Aerospace series. Steel and heat resisting alloys. Wrought products. Technical specification Bars sections
€299.00
Aerospace series. Aluminium alloy 2024 T3510. Drawn bar. a < 75 mm
€165.00
Aerospace series. Aluminium alloy 2014A T6. Tubes for structures. 0,6 mm < a < 12,5 mm
Aerospace series. Steel X7CrNiAl17-7 (1.4568). Air melted. Solution treated and precipitation hardened. Sheet and strip. a = 6 mm. 1 240 MPa = Rm = 1 450 MPa
Aerospace series. Nuts, hexagon, plain, reduced height, reduced across flats, in heat resisting steel, silver plated, left hand thread. Classification: 600 MPa (at ambient temperature) / 425 °C
BS EN 4869-001. Aerospace series. Expanded beam termini, fibre optic non physical contact in 3645 standard cavities Part 001. Technical specification
€23.00
BS EN 4869-101. Aerospace series. Expanded beam termini, fibre optic non physical contact in 3645 standard cavities Part 101. Male termini size 16 technical specification
BS EN 4869-102. Aerospace series. Expanded beam termini, fibre optic non physical contact in 3645 standard cavities Part 102. Female termini size 16 technical specification
BS EN 4869-103. Aerospace series. Expanded beam termini, fibre optic non physical contact in 3645 standard cavities Part 103. Male termini size 12 technical specification
BS EN 4869-104. Aerospace series. Expanded beam termini, fibre optic non physical contact in 3645 standard cavities Part 104. Female termini size 12 technical specification
Aerospace series. Heat resisting nickel base alloy NI-P96-HT. Cold drawn and precipitation treated. Wire. D = 10 mm
Aerospace series. Steel FE-PM1503 (X3CrNiMoAl 13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar for machining. a or D = 150 mm. 1 200 MPa = Rm = 1 400 MPa
Aerospace series. Electrical cables, installation. Protection sleeves. Test methods Mark adherence and print permanence
Aerospace series. Steel FE-PM1506 (X5CrNiMoAl13-8-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bar. a or D = 150 mm. Rm = 1400 MPa
Aerospace series. Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb).Solution treated, forging De = 200 mm
