• MA2079

• 1988-01-01

• G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

This aerospace standard covers hose assemblies intended for use in aircraft high temperature fluid systems. The specified temperature range is -55--C (-67--F) to +204--C (400--F). Operating pressures are listed in Table 1. The assemblies shall be of the following types: Type I - non-conductive inner tube; and Type II - conductive inner tube. The hose assemblies shall be of the following classes: Class 1 - liquid proof test; and Class 2 - pneumatic proof test.

• SAE MA 2079

• Aerospace

• Parts
• Hoses
• Hydraulic systems
• Crashworthiness
• Certification