This document specifies the required characteristics of loop style clamps ("P" type) in aluminium alloy with various cushion materials.
These clamps are used for supporting aerospace pipe assemblies and electrical cable bundles.
They are used up to 80 °C max.
Usage at a higher temperature is at the option of the user.
For temperature range and environmental considerations, see the various cushion material standards.

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This document defines the requirements for micro-arc oxidation of aluminium and aluminium alloys for corrosion protection, wear, erosion, dielectric and thermal properties.
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.
This document relates only to micro-arc oxidation. It does not relate to finishing techniques, such as mechanical post treatment.

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This document defines the requirements for micro-arc oxidation of aluminium and aluminium alloys for corrosion protection, wear, erosion, dielectric and thermal properties.
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.
This document relates only to micro-arc oxidation. It does not relate to finishing techniques, such as mechanical post treatment.

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

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This document defines the requirements for qualification, acceptance, delivery and inspection of 100° countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear type in aluminium alloy 7050T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061T7 for use as permanent fasteners in aerospace applications.

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This document specifies the requirements for hexavalent chromium free anodizing of aluminium and aluminium alloys for corrosion protection, bonding and painting.
This document does not apply to hard anodizing and plasma electrolytic anodizing (micro-arc oxidation).
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 processor's detailed process instructions.

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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 characteristics of externally threaded fasteners, 100° countersunk normal head, Spiral Drive Recess, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated, for aerospace applications.
Classification: 1 100 MPa /425 °C

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

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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 2024-T3
Bars and sections
a ≤ 150 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 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 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, 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 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 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 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 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 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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    8 pages
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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 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-C42101
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 requirements relating to:
Aluminium alloy AL-C42201
T6
Sand casting
a ≤ 20 mm
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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    40 pages
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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.

  • Standard
    40 pages
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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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    37 pages
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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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    9 pages
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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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    8 pages
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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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