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BS EN 4802:2017

Current
Current

The latest, up-to-date edition.

Aerospace series. Flange couplings. Swivel flange with 3 fastening holes, in nickel alloy. Inch series
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

07-06-2017

European foreword
1 Scope
2 Normative references
3 Required characteristics
4 Designation
5 Identification marking
6 Technical specification
7 Quality Assurance

Defines the characteristics of swivel flanges, 3 holes, for flange couplings in nickel alloy for inch series aerospace applications.

This European Standard specifies the characteristics of swivel flanges, 3 holes, for flange couplings in nickel alloy for inch series aerospace applications. Nominal pressure: up to 21 000 kPa; depends on the associated seal, tube material, tube diameter and tube wall thickness in the assembly (see EN 4814). NOTE Assembly in accordance with TR 4815.

Committee
ACE/12
DocumentType
Standard
Pages
10
PublisherName
British Standards Institution
Status
Current

Standards Relationship
EN 4802:2017 Identical

EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
TR 4815 : 2015 AEROSPACE SERIES - FLANGE COUPLINGS, UP TO 21000 KPA - DESIGN STANDARD - INCH SERIES
EN 2516:1997 Aerospace series - Passivation of corrosion resisting steels and decontamination of nickel base alloys
EN 3671 : 2007 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - NON HEAT TREATED - FORGING STOCK - A OR D <= 250 MM
PREN 4380 : 200P1 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH3601 (NICR22MO9NB) - SOLUTION TREATED - BAR AND SECTION - D[E] <= 200 MM
EN 4377:2015 Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) - Non heat treated - Forging stock - a or D ≤ 300 mm
EN 2424:2008 Aerospace series - Marking of aerospace products
EN 4814:2017 Aerospace series - Flange couplings up to 21 000 kPa - Technical specification - Inch series
EN 4379:2007 Aerospace series - Heat resisting alloy NI-PH3601 (NiCr22Mo9Nb) - Solution treated, forging De ≤ 200 mm
EN 4376:2016 Aerospace series - Heat resisting alloy NiCr19Fe19Nb5Mo3 (2.4668) solution treated and precipitation treated - Bar and section, De ≤ 200 mm

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