49.045 : Structure and structure elements

ASTM E3188-19

ASTM E3188-19

Superseded Historical

Standard Terminology for Aircraft Braking Performance

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ASTM F3409-19

ASTM F3409-19

Superseded Historical

Standard Practice for Simplified Aircraft Loads Determination

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ASTM F3310-18

ASTM F3310-18

Superseded Historical

Standard Specification for Non-Essential Ice Detectors for Aircraft

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ASTM F428-19

ASTM F428-19

Superseded Historical

Standard Test Method for Intensity of Scratches on Aerospace Glass Enclosures

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ASTM F548-19

ASTM F548-19

Superseded Historical

Standard Test Method for Intensity of Scratches on Aerospace Transparent Plastics

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BS EN 2851:1992

BS EN 2851:1992

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Marking of parts and assemblies other than engines. Indications on drawings

€165.00

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BS EN 2155-2:1993

BS EN 2155-2:1993

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Specification for test methods transparent materials aircraft glazing Determination of water absorption

€165.00

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BS EN 2155-3:1993

BS EN 2155-3:1993

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Specification for test methods transparent materials aircraft glazing Determination of refractive index

€165.00

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BS EN 2155-13:1993

BS EN 2155-13:1993

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Test methods for transparent materials aircraft glazing Determination of temperature at deflection under load

€165.00

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BS EN 2155-14:1993

BS EN 2155-14:1993

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Test methods for transparent materials aircraft glazing Determination of the 1/10 Vicat softening temperature

€165.00

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BS EN 2155-19:1997

BS EN 2155-19:1997

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Specification for test methods transparent materials aircraft glazing Determination of craze resistance

€165.00

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BS M 91:1997

BS M 91:1997

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Aircraft. Methodology of calculating cargo compartment volumes

€193.00

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BS EN 2258:1997

BS EN 2258:1997

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Circular tubes for fluids in aluminium and aluminium alloys. Diameter 3,2 mm = D = 100 mm. Thickness 0,6 mm = a = 2,5 mm. Dimensions

€165.00

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BS EN 2257:1997

BS EN 2257:1997

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Circular tubes for structures in aluminium and aluminium alloys. Diameter 6 mm = D = 100 mm. Thickness 1 mm = a = 6 mm. Dimensions

€165.00

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BS EN 2155-12:1997

BS EN 2155-12:1997

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Specification for test methods transparent materials aircraft glazing Determination of linear thermal expansion

€165.00

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