This European Standard specifies the requirements relating to:
Heat resisting nickel base alloy (Ni-P101HT)
Cold worked and solution treated
Bar for machining for fasteners
3 mm ≤ D ≤ 50 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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EN 4244 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

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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 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 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 standard specifies the requirements relating to:Heat resisting nickel base alloy (NI-P100HT)Cold worked and softenedBar and wire for continuous forging or extrusion for fasteners3 mm ≤ D ≤ 30 mmfor aerospace applications.

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This standard specifies the requirements relating to: Heat resisting alloy NI-PH 2601Solution treated and cold worked Bar for forged fasteners D ≤ 50 mm1 550 MPa ≤ Rm ≤ 1 830 MPa.

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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 European Standard 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 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 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 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 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 European Standard specifies two methods for the determination of the application time of sealants.

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This European Standard specifies two methods for the determination of the application time of sealants.

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This standard specifies the requirements for glass fabric/phenolic resin preimpregnates. It shall be used together with EN 2833-1.

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This European Standard describes the preparation of panels with any desired fibre orientation of unidirectional orientated carbon fibre or fabric with thermosetting resins. The purpose of this standard is to describe recommended processes for the preparation of the panels from which test specimens subsequently are machined. Standard specimens prepared in this manner may be used either for evaluating the components i.e. the carbon reinforcement, finishes, resins, catalysts, curing agents, etc. or for verifying the overall quality of the finished products.

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This European Standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.

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This European Standard defines the requirements for the determination of the modulus of rupture of glass transparencies for aircraft applications, whether in the annealed or chemically or thermally tempered condition.

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This European Standard specifies the requirements relating to universally available and high light transmission, thermally tempered float glass plies, for aerospace applications.

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This European Standard specifies the requirements relating to universally available and high light transmission, chemically tempered float glass plies, for aerospace applications.

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This European Standard defines a qualitative method for the determination of the ream and surface ripple in glass transparencies for aircraft applications.

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This European Standard defines the requirements for the determination of the modulus of rupture of glass transparencies for aircraft applications, whether in the annealed or chemically or thermally tempered condition.

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This European Standard defines the test method for the determination of the operability of a cured sealant during and after submission to a bending load at low temperatures (low-temperature flexibility).

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This European Standard defines the test method for the determination of the operability of a cured sealant during and after submission to a bending load at low temperatures (low-temperature flexibility).

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This European Standard defines a qualitative method for the determination of the ream and surface ripple in glass transparencies for aircraft applications.

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This European Standard defines the requirements for the determination of the flatness of monolithic glass transparencies for aircraft applications. The method is designed to eliminate the effect of the glass deflecting under its own weight, thus eliminating false results.

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This European Standard specifies the requirements relating to universally available and high light transmission, thermally tempered float glass plies, for aerospace applications.

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This European Standard specifies the requirements relating to universally available and high light transmission, chemically tempered float glass plies, for aerospace applications.

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This standard defines the test equipment, apparatus and media required for determination of the smoke density according to EN 2825 and the concentration of the gas components in the smoke according to EN 2826 due to pyrolitic decomposition of solid materials and composite materials of up to 25 mm in thickness under the influence of radiant heat only or with simultaneous flame application.
This test method applies exclusively to materials whose specific standard requires this type of test. It cannot be substituted for the statutory tests required for a final specific use of the material concerned.
NOTE   The smoke gas density and the gas components in the smoke are determined according to the specific environmental and test conditions defined in this standard, in EN 2825 and EN 2826. No studies have been made up to now to determine whether the results can be transferred to differing conditions, particularly to actual fire conditions. The inhalatory toxical risk and irritancy affect cannot be assessed by merely measuring the concentration of individual gas components in the smoke.

