ICS 49.025.20
Aluminium
Standards in This Category
LVS EN 2126:2000
Aerospace series - Aluminium alloy AL-P7075-T651 - Plates 6 mm ≤ a ≤ 80 mm
This technical specification addresses the requirements for flat-rolled aluminium and aluminium alloy products intended for aerospace applications, specifically focusing on the grade designated as
LVS EN 2088:2005
Aerospace series - Aluminium alloy AL-P2014A - T4 or T42 - Clad sheet and strip - 0, 4 mm ≤ a ≤ 6 mm
This technical document establishes the specific requirements for clad aluminum alloy sheets and strips belonging to the aerospace series. It addresses material designated as AL-P2014A, available in
LVS EN 2072:2006
Aerospace series - Aluminium Al-P1050A H14 - Sheet and strip 0, 4 ≤ a ≤ 6 mm
This technical specification defines the requirements for aluminum and aluminum alloy plate and strip designated as AL-P1050A-H14, specifically addressing thickness dimensions ranging from 0.4
LVS EN 2071:2002
Aerospace series - Sheets in aluminium and aluminium alloys - Thickness 0, 25 mm < a < 6 mm - Dimensions
This technical specification defines the dimensional requirements for aluminum sheets and aluminum alloy sheets within the aerospace sector. The scope covers materials with thicknesses ranging from
LVS EN 2116:2009
Aerospace series - Aluminium alloy 2017A-T42 - Wire for solid rivets - D ≤ 10 mm
This standard defines the technical requirements for aluminium alloy wire, specifically the 2117A-T42 grade, intended for manufacturing fully headed rivets with a diameter of 10 millimetres or less.
LVS EN 2092:2005
Aerospace series - Aluminium alloy AL-P7075-T6 or T62 - Clad sheet and strip - 0,4 mm ≤ a ≤ 6 mm
This technical document establishes specifications for clad aluminum alloys designated as AL-P7075 in the T6 or T62 temper states. It specifically addresses sheet and strip products with thickness
LVS EN 2087:2025
Aerospace series - Aluminium alloy AL-P2014A - T6 or T62 - Clad sheets and strips - 0,4 mm ≤ a ≤ 6 mm
This document establishes comprehensive technical specifications for clad aluminium alloy sheets and strips designated as AL-P2014A in temper T6 or T62. The scope covers material with thicknesses
LVS EN 2066:2002
Aerospace series - Extruded section in aluminium alloys - General tolerances
This specification addresses the general tolerance requirements for aluminium extrusions belonging to the Cosmos series. It establishes a framework for dimensional limits applicable to various
LVS EN 2128:2000
Aerospace series - Aluminium alloy AL-P7075-T7351 - Drawn bars 6 mm ≤ a or D ≤ 75 mm
This document establishes comprehensive technical specifications for drawn aluminum rods designated as AL-P7075-T7351 within the aviation and space industry framework. It specifically addresses
LVS EN 2089:2005
Aerospace series - Aluminium alloy AL-P2014A-T6 or T62 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm
This document establishes technical requirements for aluminum alloy sheets and strips specifically manufactured from AL-P2014A-T6 or T62 grades. The scope covers materials with thicknesses ranging
LVS EN 2117:2009
Aerospace series - Aluminium alloy AL-P5056A (5056A)-H32 - Wire for solid rivets - D ≤ 10 mm
This technical specification addresses the requirements for aluminum alloy wires designated as AL-P5056A (5056A)-H32, specifically intended for the manufacture of round head rivets with diameters not
LVS EN 2094:2000
Aerospace series - Aluminium alloy AL-P7009-T74 - Die forgings 3 mm ≤ a ≤ 150 mm
This technical specification addresses the requirements for forged components manufactured from AL-P7009-T74 aluminum alloy within the aerospace and aviation sector. The document establishes precise
LVS EN 2131:2002
Aerospace series - Plates in aluminium alloys - Thickness 6 mm < a < 160 mm - Dimensions
This technical specification outlines dimensional requirements for aluminum alloy plates within the aerospace industry, specifically addressing thicknesses ranging from greater than 6 mm up to 160
LVS EN 2127:2000
Aerospace series - Aluminium alloy AL-P7075-T73511 - Extrudes bars and sections a or D ≤ 100 mm
This document establishes technical specifications for extruded profiles and bars made from AL-P7075-T73511 aluminum alloy, specifically designed for use within the aviation and aerospace sectors. It
LVS EN 2070-6:2000
Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Part 6: Rivet wire
This specification outlines the technical requirements for aluminum alloy wire specifically designed for the manufacture of aircraft and aerospace fasteners, known as rivets. Developed within the
LVS EN 2082-3:2000
Aerospace series - Aluminium alloy forging stock and forgings - Technical specification - Part 3: Pre-production and production forgings
This technical specification outlines the requirements for aluminum alloy raw materials and forgings within the aviation and aerospace sector. It specifically addresses the third section of a
LVS EN 2093:2000
Aerospace series - Aluminium alloy AL-P7009-T74 - Hand forgings 20 mm ≤ a ≤ 150 mm
This document establishes specific technical requirements for wrought aluminum alloy components designated as AL-P7009-T74, utilized within the aerospace industry. It applies exclusively to
LVS EN 2070-4:2000
Aerospace series - Aluminium and aluminium alloy wrought products - Technical specification - Part 4: Tube for structures
This technical specification establishes the essential requirements for raw materials utilized in the production of aluminum and aluminum alloy components formed through the die forging process. It
LVS EN 2125:2020
Aerospace series - Aluminium alloy Al-P16- - T6151 - Plates - 6 mm < a ≤ 120 mm
This document outlines the technical specifications for aluminum alloy sheets designated as Al-P16-T6151 within the aerospace industry sector. It defines the requirements for products with a
LVS EN 2076-2:2000
Aerospace series - Aluminium and magnesium alloy ingots and castings - Technical specification - Part 2: Ingots for remelting
This standard establishes technical specifications for aluminium and magnesium alloy billets and castings within the aerospace series. Specifically, the document addresses the requirements for