intended to be used in conjunction with the detailed specification that is particular to each