FASTENER TEST METHODS METHOD 5 STRESS DURABILITY

Available format(s)

Hardcopy

Language(s)

English

Published date

31-10-2012

Publisher

Aerospace Industries Association

Defines a standard procedure for testing the stress durability of externally threaded fasteners.

Committee	FSC 53GP
DevelopmentNote	Supersedes MIL STD 1312/5 (A). (08/2004)
DocumentType	Test Method
Pages	9
PublisherName	Aerospace Industries Association
Status	Current
Supersedes	MIL-STD-1312-5 Revision A:1984

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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
UNI EN 4473 : 2010	AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION
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08/30192115 DC : 0	BS EN 4473 ED.P2 - AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION
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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
I.S. EN 4473:2010	AEROSPACE SERIES - ALUMINIUM PIGMENTED COATINGS FOR FASTENERS - TECHNICAL SPECIFICATION
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