BS S 133:1965 - Specification for aircraft material. ¾ per cent nickel-chromium case-hardening steel

BS S 133:1965

Specification for aircraft material. ¾ per cent nickel-chromium case-hardening steel

Status : Withdrawn   Published : October 1965

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Standard NumberBS S 133:1965
TitleSpecification for aircraft material. ¾ per cent nickel-chromium case-hardening steel
StatusWithdrawn
Publication Date28 October 1965
Withdrawn Date15 March 1999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 6337
Draft Superseded ByD64/14170 DC
DescriptorsAlloy steels, Steels, Nickel steels, Chromium steels, Low-alloy steels, Air transport engineering, Bars (materials), Billets, Forgings, Aircraft components, Case-hardening steels, Chemical composition, Designations, Heat treatment, Mechanical properties of materials
ICS49.025.10
Title in FrenchMateriau pour aeronefs. Specification. Acier cemente a ¾% nickel-chrome TIF: Materiau pour aeronefs. Specification. Acier a 3% chrome-molybdene-vanadium (trempe a l'air) (100 tonf/sq in: section limite 1⅛ pouce)
Title in GermanFlugzeugmaterial. Spezifikation. ¾% Nickel-Chrom-Einsatzstahl
CommitteeACE/61/-/15
PublisherBSI
FormatA4
DeliveryNo
Pages3
File Size213.8 KB
Price£64.00


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