Procedure for inspection and testing of textiles for aerospace purposes
€404.00
Aerospace series. Steel FE-PL1505 (15CrMoV6). Air melted. Hardened and tempered. Bars. De = 16 mm. 980 MPa = Rm = 1 180 MPa
€165.00
Aerospace series. Titanium alloy Ti-6Al-4V. Annealed. Sheet for superplastic forming. a = 6 mm
Aerospace series. Steel FE-PM1507 (X1CrNiMoAlTi12-11-2). Vacuum induction melted and consumable electrode remelted. Solution treated and precipitation treated. Bars. a or D = 200 mm. Rm = 1650 MPa
Aerospace series. Chloroprene rubber (CR). Heat resistance. Hardness 40 IRHD
Aerospace series. Chloroprene rubber (CR). Heat resistance. Hardness 50 IRHD
Aerospace series. Chloroprene rubber (CR). Heat resistance. Hardness 60 IRHD
Aerospace series. Steel X2NiCoMo18-8-5 (1.6359). Vacuum induction melted and vacuum arc remelted. Solution treated and precipitation treated. Bar. a or D = 150 mm. 1 750 MPa = Rm = 2 000 MPa
Aerospace series. Titanium alloy TI-P64001 (Ti-6Al-4V). Annealed. Sheet and strip, hot rolled. a = 6 mm
Aerospace series. Titanium alloy (Ti-6Al-4V). Annealed. Plate. 6 mm < a = 100 mm
Specification for nickel-chromium-cobalt-titanium-aluminiumheat-resistin g alloy billets, bars, forgings and parts (Nickel base, Cr19.5, Co 18.0 , Ti 2.5, Al 1.5)
€193.00
Aerospace series. Procedure for inspection, testing and acceptance of wrought heat-resisting alloys
€374.00
BS EN 4711. Aerospace series. Screw, 12-point flange head (bi hexagonal head bolt), long thread, for tensile applications, continuous fibre reinforced-PEEK composite, temperature range -65°C to 135°C. Inch series
€23.00
BS EN 4712. Aerospace series. Nuts, 12-point flange, self-locking, continuous fibre reinforced-PEEK composite, temperature range -65%0DC to 135°C. Inch series
BS EN 4713. Aerospace series. Nuts, anchor, self-locking, floating. Continuous fibre reinforced PEEK composite, temperature range -65°C to 135°C. Inch series
