Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm2 (100 tonf/in2): limiting ruling section 30 mm (1? in))
€165.00
Specification for patented cold drawn carbon steel wire and springs (high duty unground wire)
Specification for patented cold drawn carbon steel wire and springs (high duty ground wire)
Specification for carbon steel wire and springs (high duty unground wire - hardened and tempered)
Specification for chromium-vanadium steel wire and springs (high duty ground wire - hardened and tempered)
Specification for test pieces and methods metallic materials. Tensile tests - elevated temperature. Metric units
Magnesium-aluminium-zinc alloy forging stock and forgings
This product is not for sale, please contact us for more information
Specification for plywood for aeronautical purposes
€95.00
Titanium Alloy, Bars and Forgings 2cr 2fe 2mo Annealed, 120,000 Psi Yield
€68.00
Titanium Alloy, Bars and Forgings 5zr 5al 5sn Annealed
Test pieces and test methods for metallic materials for aircraft. Metric units
€193.00
Specification for phenolic mouldings for aeronautical purposes
€81.00
Aluminum Alloy, Tubing, Seamless, Drawn (6062 T6)
Specification for aircraft material. ¾ per cent nickel-chromium case-hardening steel
Specification for aircraft material. Manganese-molybdenum steel (55/65 tonf/sq in: limiting ruling section 2½ inches)
