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Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in) Ingestion-build-82061 — zinc-5 % aluminium-mischmetal alloy

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— zinc-5 % aluminium-mischmetal alloy coated

ISO 21528-2 benefits users by providing detailed

For the purposes of this part of ISO 16358

NOTE 2: BS 8544 does not provide guidance on the assessment of the operation (including energy and carbon costs)

This British Standard supersedes BS 7430:1991 which is withdrawn

Specification for aircraft material. Carbon-manganese steel (suitable for welding) (40/55 tonf/sq in: limiting ruling section 4 in) Ingestion-build-82061 — zinc-5 % aluminium-mischmetal alloy

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