This specification defines the requirements for a PTFE lined, non-metallic, aramid reinforced assembly suitable for use to 275°F and to 4000 lbf/in2 (27 500 kPa) aircraft and missile hydraulic and pneumatic systems.
SAE AS1975-1988 history
2016SAE AS1975G-2016 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
2015SAE AS1975F-2015 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
2013SAE AS1975SUP1-2013 Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems (Supplement 1)
2013SAE AS1975E-2013 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
2008SAE AS1975D-2008 Hose Assembly@ Polytetrafluoroethylene@ Para-Aramid Reinforced@ 3000/4000 psi@ 275 °F@ Standard Duty@ Hydraulic@ Aircraft Systems
2007SAE AS1975C-2007 Hose Assembly, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
2001SAE AS1975C-2001 Hose Assemblies, Polytetrafluoroethylene, Para-Aramid Reinforced, 3000/4000 psi, 275 °F, Standard Duty, Hydraulic, Aircraft Systems
1994SAE AS1975B-1994 Hose Assemblies@ Polytetrafluoroethylene@ Aramid Reinforced@ 275 Degrees F@ Standard Duty@ 4000/3000 psi@ Hydraulic@ Aircraft Systems
1992SAE AS1975A-1992 HOSE ASSEMBLIES, POLYTETRAFLUOROETHYLENE, ARAMID REINFORCED, 275 °F, STANDARD DUTY, 4000/3000 lbf/in2, HYDRAULIC, AIRCRAFT SYSTEMS