• ARP1084
• Revision: A

• 2013-10-04

• A-6a1 Commercial Aircraft Committee

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.

• SAE ARP 1084

• Aerospace

• Flight control systems
• Flight control actuators
• Fly-by-wire control systems
• Flight management systems
• Sensors and Actuators
• Fluid power systems
• Hydraulic systems
• Electrohydraulics
• Hydraulic control
• Hydraulic drives
• Hydraulic equipment
• Hydraulic fittings
• Hydraulic fluids
• Hydraulic motors
• Fuel pumps
• Safety
• Tests and Testing