Aerospace. Linear hydraulic utility actuator. General specifications seo-ignore NOTE 3 For an explanation

NOTE 3 For an explanation of the case for material efficiency including the financial

on which travels a carriage from which a bucket is suspended: used in carrying persons heavy construction work

Compression ignition engines

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

Aerospace. Linear hydraulic utility actuator. General specifications seo-ignore NOTE 3 For an explanationWhat 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