HYDRAULIC SYSTEM FOR THE BELL 214ST HELICOPTER


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HYDRAULIC SYSTEM FOR THE BELL 214ST HELICOPTER
HYDRAULIC SYSTEM FOR THE BELL 214ST HELICOPTERThe hydraulic power systems on the Bell 214ST helicopter consist of three separate and independent systems: two flight-control hydraulic systems, called PC1 and PC2, and a utility hydraulic system. The two flight-control systems operate in parallel, so that if either system should fail, the remaining system will provide full control capabilities. The utility system is used only to power the cooling fan for the gearbox and transmission oil cooler. Each system is equipped with a pump, closed-circuit reservoir, hydraulic module, distribution circuit, and ground test circuit.The hydraulic power for each system is generated by its own variable-displacement hydraulic pump. The PC1 pump is powered by …
Citation
Michael J. Kroes; Ronald Sterkenburg: Aircraft Maintenance & Repair, Seventh Edition. HYDRAULIC SYSTEM FOR THE BELL 214ST HELICOPTER, Chapter (McGraw-Hill Professional, 2013), AccessEngineering Export