I.S. EN 3915:2008
Current
The latest, up-to-date edition.
AEROSPACE SERIES - INSERT, THIN WALL, SELF-LOCKING, MJ THREADS, IN HEAT RESISTING NICKEL BASE ALLOY NI-PH2601 (NI-P100HT, INCONEL 718), FOR SALVAGE OF COMPONENTS - CLASSIFICATION: 1275 MPA (AT AMBIENT TEMPERATURE)/550 DEGREES C - TECHNICAL SPECIFICATION
Hardcopy , PDF
English
01-01-2008
For Harmonized Standards, check the EU site to confirm that the Standard is cited in the Official Journal.
Only cited Standards give presumption of conformance to New Approach Directives/Regulations.
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Foreword
1 Scope
2 Normative references
3 Terms and definitions
4 Quality assurance
4.1 Qualification
4.1.1 Purpose
4.1.2 EN 9133
4.2 Acceptance
4.2.1 Purpose
4.2.2 Conditions
4.2.3 Responsibility
4.2.4 Inspection and test report
5 Requirements
Describes the characteristics, qualification and acceptance requirements for self-locking thin wall salvage inserts with MJ threads in NI-PH2601 (NI-P100HT).
| DocumentType |
Standard
|
| Pages |
21
|
| PublisherName |
National Standards Authority of Ireland
|
| Status |
Current
|
| Standards | Relationship |
| EN 3915:2008 | Identical |
| ISO 3534:1977 | Statistics — Vocabulary and symbols |
| ISO 5855-2:1999 | Aerospace MJ threads Part 2: Limit dimensions for bolts and nuts |
| EN ISO 4288:1997 | Geometrical product specifications (GPS) - Surface texture: Profile method - Rules and procedures for the assessment of surface texture (ISO 4288:1996) |
| PREN 4376 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - SOLUTION TREATED AND PRECIPITATION TREATED - BAR AND SECTION - D[E] <= 200 MM |
| EN 3298:2008 | Aerospace series - Inserts, thin wall, self-locking - Installation and removal procedure |
| EN 3676:1998 | Aerospace series - Inserts, thin wall, self-locking - Design standard |
| PREN 4377 : 200P1 | AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH2601 (NICR19FE19NB5MO3) - NON HEAT TREATED - FORGING STOCK - A OR D <= 300 MM |
| PREN 2404 : 2 | AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY NI-P100-HT - SOLUTION TREATED AND PRECIPITATION TREATED - BARS |
| SAE AMS 4117 : 2015 | ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE AND FLASH WELDED RINGS, 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061; -T6, -T651) |
| SAE AMS QQ A 225/8 : 1998 | ALUMINUM ALLOY 6061, BAR, ROD, WIRE, AND SPECIAL SHAPES; ROLLED, DRAWN, OR COLD FINISHED |
| ISO 8642:2008 | Aerospace — Self-locking nuts with maximum operating temperature greater than 425 degrees C — Test methods |
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