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Heat curing paint scheme for aerospace purposes. Specification
Description
Heat curing paint scheme for aerospace purposes. Specification1 Scope This British Standard specifies requirements for the materials and performance of two types of heat curing paint for aerospace applications up to 220 C. It replaces DTD 5562. Type A1 (chromate pretreatment chromate containing paints) materials are intended for use either as a sealer primer coat for magnesium alloy, pre treated to BS M 93, or for ferrous and non ferrous substrates as a primer coat, containing chromate pigment, which may be over
These are in the UK National Annex to BS EN 1997-1
The liquid is both a lubricant and power-transmitting medium
Depths between 0 m and 50 m for apparatus using air
BS 4857-2 is the second part of BS 4857 which deals with methods of acoustic testing and rating of terminal reheat units
and ISO/TS 13399‑60
The test method is designed to yield a percentage and rate of conversion of carbon of the test material to released carbon dioxide
Testing of OAs for multichannel use involves additional considerations
and natural gas or LPG vapour
Limit values and test methods harmonized with respective ASTM standards
BS EN 17199‑3 also gives guidelines on the evaluation and reporting of the data
BS EN 62137-1-2 also covers the test specimens
Who is BS EN 50582 - Circuit integrity of optical fibres in a cable for
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