Specification for harmonized system of quality assessment for electronic components. Blank detail specification: electromechanical switches for use in electronic equipment. Blank detail specification for pushbutton switches
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Harmonized system of quality assessment for electronic components. Electromechanical switches for use in electronic equipment. Sectional specification for in-line package switches
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Quality management handbook.-Part 1: Quality assurance, Part 2: Reliability and maintainability
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Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (titanium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
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Specification for aircraft material. 23/14 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
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Specification for aircraft material. 24/17 chromium-nickel heat-resisting steel (niobium stabilized) (35 tonf/sq in: limiting ruling section 6 in)
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Specification for aircraft material. 3 per cent chromium-molybdenum-vanadium steel (air hardening) (100 tonf/sq in: limiting ruling section 1 1/8 inches)
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Specification for 3 per cent chromium-molybdenum-vanadium steel (vacuum remelted - air hardening) (157 kgf/mm<sup>2</sup> (100 tonf/in<sup>2</sup>): limiting ruling section 30 mm (1⅛ in))
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Specification for chromium-nickel-molybdenum-vanadium heat-resisting steel billets, bars, forgings and parts (930-1130 MPa: limiting ruling section 150 mm) (Cr 12, Ni 2.5, Mo 1.7, V 0.3)
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