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SAE ARP1084A

Заменен
External Hydraulic Leakage for In-Service Components
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 °F (38 °C) temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual.
Тематика
Hydraulic control
Hydraulic drives
Tests and Testing
Electrohydraulics
Safety
Fly-by-wire control systems
Hydraulic systems
Hydraulic motors
Flight control systems
Fluid power systems
Fuel pumps
Hydraulic fittings
Flight control actuators
Sensors and actuators
Flight management systems
Hydraulic equipment
Hydraulic fluids