This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal. It is presupposed to be applied when referred to and in conjunction with the product procurement specification unless otherwise specified on the drawing, order or inspection schedule.

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This document specifies a list of procurement specifications and standards for welding products authorized for the welding of parts.

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This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMnMoV26-15 (1.4944)
Softened and cold worked
Wire for forged fasteners
D ≤ 15 mm
1 100 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.

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This document specifies the requirements relating to:
Heat-resisting alloy X6NiCrTiMnMoV26-15 (1.4944)
Softened and cold worked
Wire for forged fasteners
D ≤ 15 mm
1 100 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.

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This document defines the general terms to be used in the standards of metallic materials for aerospace applications. It is intended only to give terms which are truly general and where definition, in this context, is required. The definitions of more specific terms are to be found in the technical specifications, test methods, etc. which are referenced in the material standard concerned.

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This document specifies the rules for the drafting and presentation of technical specifications for metallic materials.

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This document specifies the rules for the drafting and presentation of test method standards.

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This document defines the general terms to be used in the standards of metallic materials for aerospace applications. It is intended only to give terms which are truly general and where definition, in this context, is required. The definitions of more specific terms are to be found in the technical specifications, test methods, etc. which are referenced in the material standard concerned.

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This document specifies the rules for the drafting and presentation of technical specifications for metallic materials.

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    18 pages
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This document specifies the rules for the drafting and presentation of test method standards.

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This document specifies the requirements relating to:
Heat resisting alloy X6NiCrTiMoV26-15 (1.4980)
Softened and cold worked
Wires for forged fasteners
D ≤ 15 mm
900 MPa ≤ Rm ≤ 1 100 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.

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This document specifies the requirements relating to:
Heat resisting alloy X6NiCrTiMoV26-15 (1.4980)
Softened and cold worked
Wires for forged fasteners
D ≤ 15 mm
900 MPa ≤ Rm ≤ 1 100 MPa
for aerospace applications.
W.nr: 1.4980.
ASD-STAN designation: FE-PA2601.

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This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

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This document specifies the requirements relating to:
Heat resisting alloy X4NiCrMoTi43-13
As forged
Forging stock
a or D ≤ 200 mm
for aerospace applications.
ASD-STAN designation: FE-PA2501.

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This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated
Sheets and strips
a ≤ 3 mm
for aerospace applications.
ASD-STAN designation: FE-PA4901.

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This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCOMoW21-20
Solution treated and descaled
Sheets and plates
3 mm < a ≤ 50 mm
for aerospace applications.
ASD-STAN designation: FE-PA4901.

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This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

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This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated and precipitation treated
Forgings
De ≤ 100 mm
for aerospace applications.
ASD-STAN designation: FE-PA4901.

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  • Standard
    8 pages
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This document specifies the requirements relating to:
Heat resisting alloy X12CrNiCoMoW21-20
Solution treated
Bars and sections
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

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    8 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA2601
Softened and cold worked
Bar for forged fasteners
D ≤ 50 mm
1 100 MPa ≤ Rm ≤ 1 300 MPa
for aerospace applications.

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This document specifies the requirements for the radiographic testing of castings for aerospace applications.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or testing schedule.

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This document specifies the requirements for penetrant testing of metallic materials for aerospace applications. It is limited to the direction of surface-breaking defects, e.g. cracks, laps, seams and inclusions.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.

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  • Standard
    9 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.

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    8 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA2501 (X4NiCrMoTi43-13)
As forged
Forging stock
a or D ≤ 200 mm
for aerospace applications.

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This document is part of the series of EN metallic material standards for aerospace applications. The general organization of this series is described in EN 4258.
This document has been prepared in accordance with EN 4500-003.

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This document specifies the requirements relating to:
Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15)
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm

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    9 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated and precipitation treated
Bars and sections
De ≤ 100 mm
for aerospace applications.

