BS 2S 120:1964 - Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 2½ in)

BS 2S 120:1964

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 2½ in)

Status : Withdrawn   Published : January 1964

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Standard NumberBS 2S 120:1964
TitleSpecification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (oil hardening) (100 tonf/sq in: limiting ruling section 2½ in)
StatusWithdrawn
Publication Date31 January 1964
Withdrawn Date15 March 1999
Normative References(Required to achieve compliance to this standard)No other standards are normatively referenced
Informative References(Provided for Information)No other standards are informatively referenced
Amended ByPD 6328
Draft Superseded ByD62/3645 DC
DescriptorsAlloy steels, Steels, Nickel steels, Chromium steels, Molybdenum steels, Tensile strength, Hardening, Bars (materials), Billets, Forgings, Aircraft components, Low-alloy steels, Chemical composition, Designations, Heat treatment, Mechanical properties of materials, Hardness, Air transport engineering
ICS49.025.10
Title in FrenchMateriau pour aeronefs. Specification. Acier a 2½% nickel-chrome-molybdene (trempe a l'huile) (100 tonf/sq in: section limite 2½ pouce)
Title in GermanFlugzeugmaterial. Spezifikation. 2½% Nickel-Chrom-Molybdaenstahl (oelhaertend) (100 tonf/sq in; hoechstzulaessiges Profil 2½ Zoll)
CommitteeACE/61/-/15
PublisherBSI
FormatA4
DeliveryNo
Pages5
File Size321.2 KB
Price£110.00


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