Specification for sheet and strip of aluminium-coated aluminium-copper-magnesium-silicon-manganese alloy (solution treated and aged at room temperature) (Cu 4.4, Mg 0.5, Si 0.8, Mn 0.8)
€165.00
Aerospace. Nuts, metric. Tolerances of form and position
€269.00
Specification for sheet and strip of commercially pure titanium (tensile strength 570-730 N/mm2)
Space systems. Structural design. Determination of loading levels for static qualification testing of launch vehicles
Procedure for inspection and testing of wrought titanium and titanium alloys
Air cargo equipment. Non-certified lower-deck containers for air transport. Specification and testing
€193.00
Qualification and approval of personnel for non-destructive testing
Aircraft de-icing/anti-icing methods with fluids
Aerospace. Constant displacement hydraulic motors. General specifications for 35000 kPa systems
€316.00
Aerospace. Hydraulic, pressure-compensated, variable delivery pumps. General requirements for 35000 kPa systems
Specification for sheet and strip of commercially pure titanium (tensile strength 390-540 N/mm2)
Specification for sheet and strip of commercially pure titanium (tensile strength 290-420 MPa)
Bolts, with MJ threads, made of heat-resistant nickel-based alloy, strength class 1 550 MPa. Procurement specification
Aerospace. MJ threads. Gauging
Nuts, self-locking, with maximum operating temperature less than or equal to 425°C. Test methods
