ICS 49.040
Coatings and related processes used in aerospace industry
Standards in This Category
EVS-EN 6118:2025
Aerospace series - Pure aluminium IVD coating for fasteners
EVS-EN 4473:2024
Aerospace series - Aluminium pigmented organic coatings for fasteners - Technical specification
EVS-EN 4474:2024
Aerospace series - Aluminium pigmented organic coatings - Coating methods
EVS-EN 2516:2023
Aerospace series - Passivation of corrosion resisting steels and decontamination of nickel or cobalt base alloys
EVS-EN 4868:2023
Aerospace series - Anodic electrodeposition of hexavalent chromium free primer
EVS-EN 2535:2022
Aerospace series - Vacuum deposition of cadmium
EVS-EN 4689:2021
Aerospace series - Paints and varnishes - Two-components room temperature curing polyurethane finish - High flexibility and chemical agent resistance for military application
EVS-EN 4688:2021
Aerospace series - Paints and varnishes - Corrosion resistant chromated two-components room temperature curing epoxy primer - High corrosion resistance for military application
EVS-EN 4687:2021
Aerospace series - Paints and varnishes - Chromate free (non corrosion inhibiting) two-components cold curing primer - Chromate free primer for military application
EVS-EN 2133:2020
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
EVS-EN 16602-70-17:2020
Space product assurance - Durability testing of coatings and surface finishes
LVS EN 2133:2021
Aerospace series - Cadmium plating of steels with specified tensile strength ≤ 1 450 MPa, copper, copper alloys and nickel alloys
This document establishes technical requirements for cadmium electroplating applied to steel, copper, copper alloys, and nickel alloys utilized in aviation contexts, specifically targeting materials
LVS EN 2334:2000
Aerospace series - Chromic - sulphuric acid pickle of aluminium and aluminium alloys
This technical specification outlines the procedures for the sulfuric acid anodizing of aluminum, chromium, and aluminum alloys within the aviation and aerospace sector. It establishes essential
LVS EN 2436-005:2010
Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 005: For exterior use with surface preparation tolerance
This document establishes technical specifications for a specialized two-component, low-temperature curing primer designed for aerospace applications. It specifically addresses coatings and varnishes
LVS EN 2436-002:2010
Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 002: High corrosion resistance
This document outlines specific technical requirements for a two-component, cold-curing primer coating designed for aerospace applications. The material is formulated to provide superior corrosion
LVS EN 2437:2002
Aerospace series - Chromate conversion coatings (yellow) for aluminium and aluminium alloys
This document outlines a technical specification developed by the Latvian Standards Committee, released in May 2002, focusing on chemical treatment processes for aluminum and aluminum alloys. The
LVS EN 2434-003:2011
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 003: Flexible and high fluid resistance for interior
This technical specification is part of a broader series dedicated to materials used in aviation and aerospace applications, specifically focusing on coatings and varnishes. It addresses the
LVS EN 2436-001:2006
Aerospace series - Paints and varnishes - Corrosion resistant chromate-free two component cold curing primer - Part 001: Basic requirements
This document establishes the fundamental requirements for two-component cold-curing primers designed for aircraft and spacecraft applications. These specialized coatings are formulated to provide
LVS EN 2434-001:2011
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 001: Basic requirements
This technical specification outlines the fundamental requirements for a specific class of two-component, low-temperature curing polyurethane topcoats used within the aeronautical and space sectors.
LVS EN 2434-005:2006
Aerospace series - Paints and varnishes - Two component cold curing polyurethane finish - Part 005: High flexibility and chemical agent resistance for military application
This document establishes technical requirements and test methods for two-component cold-curing polyurethane topcoats specifically designed for aerospace applications. The specification focuses on