49.025.20 - Aluminium
ICS 49.025.20 Details
Aluminium
Aluminium
Aluminium
Aluminij
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This document specifies the requirements relating to:
Aluminium alloy AL-P7010
Forging stock
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy AL-P7010
Forging stock
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics and the tests required to qualify and control lots of high purity (≥99 %) aluminium coatings applied by ion-vapor deposition (IVD) on fasteners.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This document 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 115 mm2 inclusive.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy AL-P2014A
T6 or T62
Clad sheets and strips
0,4 mm ≤ a ≤ 6 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of flanged bushes in aluminium alloy with self-lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for use in assembly with an interference fit into fixed and moving aerospace parts.
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of plain bushes in aluminium alloy with self-lubricating liner and the design recommendation of shafts and housings.
The bushes are intended for use in assembly with an interference fit into fixed and moving aerospace parts.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy AL-P2014A
T6 or T62
Clad sheets and strips
0,4 mm ≤ a ≤ 6 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the list of product standards and common characteristics of electrical cables for general purpose with conductors in aluminium or copper-clad aluminium, intended for installation in aircraft electrical systems.
- Standard11 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of UV laser printable electrical lightweight wires ADA family for use in the on-board 115 V (phase to neutral) or 200 V (phase-to-phase) AC, 28 VDC electrical systems of aircraft at operating temperatures between −65 °C and 180 °C. These cables are demonstrated to be arc resistant in sizes AWG 26 to 14 (115 VAC/200 VAC).
In addition, these cables can be suitable for use at 230 VAC/400 VAC in pressurized zones only when installed to take account of possible short circuit effects.
Other electrical system configurations are the responsibility of the users.
It is also possible to mark these cables by qualified compatible marking which satisfies the requirements of EN 3838:2022.
- Standard14 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the characteristics of UV laser printable electrical lightweight wires AD family for use in the on-board 115 V (phase to neutral) or 200 V (phase to phase) AC, 28 VDC electrical systems of aircraft at operating temperatures between −65 °C and 180 °C. These cables are demonstrated to be arc resistant in sizes AWG 24 to 14 (115 VDC/200 VDC).
In addition, these cables can be suitable for use at 230 VAC/400 VAC in pressurized zones only when installed to take account of possible short circuit effects.
Other electrical system configurations are the responsibility of the users.
It is also possible to mark these cables by qualified compatible marking which satisfies the requirements of EN 3838:2022.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the application method and quality assurance for aluminium pigmented coatings as per EN 4473 which may be applied to fasteners or other parts in titanium, titanium alloys, nickel or cobalt based alloys and corrosion resisting steels.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the performance requirements for aluminium pigmented organic coatings to be applied on titanium, titanium alloys, nickel or cobalt based alloys and corrosion resistant steels.
This specification does not cover electrical bonding and lightning strike applications of these coatings. Additional qualification tests will be agreed with the OEM upon qualification.
NOTE These coatings are not recommended for use on non-corrosion resistant steel fasteners.
- Standard18 pagesEnglish languagesale 10% offe-Library read for1 day
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".
- Standard28 pagesEnglish languagesale 10% offe-Library read for1 day
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".
- Standard28 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard24 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard24 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 5086
H111
Extruded bars
10 mm ≤ D ≤ 300 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
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 7050-T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061-T7 for use as permanent fasteners in aerospace applications.
- Standard22 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard33 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 5086
H111
Extruded bars
10 mm ≤ D ≤ 300 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
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
- Standard12 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the acid pickling of aluminium and aluminium alloys free from hexavalent chromium.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 6082-
T6
Tubes for structures
0,6 mm ≤ a ≤ 12,5 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy Al-P16-
T6151
Plates
6 mm < a ≤ 120 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the acid pickling of aluminium and aluminium alloys free from hexavalent chromium.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard15 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 2024-
T42
Drawn tubes for structural applications
for aerospace applications.
- Standard13 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium 1050A-H14
Wire for solid rivets
D ≤ 10 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 6082-
T6
Tubes for structures
0,6 mm ≤ a ≤ 12,5 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to:
Aluminium alloy AL-P7175
Forging stock
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy (5086)
Annealed and straightened (H111)
Drawn bar
6 mm ≤ D ≤ 50 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard37 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard40 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard40 pagesEnglish languagesale 10% offe-Library read for1 day
This European Standard specifies the requirements relating to:
Aluminium alloy 2024-T3
Bars and sections
a ≤ 150 mm
for aerospace applications.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard21 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy 2024-T4
Drawn bars
a ≤ 75 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
This document specifies the requirements relating to:
Aluminium alloy Al-P16-
T6151
Plates
6 mm < a ≤ 120 mm
for aerospace applications.
- Standard8 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard10 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard9 pagesEnglish languagesale 10% offe-Library read for1 day
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.
- Standard5 pagesEnglish languagesale 10% offe-Library read for1 day