Specification for plate of titanium-aluminium-molybdenum-tin-silicon alloy (tensile strength 1030-1220 MPa) (maximum thickness 65 mm)
€172.00
Specification for aircraft material. High strength plywood for aircraft
€281.00
Specification for aircraft material. Ash
€99.00
Specification for mahogany for use in airscrews
Specification for plywood for aeronautical purposes
Specification for Sitka spruce as finished timber
Specification for Sitka spruce as rough timber
Specification for plate of titanium-copper alloy (tensile strength 520-640 MPa) (maximum thickness 10 mm)
Specification for sheet and strip of titanium-aluminium-vanadium alloy (tensile strength 920 MPa to 1180 MPa)
€85.00
Specification for braided linen (flax) cord for aerospace purposes
€80.00
Specification for sheet and strip of aluminium-manganese alloy (temper designation-O)
Specification for forging stock, bars, extruded sections and forgings of aluminium-2¼% magnesium alloy
Specification for sheet and strip of aluminium-manganese alloy (temper designation H16 or H26)
Specification for sheet and strip of aluminium-manganese alloy (temper designation H12 or H22)
Specification for ingots and castings of aluminium-silicon-magnesium alloy (solution treated and artificially aged) (Si 7, Mg 0.6)
