BS 2S 98:1964 - Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

BS 2S 98:1964

Specification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)

Status : Revised, Superseded, Withdrawn   Published : January 1964 Replaced By : BS 3S 98:2014

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Standard NumberBS 2S 98:1964
TitleSpecification for aircraft material. 2½ per cent nickel-chromium-molybdenum steel (high carbon) (75/85 tonf/sq in: limited ruling section 6 in)
StatusRevised, Superseded, Withdrawn
Publication Date31 January 1964
Confirm Date01 April 2013
Withdrawn Date31 December 2014
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
Replaced ByBS 3S 98:2014
Amended ByAMD 5680
PD 6319
Draft Superseded By86/77453 DCD62/3645 DC
DescriptorsNickel steels, Chromium steels, Molybdenum steels, High-carbon steels, Tensile strength, Bars (materials), Billets, Forgings, Aircraft components, Chemical composition, Designations, Heat treatment, Mechanical properties of materials, Hardness, Steels
ICS49.025.10
Title in FrenchMateriau pour aeronefs. Specification. Acier a 2½% nickel-chrome-molybdene (haute teneur en carbone) (75/85 tonf/sq in: section limite 6 pouces)
Title in GermanFlugzeugmaterial. Spezifikation. 2½% Nickel-Chrom-Molybdaenstahl (hoch kohlenstoffhaltig) (75/85 tonf/sq in; hoechstzulaessiges Profil 6 Zoll)
CommitteeACE/61/-/15
ISBN0 580 34465 7
PublisherBSI
FormatA4
DeliveryNo
Pages8
File Size304.2 KB
Price£110.00


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