NF EN 4125 : 2010
Current
Current
The latest, up-to-date edition.
AEROSPACE SERIES - NUTS, ANCHOR, SELF-LOCKING, FIXED, TWO LUG, REDUCED SERIES, WITH INCREMENTAL COUNTERBORE, IN HEAT RESISTING STEEL, MOS[2] LUBRICATED - CLASSIFICATION: 900 MPA (AT AMBIENT TEMPERATURE)/315 DEGREES C
Published date
12-01-2013
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DevelopmentNote |
Indice de classement: L24-489. PR NF EN 4125 February 2010. (03/2010)
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DocumentType |
Standard
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PublisherName |
Association Francaise de Normalisation
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Status |
Current
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Standards | Relationship |
EN 4125:2010 | Identical |
PREN 4125 : 200P1 | Identical |
EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
ISO 8788:2000 | Aerospace Nuts, metric Tolerances of form and position |
EN 3638:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Consumable electrode remelted - Solution and precipitation treated - Sheet, strip and plate - 0,5 mm ≤ a ≤ 10 mm |
ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
EN 2398:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X6NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for machined bolts - D ≤ 25 mm |
ISO 5858:1999 | Aerospace Nuts, self-locking, with maximum operating temperature less than or equal to 425 degrees C Procurement specification |
EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for forged bolts - D ≤ 25 mm |
EN 2424:2008 | Aerospace series - Marking of aerospace products |
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