Test methods for transparent materials for aircraft glazing - Part 4 : Determination of ultraviolet light transmission over the wavelength range 280

Heat resisting alloys produced from atomized powder - Powder compacted forging stock and parts - Technical specification : Part 1 : General

Aerospace series - Connectors, electrical, circular, coupled by threaded ring, fire-resistant or non fire-resistant, operating temperatures - 65 deg C to 175

Heat Resisting Steel FE-PM38 -- 1000MPa <or= Rm <or= 1140MPa - Forgings - Aerospace SeriesData Sheet by ASD-STAN Standardization, 06/01/1981

Aerospace series - Steel X3CrNiMoAl 13-8-2 - Vacuum induction melted and consumable electrode remelted - Solution treated and precipitation treated - Bars

Non-metallic materials - Foaming structural adhesive films - Test method - Part 3: Expansion ratio and volatile contentData Sheet by ASD-STAN Standardization,

Aluminium alloy 2017A-T3 - clad sheet and strip - 0,4 <or= a <or= 6 mmData Sheet by ASD-STAN Standardization, 05/01/1985

Aluminium alloy 2024- T3510 - drawn bar a <or= 75 mmData Sheet by ASD-STAN Standardization, 05/01/1985

Aerospace series - Chloroprene rubber (CR)Heat resistance - Hardness 40 IRHDData Sheet by ASD-STAN Standardization, 07/31/2011

Sealants -- Test methods -- Determination of low-temperature flexibilityData Sheet by ASD-STAN Standardization, 06/30/2000

Titanium alloy TI-P65002 - Not heat treated -- Grade 2 forging stock, for solution treated and aged forgings - a or D

Heat resisting nickel base alloy (Ni-P100HT) - cold worked and softened - Bar and wire for continuous forging or extrusion for fasteners