Specification. 2½% nickel-chromium-molybdenum steel billets, bars, forgings and parts (880-1080 MPa: limiting ruling section 150 mm)
€165.00
Specification for pressure-driven machmeters for aircraft
Specification for pressure-driven airspeed indicators
Specification for precipitation hardening nickel base chromium-cobalt-molybdenum-titanium alloy precision castings (Cr 20, Co 20, Mo 6, Ti 2)
Specification for ingots and castings of aluminium-copper-nickel-manganese-titanium-zirconium-cobalt-antimony alloy (solution treated and artificially aged) (Cu 5.0, Ni 1.5, Mn 0.25, Ti 0.2, Zr 0.2, Co 0.2, Sb 0.2)
Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: not tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
Specification for tube of aluminium-magnesium-silicon-copper-chromium alloy (solution treated and artificially aged: tested hydraulically) (not exceeding 10 mm thickness) (Mg 1.0, Si 0.6, Cu 0.28, Cr 0.2)
Specification for general requirements for cockpit lighting controllers
Specification for dimensions of elastomeric toroidal sealing rings for aerospace use - inch series
Specification for elastomeric grommets (acrylonitrile-butadiene) for aerospace use
Specification for elastomeric grommets (polychloroprene) for aerospace use
Specification for permanent splicing of aircraft electrical cables
Specification for precipitaton hardening chromium-nickel-copper corrosion-resisting steel castings (1250-1500 MPa) (Cr 16, Ni 4, Cu 3)
Specification for 18% nickel maraging steel precision castings (1600-1850 MPa)
Specification for identification of aircraft servicing, maintenance, ground handling and safety/hazard points
