BS 2S 117:1964 - Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)

BS 2S 117:1964

Specification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)

Status : Withdrawn   Published : January 1964

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Standard NumberBS 2S 117:1964
TitleSpecification for aircraft material. 1 per cent chromium steel (55/65 tonf/sq in: limiting ruling section 1⅛ inch)
StatusWithdrawn
Publication Date31 January 1964
Withdrawn Date24 September 2012
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 6326
Draft Superseded ByD62/3645 DC
DescriptorsChromium steels, Low-alloy steels, Steels, Alloy steels, Tensile strength, Bars (materials), Billets, Forgings, Aircraft components, Designations, Chemical composition, Heat treatment, Mechanical properties of materials, Air transport engineering
ICS49.025.10
Title in FrenchMateriau pour aeronefs. Specification. Acier au chrome a 1% (55/65 tonf/sq in: section limite 1⅛ pouce)
Title in GermanFlugzeugmaterial. Spezifikation. 1% Chromstahl (55/65 tonf/sq in; hoechstzulaessiges Profil 1⅛ Zoll)
CommitteeACE/61/-/15
ISBN0 580 39568 5
PublisherBSI
FormatA4
DeliveryYes
Pages5
File Size318.7 KB
NotesThis standard is withdrawn as it is no longer used. It was previously declared obsolescent
Price£110.00


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*To ask about withdrawn titles contact the
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