This document specifies the requirements relating to:
Heat resisting alloy FE-PM1708
Vacuum arc remelted
As forged
Forging stock
De ≤ 300 mm
for aerospace applications.

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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 FE-PM1708
Vacuum arc remelted
Hardened and tempered
Bars
a or D ≤ 200 mm
1 000 MPa ≤ Rm ≤ 1 140 MPa
for aerospace applications.

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This document specifies the requirements for the determination of conductivity and pH of aqueous extracts of textile materials.
This method has been written in response to an aerospace requirement for a method of extraction using hot water as the EN 1413 requires only a cold water extraction method.

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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 precipitation 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
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
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 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
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:
Steel FE-PM1503 (X3CrNiMoAl 13-8-2)
Vacuum induction melted and consumable electrode remelted
Solution treated and precipitation treated
Bar for machining
a or D ≤ 150 mm
Rm ≥ 1 400 MPa
for aerospace applications.

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This document specifies the acid pickling of aluminium and aluminium alloys free from hexavalent chromium.

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This document specifies the requirements relating to:
Heat resisting nickel base alloy (NI-P100HT)
Cold worked and softened
Bar and wire for continuous forging or extrusion for fasteners
3 mm ≤ D ≤ 30 mm

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This document specifies the requirements relating to:
Heat resisting alloy NI-PH2601
Solution treated and cold worked
Bar for forged fasteners
D ≤ 50 mm
1 550 MPa ≤ Rm ≤ 1 830 MPa
for 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 standard specifies several chemical methods of passivation for corrosion resisting steels (austenitic, ferritic, martensitic and precipitation hardenable) and of decontamination for nickel or cobalt base alloys.

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This document describes the electrical contact resistance testing method applicable to conductive and non-conductive coatings applied on test specimens made of conductive materials (unless otherwise specified) for aerospace applications. An objective of this practice is to define and control many of the known variables in such a way that valid comparisons of the contact properties of materials can be made.
This test may be locally destructive depending on the process tested.

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This document specifies the requirements relating to:
Steel X3CrNiMoAl13-8-2 (1.4534)
Solution annealed and precipitation hardened
1 400 ≤ Rm ≤ 1 550 MPa
Forgings
De ≤ 100 mm
for aerospace applications.
ASD-STAN designation: FE-PM67.

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This document specifies the requirements relating to:
Steel X5CrNoMoCuNb14-5 (1.4594)
930 MPa ≤ Rm ≤ 1 080 MPa
Forgings
De ≤ 150 mm
for aerospace applications.
ASD-STAN designation: FE-PM66.

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This document specifies the requirements relating to:
Steel X8CrNiTi18-10 (1.4878/1.4544)
Softened
500 ≤ Rm ≤ 750 MPa
Tubes for structures
0,5 ≤ a ≤ 5 mm
for aerospace applications.
ASD-STAN designation: FE-PA13.

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This document specifies the requirements relating to:
Steel 31Ni10
1 230 MPa ≤ Rm ≤ 1 420 MPa
Forgings
De ≤ 40 mm
for aerospace applications.
ASD-STAN designation: FE-PL73.

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This document specifies the requirements relating to:
Steel X5CrNiCuNb16-4 (1.4549 type 1.4542)
As cast
Reference heat treatment:
homogenised, solution treated, precipitation hardened and sub zero
Remelting stock
for aerospace applications.
ASD-STAN designation: FE-CM61.

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This document specifies the requirements relating to:
Steel 30CrNiMo8 (1.6580)
1 100 MPa ≤ Rm ≤ 1 300 MPa
Forgings
De ≤ 100 mm
for aerospace applications.
W.nr: 1.6580
ASD-STAN designation: FE-PL74.

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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:
Steel X5CrNoMoCuNb14-5 (1.4594)
930 MPa ≤ Rm ≤ 1 080 MPa
Bars
De ≤ 150 mm
for aerospace applications.
ASD-STAN designation: FE-PM66.

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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 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 relating to:
Steel X8CrNiTi18-10 (1.4878/1.4544)
Annealed
Reference heat treatment: softened
Hollow bars
5 mm ≤ a ≤ 12 mm
for aerospace applications.

