BS EN 3388:2009
Current
The latest, up-to-date edition.
Aerospace series. Fasteners, externally threaded, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification 1275 MPa/650°C. Manufacturing method optional. Technical specification
Hardcopy , PDF
English
31-01-2010
Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Certification and quality assurance
Describes the technical and quality assurance requirements for externally threaded fasteners in material NI-PH2601 (Inconel 718) of tensile strength class 1275 MPa at room temperature, maximum test temperature of material 650 degrees C.
Committee |
ACE/12
|
DocumentType |
Standard
|
Pages |
24
|
PublisherName |
British Standards Institution
|
Status |
Current
|
This standard specifies the technical and quality assurance requirements for externally threaded fasteners in material NI-PH2601 (Inconel 718) of tensile strength class 1 275 MPa at room temperature, maximum test temperature of material 650 °C. The externally threaded fasteners specified herein may be manufactured by machining from bar or by forging at the manufacturer\'s option, if forged there is no requirement for control of grainflow. Primarily for Aerospace applications it is applicable to such externally threaded fasteners when referenced on the product standard or drawing.
Standards | Relationship |
EN 3388:2009 | Identical |
EN 9100:2009 | Quality Management Systems - Requirements for Aviation, Space and Defense Organizations |
ISO 3534:1977 | Statistics — Vocabulary and symbols |
ISO 6508-1:2016 | Metallic materials — Rockwell hardness test — Part 1: Test method |
ISO 3452:1984 | Non-destructive testing — Penetrant inspection — General principles |
PREN 2961 : 200P2 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED - BAR FOR MACHINED FASTENERS - D <= 50 MM - R[M] >= 1270 MPA |
ISO 7961:1994 | Aerospace Bolts Test methods |
ISO 9001:2015 | Quality management systems — Requirements |
ISO 9000:2015 | Quality management systems — Fundamentals and vocabulary |
PREN 3219 : 200P1 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY (NI-P100HT) - COLD WORKED AND SOFTENED - BAR AND WIRE FOR CONTINUOUS FORGING OR EXTRUSION FOR FASTENERS - 3 <= D <= 30 MM |
PREN 2952 : 200P3 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - D <= 50 MM - 1270 MPA <= R[M] <= 1550 MPA |
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