Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
€165.00
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
2½ per cent nickel-chromium-molybdenum steel (55/65 tonf/sq in: limiting ruling section 6 in)
Specification for flexible cotton rope for aeronautical purposes
Aluminium-copper-magnesium-silicon-manganese alloy tubes (solution treated and aged at room temperature)
This product is not for sale, please contact us for more information
Titanium Alloy, Sheet and Strip 4al 3mo 1v Solution Heat Treated
€68.00
Paper-hanging pastes and powders
€269.00
Rubber Or Synthetic Rubber Compounds Coolant Resistant (55-65)
75-ton chromium-molybdenum steel sheets and strips (65 ton 0.1 per cent proof stress) (suitable for welding)
Cold-rolled chromium-nickel steel sheets and strips (corrosion-resisting) (40 tons 0.1 per cent proof stress)
Chromium-nickel steel sheets and strips (13 ton 0.1 per cent proof stress)
€95.00
Carnation/rose boxes
chromium-molybdenum steel castings
Copper-silicon alloy rods, sections and forgings (for general engineering purposes)