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This document specifies the requirements relating to:
Steel X8CrNiTi18-10 (1.4878/1.4544)
Softened
500 MPa ≤ Rm ≤ 700 MPa
Forgings
De ≤ 100 mm
for aerospace applications.
ASD-STAN designation: FE-PA13.

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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 relating to:
Steel X8CrNiTi18-10 (1.4878/1.4544)
Annealed
Reference heat treatment: softened
Forging stock
De ≤ 100 mm
for aerospace applications.
ASD-STAN designation: FE-PA13.

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This document defines the requirements for the preparation of forged test samples.
Unless otherwise specified on the drawing, order, or inspection schedule, this document shall be applied when referenced in the relevant EN material standard or EN technical specification.
This document applies to round products of ≥ 20 mm diameters or other shapes of equivalent cross-section.

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This document specifies the requirements for an intermediate coat to be applied over a primer for aerospace applications and with a topcoat for aerospace applications on top.
The properties specified in this document are obtained on defined aluminium alloy test pieces prepared in accordance with EN 3837 and EN ISO 3270 and painted with primer listed in Table 1. Topcoat listed in Table 1 is to be applied on intermediate coat to this document. The ability of the material to be used for a specific application (e.g. alternative substrate, alternative primer, specific drying conditions, etc.) should be determined by supplementary tests to confirm that the requirements of this document are met.

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This document defines the requirements for hexavalent chromium free anodizing of aluminium and aluminium alloys for corrosion protection, bonding and painting.
Hard anodizing and plasma electrolytic anodizing (micro-arc oxidation) are not covered by this document.
The purpose of this document is to give design, quality and manufacturing requirements. It does not give complete in-house process instructions; these are given in the processors detailed process instructions.

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This document specifies the requirements relating to:
Steel FE-PM1802 (X5CrNiCu15-5)
Consumable electrode remelted
Solution treated and precipitation treated
Forgings
a or D ≤ 200 mm
Rm ≥ 965 MPa

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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 document specifies the requirements relating to:
Aluminium alloy 6082-
T6
Tubes for structures
0,6 mm ≤ a ≤ 12,5 mm
for aerospace applications.

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This document specifies the method of test for evaluating the tendency of paints and varnishes towards sedimentation of their pigments.
The procedure describes a method where the pigmented paint is allowed to settle at a specified temperature and for a specified time.
The procedure is not applicable to products which possess a pot life inferior to the specified measuring time.

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This document specifies the test method for determining the expansion ratio and the volatile content in structural foaming adhesive films.

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This document specifies the dimensions and tolerances of cold rolled sheets and strips in heat resisting alloys used in aerospace construction.

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This document specifies the requirements relating to:
Aluminium alloy Al-P16-
T6151
Plates
6 mm < a ≤ 120 mm
for aerospace applications.

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This document defines the requirements for hexavalent chromium free anodic electrodeposition of organic coatings on aluminium and aluminium alloys for corrosion protection of parts.
The purpose of this standard is to give design, quality and manufacturing requirements. It doesn’t give complete in-house process instructions; these shall be given in the processor detailed process instructions.

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This document specifies the requirements relating to:
Steel X2CrNi18-9 (1.4307)
Softened
450 MPa ≤ Rm ≤ 680 MPa
Bars for machining
4 mm ≤ De ≤ 100 mm
for aerospace applications.

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This document defines the nature of and the surface preparation method for test pieces in aluminium alloys intended for testing paints and varnishes used for aerospace applications.

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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 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 European Standard specifies the marking rules for aerospace products, semi-finished products, and ready to use parts, which need surface marking by discoloration using a laser source to identify the part and/or enhance its traceability.
This type of marking can be used on a wide range of materials (both metallic and non-metallic) and coatings (paints, varnishes…). It is in line with the part definition.

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This document specifies the requirements relating to:
Steel FE-PM1503 (X3CrNiMoAl 13-8-2)
Vacuum induction melted and consumable electrode remelted
Solution treated and precipitation treated
Bar for machining
a or D ≤ 150 mm
1 200 MPa ≤ Rm ≤ 1 400 MPa
for aerospace applications.

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This document specifies the requirements relating to:
Titanium TI-P99002
Annealed
Bar for machining
a or D ≤ 150 mm
Rm ≥ 390 MPa
for aerospace applications.

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