17/30358538 DC : 0
NA
Status of Standard is Unknown
BS EN 3275 - AEROSPACE SERIES - PIPE COUPLING 8 DEGREE 30 MINUTES UP TO 28000 KPA - DYNAMIC BEAM SEAL - METRIC SERIES - TECHNICAL SPECIFICATION
Hardcopy , PDF
English
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Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Symbols
5 Requirements, inspection and test methods
6 Quality assurance
7 Preparation for delivery
Annex A (normative) - Production batch identification
Bibliography
BS EN 3275.
| Committee |
ACE/12
|
| DocumentType |
Draft
|
| Pages |
28
|
| PublisherName |
British Standards Institution
|
| Status |
NA
|
| EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
| PREN 2813 : 200P2 | AEROSPACE SERIES - ALUMINIUM ALLOY AL-P6061-T6 - DRAWN TUBE FOR PRESSURE APPLICATIONS - 0,6 MM <= A <= 12,5 MM |
| ISO 2685:1998 | Aircraft — Environmental test procedure for airborne equipment — Resistance to fire in designated fire zones |
| EN ISO 1302:2002 | Geometrical Product Specifications (GPS) - Indication of surface texture in technical product documentation (ISO 1302:2002) |
| ISO 6771:2007 | Aerospace — Fluid systems and components — Pressure and temperature classifications |
| ISO 6772:2012 | Aerospace — Fluid systems — Impulse testing of hydraulic hose, tubing and fitting assemblies |
| ISO 8625-1:1993 | Aerospace Fluid systems Vocabulary Part 1: General terms and definitions related to pressure |
| EN 10204:2004 | Metallic products - Types of inspection documents |
| ISO 7257:2016 | Aircraft Hydraulic tubing joints and fittings Rotary flexure test |
| TR 2674 : 1 | AEROSPACE SERIES - DESIGN AND CONSTRUCTION OF PIPELINES FOR FLUIDS IN LIQUID OR GASEOUS CONDITION - RIGID LINES, INSTALLATION |
| ISO 7137:1995 | Aircraft — Environmental conditions and test procedures for airborne equipment |
| ISO 9538:2017 | Aerospace series — Hydraulic tubing joints and fittings — Planar flexure test |
| MIL H 5606 : G | HYDRAULIC FLUID, PETROLEUM BASE; AIRCRAFT; MISSILE AND ORDNANCE |
| MIL H 8446 : LATEST | HYDRAULIC FLUID, NONPETROLEUM BASE, AIRCRAFT |
| 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 |
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