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

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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 document specifies the requirements relating to:
X5CrNiCu15-5 (1.4545)
Consumable electrode remelted (ESR or VAR)
Solution treated and precipitation treated (H1025)
Bar for machining
a or D ≤ 250 mm
1 070 MPa ≤ Rm ≤ 1 200 MPa
Premium quality (pq)
for aerospace applications.
NOTE Other designation:
Only the chemical composition of this standard must be considered.

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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 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 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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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 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 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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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 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 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 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 specifies the acceptance criteria for products ultrasonically inspected in accordance with EN 4050 1.

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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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This European Standard specifies the method of performing ultrasonic testing. The general requirements are given in EN 4050 1.

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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 standard specifies the requirements for determining fatigue crack growth rates using the corner-crack (CC) test piece. Crack development is measured using a potential-drop system, and the calculated crack depths can be corrected via marker bands created on the fracture surface during the test. Results are expressed in terms of the crack-tip stress-intensity range (K), with crack depths and test stress level noted.

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This European Standard defines a method to determine constant amplitude fatigue data of metallic materials and the S N curve (or Wöhler curve).

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This European Standard defines degrees of weldability and brazeability for materials or families of materials used in the aerospace industry. It comprises a series of sheets, by materials or by material family, which: - indicate the main titles, the chemical composition and the main characteristics; - contain recommendations for welding and brazing; - indicate a degree of weldability or brazeability for a given process under defined conditions; - indicate a value of the mechanical strength coefficient of the welded joint for each welding process, when it could be extracted from bibliographic references referring to it. The joint coefficient is expressed as a ratio of the tensile strength of the welded joint to the tensile strength of the base alloy (to be in accordance with EN 4632-002). It is applicable without restriction for the manufacturing of new parts or for repair.

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This standard applies to uninterrupted constant-load tensile creep strain and stress-rupture testing of metallic materials governed by aerospace standards. It defines the properties that may need to be determined and the terms used in describing tests and test pieces. It specifies the dimensions of test pieces and the method of testing. The duration of the creep strain and stress-rupture tests complying with this standard shall be less than 10 000 h and at temperatures not exceeding 1 100 °C.
This standard may also apply to metallic materials for test durations exceeding 10 000 h and/or for test temperatures exceeding 1 100 °C providing that previous agreement has been reached between the manufacturer and the purchaser.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-CH1303 (NiCo20Cr20Mo5Ti2Al)
Non heat treated
Remelting stock
for aerospace applications.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-PH2301 (NiCr21Fe18Mo9)
Non heat treated
Forging stock
a or D ≤ 250 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Heat resisting nickel alloy with copper NI-PD9001 (NiCu31)
Wire for solid rivets
D < or = 10 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm for aerospace applications.

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