THE S‐3A VEHICLE is equipped with 2 completely independent hydraulic systems which have been designated as the combined flight control/utility system. These systems are both structurally and hydraulically isolated from each other and are designed and installed in accordance with spec. MIL‐H‐5440 type II (−65° to 275°F temperature range) class 3000 (cutout pressure at pump is 3,100psi).
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