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 FE-PA2501 (X4NiCrMoTi43-13)
As forged
Forging stock
a or D ≤ 200 mm
for aerospace applications.

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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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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-PA4901 (X12CrNiCoMoW21-20)
Solution treated
Bars and sections
De ≤ 100 mm

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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 (X12CrNiCOMoW21-20)
Solution treated and descaled
Sheet and plate
3 mm < a ≤ 50 mm
for aerospace applications.

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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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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
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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
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 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
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 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 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
Bars and sections
De ≤ 100 mm
for aerospace applications.
ASD-STAN Designation: FE-PA4901.

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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 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 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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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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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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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 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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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 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 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 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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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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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 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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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 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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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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This 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  960 MPa
for aerospace applications.

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This European Standard specifies the general rules for the drafting and presentation of metallic material standards for aerospace applications. It is supported by additional rules specific to: - Aluminium, aluminium alloys and magnesium alloys EN 4500-2; - Heat resisting alloys, EN 4500-003; - Titanium and titanium alloys, EN 4500-004; - Steels, EN 4500-005; - Filler metals for welding, EN 4500-2 to EN 4500-005; - Filler metals for brazing, EN 4500-6.

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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 covers the general requirements for heat treatment facilities processing semi-finished products and parts in metallic aerospace materials. It defines the terms used herein and describes the test procedures and requirements for mandatory tests of heat treatment facilities. It also serves as an aid in the surveillance and approval of heat treatment facilities. This standard applies to all types of heat treatment facilities, including those using direct or indirect heat transfer and liquid or gaseous heating media, with our without circulation, and to vacuum furnaces.

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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 specifies the requirements for sharp edge-notch tensile testing for sheet and strip 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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This specification 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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This European Standard specifies the requirements for sharp edge-notch tensile testing for sheet and strip 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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This European Standard specifies the general rules for the drafting and presentation of metallic material standards for aerospace applications.
It is supported by additional rules specific to:
-   Aluminium, aluminium alloys and magnesium alloys   EN 4500-2;
-   Heat resisting alloys   EN 4500-003;
-   Titanium and titanium alloys   EN 4500-004;
-   Steels   EN 4500-005;
-   Filler metals for welding   EN 4500-2 to EN 4500-005;
-   Filler metals for brazing   EN 4500-6.

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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 covers the general requirements for heat treatment facilities processing semi-finished products and parts in metallic aerospace materials.
It defines the terms used herein and describes the test procedures and requirements for mandatory tests of heat treatment facilities. It also serves as an aid in the surveillance and approval of heat treatment facilities.
This standard applies to all types of heat treatment facilities, including those using direct or indirect heat transfer and liquid or gaseous heating media, with our without circulation, and to vacuum furnaces.

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This European Standard defines the ultrasonic inspection procedure for rolled, drawn, extruded and forged billets, bars and plates, rolled rings and forgings with a uniform square, rectangular or round cross section. It does not cover critical rotating parts in steel, titanium, titanium alloys, aluminium alloys and heat resisting alloys that are to be inspected in accordance with the technical supply conditions of the relevant EN standards or internal specifications.
For products with geometries other than those described above, the test conditions and acceptance criteria shall be agreed between the manufacturer and purchaser.

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This European Standard specifies the requirements for the manufacture, checking and marking of the series of ultrasonic testing reference blocks containing flat bottom holes (FBH) which define the indicated defect size to which reference is made in EN standards.
The application of ultrasonic testing reference blocks containing side drilled holes (SDH) which define an indicated defect size shall be agreed between manufacturer and purchaser.
This standard is applicable to the production of master and standard test blocks to be used when carrying out ultrasonic inspection to the requirements of EN 4050 1 (FBH method).
It is recognized that particular difficulties are encountered with round forging stock and bars due to the wide range of curvatures. For this application, only one block shall be produced to act as both master and standard test block.

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