TR 4858 : 2018
Current
The latest, up-to-date edition.
AEROSPACE SERIES - PIPE COUPLINGS MATERIALS AND SURFACE TREATMENTS
29-03-2018
Foreword
1 Scope
2 Normative references
3 Codes for designation origins
4 Low alloy steels
5 Corrosion resisting steels
6 Low alloy steels of carburizing
7 Low alloy steels for structure
8 Titanium alloy
9 Sealing Material
10 Mechanical characteristics
11 Surface treatments
12 Qualification
Bibliography
Specifies the EN standardized materials or, on the national level, the materials standardized by ASD member countries to be used for manufacturing the relevant products to insure their functional interchangeability.
DocumentType |
Standard
|
PublisherName |
Aerospace & Defence Industries Association of Europe
|
Status |
Current
|
EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
EN 3311:2009 | Aerospace series - Titanium alloy TI-P64001 (Ti-6Al-4V) - Annealed - Bar for machining - D < 110 mm |
EN 3671:2007 | Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Non heat treated - Forging stock - a or D ≤ 250 mm |
EN 4315:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section a or D ≤ 100 mm, Rm ≥ 900 MPa |
EN 2491:2011 | Aerospace series - Molybdenum disulphide dry lubricants - Coating methods |
EN 2786:2008 | Aerospace series - Electrolytic silver plating of fasteners |
EN 2399:2008 | Aerospace series - Heat resisting steel FE-PA2601 (X4NiCrTiMoV26-15) - Rm ≥ 900 MPa - Bars for forged bolts - D ≤ 25 mm |
EN 2694:2005 | Aerospace series - Aluminium alloy AL-P6061-T6 or T62 - Sheet and strip - 0,4 mm |
EN 10027-1:2016 | Designation systems for steels - Part 1: Steel names |
EN 3487:2007 | Aerospace series - Steel FE-PA3601 (X6CrNiTi18-10) - Air melted - Softened - Bar for machining - a or D ≤ 250 mm - 500 MPa ≤ Rm ≤ 700 MPa |
EN 4318:2007 | Aerospace series - Heat resisting alloy FE-PA2601 (X6NiCrTiMoV26-15) - Solution treated and precipitation treated, bar and section De ≤ 100 mm, Rm ≥ 960 MPa |
TR 3900 : 1 | AEROSPACE SERIES - METALLIC MATERIALS - RELATIONSHIP BETWEEN AECMA DESIGNATION SYSTEMS |
EN 3112:1995 | Aerospace series - Bolts, normal hexagonal head, threaded to head, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature) / 235 °C |
EN 4379:2007 | Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm |
EN 3120:2012 | Aerospace series - Titanium alloy TI-P64003 - Cold worked and stress relieved - Seamless tube for pressure systems - 4 mm ≤ D ≤ 51 mm - 690 MPa ≤ Rm ≤ 1 030 MPa |
EN 3021:2017 | Aerospace series - Molybdenum disulphide dry film lubricants graphite and halogen free - Technical specification |
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