Specification for nickel-chromium-iron alloy sheet, strip and plate: annealed (Nickel base, Cr 15.5, Fe 8)
€165.00
Classification for pressure and temperature for fluid systems and components
Nickel-copper alloy sheet and strip: annealed (Nickel base, Cu 31)
Specification for nickel-chromium-cobalt-molybdenum-titanium-aluminium heat-resisting alloy sheet, strip and plate: softened (nickel base, Cr 18, Co 14, Mo 7, Ti 2.2, Al 2.1)
Specification for general requirements for construction and performance of airborne chemical oxygen generators
Specification for 2.5% nickel-chromium-molybdenum (high carbon) steel billets, bars, forgings and parts (1230-1420 MPa: limiting ruling section 150 mm)
Specification for cadmium-plated steel bolts (Unified hexagons and Unified threads) with close tolerance shanks for aircraft
Methods of test for self-locking nuts with maximum operating temperature greater than 425°C
€193.00
Specification for braided nylon cord with specified dimensional stability for aerospace purposes
€81.00
Specification for electric cables for general airframe or equipment interconnect use (260°C), wrapped insulation with nickel plated conductors
€269.00
Specification for coupling requirements for aircraft pressure fuelling connection
Secondary batteries for aircraft Specification lead-acid
Specification for pressure compensated variable delivery hydraulic pumps
Crimped joints for aircraft electrical cables and wires Specification design requirements (including tests) components tools
Specification for dimensions of omega clamps (saddle clamps) for fluid tubing installations
€95.00
