This document specifies the dimensions and tolerances of plates in aluminium alloy 2024 with close-tolerance flatness, thickness 6 mm < a ≤ 55 mm, 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 acid pickling of aluminium and aluminium alloys free from hexavalent chromium.

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This document specifies the characteristics, test methods, qualification and acceptance conditions of single and multicore electric cables for general purpose with conductors in aluminium or copper-clad aluminium, intended for installation in aircraft electrical systems. The insulation of these cables is designed to withstand aircraft voltages at a frequency not exceeding 2 000 Hz. Unless specified by individual product standards the maximum demonstrated voltage of rating of these cables is ac 115 V rms phase to neutral and 200 V rms phase to phase and 28 Vdc. They are divided into types, the characteristics of which are given in the product standards. Unless otherwise specified in the product standard, the tests defined in this standard apply.

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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: Aluminium alloy 6082- T6 Tubes for structures 0,6 mm ≤ a ≤ 12,5 mm

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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:
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 requirements relating to: Aluminium alloy Al-P16- T6151 Plates 6 mm < a ≤ 120 mm.

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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. 2 Normative

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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 specifies the requirements relating to:
Aluminium alloy 2024 - -
T3
Extruded bar and section
1,2 mm ≤ (a or D) ≤ 150 mm
with coarse peripheral grain control
for aerospace applications.

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This European Standard specifies the characteristics of electrical wires AZ family for use in the on board:
   115 V (phase to neutral) or 200 V (phase to phase) electrical network of aircraft.
   230 V (phase to neutral) or 400 V (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.
This cable family is used at operating temperature between  65 °C and 180 °C.

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This European Standard specifies the characteristics of electrical wires AZA family for use in the on board:
   115 V (phase to neutral) or 200 V (phase to phase) electrical network of aircraft.
   230 V (phase to neutral) or 400 V (phase to phase) electrical network of aircraft and particularly use in non-pressurized areas.
This cable family is used at operating temperature between  65 °C and 180 °C.

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This document specifies the requirements relating to:
Aluminium 1050A-H14
Wire for solid rivets
D ≤ 10 mm
for aerospace applications.

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This document specifies the requirements relating to:
Aluminium alloy 2024-
T42
Drawn tubes for structural applications
for aerospace applications.

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This document specifies the requirements relating to:
Aluminium alloy 2024 - -
T3
Extruded bar and section
1,2 mm ≤ (a or D) ≤ 150 mm
with coarse peripheral grain control
for aerospace applications.

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This document specifies the requirements relating to:
Aluminium alloy 2024-
T42
Drawn tubes for structural applications
for aerospace applications.

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This document specifies the requirements relating to:
Aluminium 1050A-H14
Wire for solid rivets
D ≤ 10 mm
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, 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 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 specifies the requirements relating to:
Aluminium alloy AL-P7175
Forging stock
for aerospace applications.

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This document specifies the requirements relating to:
Aluminium alloy (5086)
Annealed and straightened (H111)
Drawn bar
6 mm ≤ D ≤ 50 mm
for aerospace applications.

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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 document specifies the requirements relating to:
Aluminium alloy 2024-T4
Drawn bars
a ≤ 75 mm
for aerospace applications.

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This document specifies the requirements relating to:
Aluminium alloy (5086)
Annealed and straightened (H111)
Drawn bar
6 mm ≤ D ≤ 50 mm
for aerospace applications.

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

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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 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 document specifies the requirements relating to:
Aluminium alloy 2024-T4
Drawn bars
a ≤ 75 mm
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 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 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 document specifies the requirements relating to:
Aluminium alloy AL-P-6061-
T6
Drawn tube for pressure applications
0,6 mm ≤ a ≤ 12,5 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Aluminium alloy AL-C42101
T6
Sand casting
a ≤ 20 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Aluminium alloy AL-C42201
T6
Sand casting
a ≤ 20 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Aluminium alloy 2024-
T3510
Bars and sections
1,2 mm ≤ (a or D) ≤ 150 mm
With peripheral coarse grain control
for aerospace applications.

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This European Standard specifies the procedure for the determination of the susceptibility to
intergranular corrosion of wrought aluminium alloys in AL-P2XXX- series, AL-P7XXX- series and
aluminium-lithium alloy products.
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 document specifies the requirements relating to:
Aluminium alloy AL-P-6061-
T6
Drawn tube for pressure applications
0,6 mm ≤ a ≤ 12,5 mm
for aerospace applications

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This European Standard specifies the requirements relating to:
Aluminium alloy AL-C42101
T6
Sand casting
a ≤ 20 mm
for aerospace applications.

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This European Standard specifies the procedure for the determination of the susceptibility to intergranular corrosion of wrought aluminium alloys in AL-P2XXX- series, AL-P7XXX- series and aluminium-lithium alloy products.
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 European Standard specifies the requirements relating to:
Aluminium alloy AL-C42201
T6
Sand casting
a ≤ 20 mm
for aerospace applications.

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This European Standard specifies the requirements relating to:
Aluminium alloy 2024-
T3510
Bars and sections
1,2 mm ≤ (a or D) ≤ 150 mm
With peripheral coarse grain control
for aerospace applications.

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This European Standard specifies the dimensions, linear resistance, mechanical characteristics,
construction and mass of conductors in aluminium or aluminium alloy for electrical cables for aerospace
applications.
It applies to stranded conductors with nominal cross-sections of 5 mm2 to 107 mm2 inclusive.

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