49.025.05 : Ferrous alloys in general

ASTM E1558-09(2014)

ASTM E1558-09(2014)

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Standard Guide for Electrolytic Polishing of Metallographic Specimens

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BS EN 4315:2007

BS EN 4315:2007

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Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPa

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BS EN 4314:2007

BS EN 4314:2007

Superseded Historical

Aerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D = 250 mmAerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D = 250 mmAerospace series. Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15). Non heat treated, forging stock a or D = 250 mm

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BS EN 4317:2007

BS EN 4317:2007

Superseded Historical

Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D = 200 mmAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D = 200 mmAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Non heat treated, forging stock a or D = 200 mm

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BS EN 4318:2007

BS EN 4318:2007

Superseded Historical

Aerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De = 100 mm, Rm = 960 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De = 100 mm, Rm = 960 MPaAerospace series. Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15). Solution treated and precipitation treated, bar and section De = 100 mm, Rm = 960 MPa

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DIN EN 4314:2008-03

DIN EN 4314:2008-03

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Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D 250 mm; German and English version EN 4314:2007

€77.20

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DIN EN 4315:2008-03

DIN EN 4315:2008-03

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D 100 mm, R 900 MPa; German and English version EN 4315:2007

€77.20

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DIN EN 4317:2008-03

DIN EN 4317:2008-03

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D 200 mm; German and English version EN 4317:2007

€77.20

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DIN EN 4318:2008-03

DIN EN 4318:2008-03

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section D 100 mm, R 960 MPa; German and English version EN 4318:2007

€77.20

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NBN EN 4318:2008

NBN EN 4318:2008

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De = 100 mm, Rm = 960 MPa

€50.00

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NBN EN 4317:2008

NBN EN 4317:2008

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Non heat treated, forging stock a or D = 200 mm

€50.00

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NBN EN 4315:2008

NBN EN 4315:2008

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D = 100 mm, Rm = 900 MPa

€50.00

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NBN EN 4314:2008

NBN EN 4314:2008

Superseded Historical

Aerospace series - Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15) - Non heat treated, forging stock a or D = 250 mm

€50.00

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DIN EN 2002-001 Berichtigung 1:2007-08

DIN EN 2002-001 Berichtigung 1:2007-08

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Aerospace series - Metallic materials - Test methods - Part 1: Tensile testing at ambient temperature; German and English version EN 2002-001:2005, Corrigenda to DIN EN 2002-001:2006-11

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DIN EN 2002-002 Berichtigung 1:2007-08

DIN EN 2002-002 Berichtigung 1:2007-08

Superseded Historical

Aerospace series - Metallic materials - Test methods - Part 2: Tensile testing at elevated temperature; German and English version EN 2002-002:2005, Corrigenda to DIN EN 2002-002:2006-11

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