This document specifies the requirements relating to:
Titanium alloy TI-P64001 (Ti-6Al-4V)
Annealed
Bars for machining
D < 300 mm
900 MPa ≤ Rm ≤ 1 160 MPa
for aerospace applications

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This document specifies the requirements relating to:
Aluminium alloy AL-P6061-T4
Drawn tube for pressure applications
0,6 mm ≤ a ≤ 3 mm
for aerospace applications.

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This document specifies the characteristics of self-extinguishing and low smoke emission semi-finished polycarbonate sheets with and without UV radiation protection requirement, as used for aircraft equipment, such as internal panelling, simple internal glazing, sound-proofing panels, light covers, etc.

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This document specifies the requirements relating to:
Aluminium alloy 5086
H111
Extruded bars
10 mm ≤ D ≤ 300 mm
for aerospace applications.

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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:
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 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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This European Standard defines the requirements for the ordering, manufacture, testing, inspection and
delivery of aluminium and aluminium alloy plate, clad or unclad, supplied in the as-rolled or machined
condition. It shall be applied when referred to and in conjunction with 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 aluminium and aluminium alloy sheet and strip, clad or unclad. It shall be applied when referred to and in conjunction with 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 aluminium and aluminium alloy, bar and section, produced by extrusion, rolling or drawing. It shall be applied when referred to and in conjunction with 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 aluminium alloy wrought forging stock (produced by extrusion or hot rolling) and cast forging stock. It shall be applied when referred to and in conjunction with the EN material standard, normally when the forging stock manufacturer is not the producer of the corresponding forgings.

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This European Standard specifies the requirements relating to:
Aluminium alloy 2024-T3
Bars and sections
a ≤ 150 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Aluminium alloy AL-P7175
Forging stock
for aerospace applications.

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This European Standard specifies the procedure for the macrographic examination of the cut surface from aluminium and aluminium alloy wrought products, forging stock and forgings.
It does not consider health and safety requirements. It is the responsibility of the user to adopt appropriate health and safety precautions when hazardous substances are involved.

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This standard specifies the characteristics of aluminium and aluminium alloy square and rectangular extruded bars, used in aerospace construction.

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This European Standard specifies the dimensions and tolerances of heat resisting alloys wire used in aerospace construction.

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This European Standard specifies the requirements relating to:
Aluminium alloy 2014A-
T6
Tubes for structures
0,6 mm ≤ a ≤12,5 mm

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This European Standard specifies the requirements relating to:
Steel FE-PL31
Hardened and tempered
Hollow bars
3,5 mm≤ a ≤ 55 mm
for aerospace applications.

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This European Standard specifies the dimensions and physical constants of U-section aluminium alloy folded profiles used in aerospace construction.

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This European Standard specifies the requirements relating to:
Titanium TI-P99002
Not heat treated
Grade 2 forging stock, for annealed forgings
a or D  300 mm
for aerospace applications.

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This document specifies the general requirements for recycling, by vacuum remelting or cold hearth melting, titanium and titanium alloy scrap used for the production of ingots.

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This document specifies the requirements for the ordering, manufacture, testing, inspection and delivery of titanium and titanium alloy plate, sheet and strip. It is applied when referred to and in conjunction with the EN material standard 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 titanium and titanium alloy forging stock. It is intended to be applied when referred to and in conjunction with the European material standard 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 titanium and titanium alloy remelting stock. It is intended to be applied when referred to and in conjunction with the European material standard 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 titanium and titanium alloy tube. It is applied when referred to and in conjunction with the EN material standard 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 titanium and titanium alloy wire. It is intended to be applied when referred to and in conjunction with the European material standard 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 titanium and titanium alloy bar and section. It is applied when referred to and in conjunction with the EN material standard unless otherwise specified on the drawing, order or inspection schedule.

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This document specifies the requirements relating to:
Aluminium alloy AL-P2014A
T6 or T62
Clad sheet and strip
0,4 mm ≤ a ≤ 6 mm
for aerospace applications.

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The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications.
This Part 002 specifies the "Specific rules for aluminium, aluminium alloys and magnesium alloys".

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The EN 4500 series specifies the rules for the drafting and presentation of metallic material standards for aerospace applications. This Part 004 specifies the "Specific rules for titanium and titanium alloys".

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