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This European Standard defines a test method for determination of the smoke density due to pyrolitic decomposition of solid materials and composite materials of up to 25 mm in thickness under the influence of radiant heat only or with simultaneous flame application.
The test results enable a comparison of the smoke production of different materials or material configurations under the conditions specified in this standard.
NOTE 1   The smoke gas density is determined according to the specific environmental and test conditions defined in EN 2824 and this standard. No studies have been made up to now to determine whether the results can be transferred to differing conditions, particularly to actual fire conditions.
NOTE 2   The burning behaviour - and consequently the smoke density - of aerospace materials are not only influenced by the type of material but also to a large extent by the configuration, the specific surface and mass, the combination with other materials, the means of joining as well as the processing technique.

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Cette Norme européenne définit une méthode d’essai pour déterminer la concentration de certains composants de gaz dus à la décomposition pyrolytique de matériaux solides et de matériaux composites sous l’action de chaleur rayonnante uniquement ou avec application simultanée de flammes.
NOTE 1   Les composants de gaz de fumée sont déterminés selon les conditions d’essai et d’environnement spécifiques dans l’EN 2824 et la présente norme. Aucune étude n’a été menée jusqu’à présent pour déterminer si les résultats peuvent être transposés à des conditions différentes, en particulier aux conditions de feu réelles. L'incidence concernant le risque et l’irritation toxiques par inhalation ne peut être évaluée par simple mesure de la concentration des composants individuels de gaz de fumée.
NOTE 2   Le comportement de la combustion et donc des composants de gaz de fumée des matériaux aérospatiaux ne sont pas seulement influencés par le type de matériau mais encore, dans une grande mesure, par la configuration, la surface et la masse spécifiques, la combinaison avec d'autres matériaux, les moyens de soudage ainsi que la technique de traitement.
NOTE 3   Ces influences doivent être prises en considération lors de la préparation des essais, du choix des éprouvettes et de l'interprétation des résultats d'essai.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
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 alloy NI-CH2601 (NiCr19Fe19Nb5Mo3)
Non heat treated
Remelting stock
for aerospace applications.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
Solution treated
Seamless tubes
For hydraulic application
D ≤ 50 mm, a≤ 3 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
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 alloy NI-CH2601 (NiCr19Fe19Nb5Mo3)
Non heat treated
Remelting stock
for aerospace applications.

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This standard specifies the requirements relating to:
Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb)
Solution treated
Seamless tubes
For hydraulic application
D ≤ 50 mm, a≤ 3 mm
for aerospace applications.

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This standard specifies the dimensions and tolerances of:
Round bars, machined
in heat resisting alloys
Diameter 10 mm L D L 180 mm
for aerospace applications.

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This standard specifies the dimensions and tolerances of:
Hot rolled sheets and plates
in heat resisting alloys
Thickness 2,0 mm L a L 100 mm
for aerospace applications.

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This standard specifies the dimensions and tolerances of:
Round bars, machined
in heat resisting alloys
Diameter 10 mm £ D £ 180 mm
for aerospace applications.

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This standard specifies the dimensions and tolerances of:
Hot rolled sheets and plates
in heat resisting alloys
Thickness 2,0 mm £ a £ 100 mm
for aerospace applications.

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This standard specifies the requirements relating to:
Nickel base alloy NI-B40002
Filler metal for brazing
Powder or paste
for aerospace applications.

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This standard defines the test methods for the flame resistance rating of non-metallic materials. It applies exclusively to materials whose specific standard requires this type of test. It cannot be substituted for the statutory test required for a final specific use of the material concerned.

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This standard specifies the general requirements for the manufacture, inspection and testing of steel, nickel base or cobalt base alloy remelting stock and castings. Particular requirements applicable to remelting stock and castings are defined in EN 2103-2 and EN 2103-3 respectively. Unless otherwise specified on the drawing, order or inspection schedule, the reference to EN 2103 only defines one quality level which is quality level 2 in table 4 or5 of EN 2103-3.

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This standard specifies the requirements relating to: Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Wire for aerospace applications.

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