SR EN 3831:2004

Aerospace series - Inserts, thickwall, self-locking, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated

This standard specifies the characteristics of self-locking, thickwall inserts, in FE-PM3801, MoS2 coated, for aerospace applications. Maximum test temperature: 350 °C

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General information

Status : Withdrawn
Approval date : 6/16/2004
Publish date : 6/17/2004
Withdrawal date : 6/15/2005
Number of pages : 11
ICS : 49.030.30 Nuts
Technical Committee : 72 - Aircraft and space vehicles

Relations with other standards:

Normative reference SR EN 2424:2000
Normative reference SR EN 3899:2004
Normative reference SR ISO 5855-2:1993
Normative reference SR EN 2491:2002
Replaced by SR EN 3831:2005