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    8 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCOMoW21-20)
Solution treated and descaled
Sheet and plate
3 mm < a ≤ 50 mm
for aerospace applications.

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    8 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Bars and sections
De ≤ 100 mm

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    8 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Sheets and strips
a ≤ 3 mm
for aerospace applications.

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This document specifies the requirements relating to:
Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21)
Solution treated and precipitation treated
Forgings
De  100 mm
for aerospace applications.

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  • Standard
    8 pages
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This standard specifies the requirements relating to:Heat resisting alloy FE-PA2601 Softened and cold worked Bar for forged fasteners D ≤ 50 mm 1 100 MPa ≤ Rm ≤ 1 300 MPafor aerospace applications.

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This document specifies the requirements for the radiographic inspection of castings for aerospace applications.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.

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    7 pages
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This document specifies the requirements for penetrant testing of metallic materials for aerospace applications. It is limited to the direction of surface breaking defects, e.g. cracks, laps, seams and inclusions.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.

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  • Standard
    9 pages
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This document specifies the requirements relating to:
Heat resisting alloy FE-PA2602 (X4NiCrTiMoV26-15)
Solution treated and precipitation treated
Bar and section
De ≤ 100 mm
for aerospace applications.

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This document specifies the designation rules for metallic semi-finished products given in Table 1, used in aerospace construction.
It is applicable only if referred to in the metallic semi-finished product standard.

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This document specifies the requirements relating to:
Heat resisting nickel base alloy (Ni-P101HT)
Cold worked and softened
Bar and wire for continuous forging or extrusion for fasteners
3 mm ≤ D ≤ 30 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Heat resisting alloy NI-PH2601
Solution treated and cold worked
Bar for forged fasteners
D ≤ 50 mm
1 270 MPa ≤ Rm ≤ 1 550 MPa
for aerospace applications.

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This document specifies the designation rules for metallic semi-finished products given in Table 1, used
in aerospace construction.
It is applicable only if referred to in the metallic semi-finished product standard.

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This European Standard specifies the requirements relating to:
Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)
Solution treated and precipitation treated
Wires for rivets
2 mm ≤ D ≤ 10 mm
Rm ≥ 960 MPa
for aerospace applications.

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This European Standard defines the determination of density according to displacement method for metallic materials.

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    4 pages
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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal for brazing for aerospace applications. It shall be applied when referred to in the EN material standard unless otherwise specified on the drawing, order or inspection schedule.

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This European Standard specifies the requirements relating to:
Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15)
Solution treated and precipitation treated
Wires for rivets
2 mm ≤ D ≤ 10 mm
Rm ≥ 960 MPa
for aerospace applications.

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    8 pages
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This European Standard defines the determination of density according to displacement method for
metallic materials.

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    4 pages
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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and delivery of all forms of filler metal for brazing for aerospace applications. It shall be applied when referred to in the EN material standard unless otherwise specified on the drawing, order or inspection schedule.

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This European Standard specifies the rules for establishing the conventional designation of unalloyed, commercially pure and alloyed metallic materials used for aerospace applications.
NOTE Information relating to former ASD-STAN designations for nickel base or cobalt base alloys, steel, commercially pure titanium and titanium base alloys, is contained in Annex (informative).

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EN 2032-001 specifies the rules for establishing the conventional designation of unalloyed, commercially pure and alloyed metallic materials used for aerospace applications.

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This European Standard specifies the requirements relating to: Heat resisting alloy FE-PA4901 (X12CrNiCoMoW21-20) As forged Forging stock a or D 200 mm 690 MPa < Rm < 880 MPa for aerospace applications.

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This European Standard specifies the specific rules for the drafting and presentation of heat resisting alloy material standards for aerospace applications. It should be used in conjunction with EN 4500-001.

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This European Standard defines the general requirements for semi-finished product qualification of EN metallic materials (excluding forgings and castings). Specific requirements are given in the material standards and/or relevant technical specification.

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