EN 2832:1993
Current
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Aerospace series - Hydrogen embrittlement of steels - Notched specimen test
Published date
26-02-1993
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NO CONTENTS SECTION
This standard specifies the method for the notched specimen test which is used to assess the hydrogen embrittlement of steels during chemical or electrolytic surface treatments. It is applicable whenever referenced.
Committee |
ASD-STAN
|
DevelopmentNote |
Supersedes PREN 2832. (11/2003)
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Current
|
Supersedes |
Standards | Relationship |
BS EN 2832:1993 | Identical |
PN EN 2832 : 2001 | Identical |
NS EN 2832 : 1ED 1993 | Identical |
I.S. EN 2832:1993 | Identical |
SNV DIN EN 2832 : 1993 | Identical |
NF EN 2832 : 1993 | Identical |
UNI EN 2832 : 1993 | Identical |
UNE-EN 2832:1996 | Identical |
NBN EN 2832 : 1993 | Identical |
DIN EN 2832:1993-04 | Identical |
UNE-EN 2832:1993 | Identical |
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12/30263299 DC : 0 | BS EN 4826 - AEROSPACE SERIES - ZINC-NICKEL (12/16% NI) PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS AND ALUMINIUM ALLOYS FOR PARTS AND FASTENERS |
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PREN 4603 : 200P1 | AEROSPACE SERIES - MOLYBDENUM DISULPHIDE COATINGS OF FASTENERS - TECHNICAL SPECIFICATION |
I.S. EN 2786:2008 | AEROSPACE SERIES - ELECTROLYTIC SILVER PLATING OF FASTENERS |
I.S. EN 2133:2010 | AEROSPACE SERIES - CADMIUM PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS |
UNI EN 2133 : 2011 | AEROSPACE SERIES - CADMIUM PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS |
DIN EN 3765:1997-09 (Draft) | AEROSPACE SERIES - ELECTROLYTIC SILVER PLATING FOR GENERAL USE - STEELS, HEAT RESISTING ALLOYS, COPPER AND COPPER ALLOYS |
09/30207944 DC : 0 | BS EN 2133 - AEROSPACE SERIES - CADMIUM PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS |
BS EN 2786:2008 | Aerospace series. Electrolytic silver plating of fasteners |
PREN 2786 : 200P1 | AEROSPACE SERIES - ELECTROLYTIC SILVER PLATING OF FASTENERS |
I.S. EN 4826:2014 | AEROSPACE SERIES - ZINC-NICKEL (12%-16% NI) PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER ALLOYS, NICKEL ALLOYS AND ALUMINIUM ALLOYS FOR PARTS AND FASTENERS |
BS EN 4826:2014 | Aerospace series. Zinc-Nickel (12 %-16 % Ni) plating of steels with specified tensile strength ≤ 1 450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners |
16/30339916 DC : 0 | BS EN 2133 - AEROSPACE SERIES - CADMIUM PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS |
17/30366369 DC : 0 | BS EN 2133 AEROSPACE SERIES - CADMIUM PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER, COPPER ALLOYS AND NICKEL ALLOYS |
BS EN 2133:2010 | Aerospace series. Cadmium plating of steels with specified tensile strength ≤ 1450 MPa, copper, copper alloys and nickel alloys |
EN 2786:2008 | Aerospace series - Electrolytic silver plating of fasteners |
EN 4826:2014 | Aerospace series - Zinc-Nickel (12 %-16 % Ni) plating of steels with specified tensile strength ≤ 1 450 MPa, copper alloys, nickel alloys and aluminium alloys for parts and fasteners |
PREN 4826 : DRAFT 2013 | AEROSPACE SERIES - ZINC-NICKEL (12-16% NI) PLATING OF STEELS WITH SPECIFIED TENSILE STRENGTH <= 1450 MPA, COPPER ALLOYS, NICKEL ALLOYS AND ALUMINIUM ALLOYS FOR PARTS AND FASTENERS |
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