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 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 the requirements relating to:
Heat resisting nickel base alloy Ni Cr20Co3Fe3
Rm ≥ 650 MPa
Sheets and strips, cold rolled
0,25 mm < a ≤ 3 mm
for aerospace applications.

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This document specifies the requirements relating to:
Steel X5CrNiCu15-5 (1.4545)
Consumable electrode remelted (ESR or VAR)
Solution treated and precipitation treated (H1025)
Bars for machining
a or D ≤ 250 mm
1 070 MPa ≤ Rm ≤ 1 200 MPa
Premium quality (pq)
for aerospace applications.
NOTE   Other designation: The ASD-STAN designation of this material is FE-PM1802.
Only the chemical composition of this document are to be considered.

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This document specifies the requirements relating to:
Heat-resisting nickel base alloy NiCr20Co3Fe3
Rm ≥ 650 MPa
Sheets and strips, cold rolled
0,25 mm < a ≤ 3 mm
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 test method standards.

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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 requirements relating to:
Heat resisting alloy CO-PH4101 (CoCr20W15Ni)
Vacuum melted
Solution treated
Forgings
De ≤ 100 mm
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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    15 pages
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This document specifies the requirements relating to:
Heat resisting alloy CO-PH4101 (CoCr20W15Ni)
Vacuum melted
Solution treated
Forgings
De ≤ 100 mm
for aerospace applications.

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This document specifies the requirements relating to:
Heat resisting nickel base alloy (NI-P101HT)
Cold worked and solution treated
Bars for machining for fasteners
3 mm ≤ D ≤ 50 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1)
Consumable electrode remelted
Cold drawn wire for the manufacture
of the thread inserts
D  3 mm
for aerospace applications.

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This document specifies the requirements relating to:
Heat resisting nickel base alloy Ni-P96-HT
Cold drawn and precipitation treated
Wire
D ≤ 10 mm
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 test method for the determination of the horizontal flame propagation of non-metallic materials when subjected to a small flame in part or in whole.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the horizontal Bunsen burner test.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.

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This document specifies the test method for the determination of the vertical flame propagation and after flame time of non-metallic materials in part or in whole.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the vertical Bunsen burner test:
a)   with a flame application time of 60 s;
b)   with a flame application time of 12 s.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.

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This document specifies the test for the determination of the resistance of non-metallic materials in part or in whole to flame and glow propagation and to flame penetration.
This test method is also used for testing non-metallic materials which have to meet the test criteria for the 45° Bunsen burner test.
It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents.
This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.

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This document specifies the requirements relating to:
Heat resisting alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al)
Solution treated and cold worked
Bar for forged fasteners
3 mm  ≤ D  ≤ 30 mm
for aerospace applications.

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    8 pages
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This document specifies the requirements relating to: Heat resisting alloy NI-PH2801 (NiCr16Fe7Ti3Nb1Al1) Consumable electrode remelted Cold drawn wire for the manufacture of the thread inserts D ≤ 3 mm for 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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    9 pages
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  • Standard
    9 pages
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This document specifies the requirements relating to: Heat resisting nickel base alloy Ni-P96-HT Cold drawn and precipitation treated Wire D ≤ 10 mm for aerospace applications.

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    9 pages
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This document specifies the test for the determination of the resistance of non-metallic materials in part or in whole to flame and glow propagation and to flame penetration. This test method is also used for testing non-metallic materials which have to meet the test criteria for the 45° Bunsen burner test. It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents. This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.

  • Standard
    15 pages
    English language
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This document specifies the test method for the determination of the horizontal flame propagation of non-metallic materials when subjected to a small flame in part or in whole. This test method is also used for testing non-metallic materials which have to meet the test criteria for the horizontal Bunsen burner test. It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents. This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.

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    16 pages
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This document specifies the test method for the determination of the vertical flame propagation and after flame time of non-metallic materials in part or in whole. This test method is also used for testing non-metallic materials which have to meet the test criteria for the vertical Bunsen burner test: a) with a flame application time of 60 s; b) with a flame application time of 12 s. It is used for evaluation of non-metallic materials or constructions used in the interiors of aerospace vehicles but also may be used in other applications as specified in applicable procurement and regulatory documents. This standard should be used to measure and describe the properties of non-metallic materials, products or assemblies in response to heat and flame under controlled laboratory conditions and should not be used to describe or appraise the fire hazard or fire risk of materials, products, or assemblies under actual fire conditions. However, results of this test may be used as elements of a fire risk assessment which takes into account all of the factors which are pertinent to an assessment of the fire hazard of a particular end use.

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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 alloy NI-PH1302 (NiCr20Co13Mo4Ti3Al)
Solution treated and cold worked
Bar for forged fasteners
3 mm ≤ D ≤ 30 mm
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 standard specifies the requirements relating to:
This European Standard specifies the requirements relating to:
Heat resisting
Nickel base alloy Ni-Cr20Co3Fe3
Annealed
Bars
for aerospace applications.

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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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    22 pages
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This standard specifies the requirements relating to:
This European Standard specifies the requirements relating to:
Heat resisting
Nickel base alloy Ni-Cr20Co3Fe3
Annealed
Bars
for aerospace applications.

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    7 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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This European Standard specifies the requirements relating to: Heat resisting nickel base alloy NiCr20Co3Fe3 Annealed Wire D ≤ 10 mm
for aerospace applications.
NOTE Other designation: Only the chemical composition of this standard must be considered.

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EN 2402 specifies the requirements relating to: Heat resisting nickel base alloy NiCr20Co3Fe3 Annealed Wire D ≤ 10 mm for aerospace applications.

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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 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 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 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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    14 pages
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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 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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    7 pages
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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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    21 pages
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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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