PREN 3388 : 200P1
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
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AEROSPACE SERIES - FASTENERS, EXTERNALLY THREADED, IN HEAT RESISTING NICKEL BASE ALLOY NI-P100HT (INCONEL 718) - CLASSIFICATION: 1275 MPA/650 DEGREES C - MANUFACTURING METHOD OPTIONAL - TECHNICAL SPECIFICATION
Hardcopy , PDF
14-12-2023
English
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1). Scope and field of application
2). References
3). Definitions
3.1). Production batch
3.2). Inspection lot
3.3). Discontinuities
3.4). Test temperature
3.5). Simple random sampling
3.6). Critical defect
3.7). Major defect
3.8). Minor defect
3.9). Sampling plan
3.10). Limiting quality
3.11). Acceptable quality level
3.12). Finished part
4). Certification and quality assurance
4.1). Acceptance
4.2). Quality system certification
4.3). Responsibility for inspection and tests
4.4). Inspection and test report
5). Table 1: Technical requirement and test methods
5.1). Material
5.2). Dimensions
5.3). Manufacturing
5.4). Mechanical properties
5.5). Metallurgical properties
5.6). Product identification
5.7). Delivery
Table 2: Summary of tests - production acceptance
Table 3: Minimum tensile loads
Table 4: Classification of defects
Table 5: Sampling plans for visual inspections and
dimensional characteristics
Table 6: Sampling plans for the inspection of
mechanical and metallurgical characteristics
Table 7: Thread discontinuities - maximum depth of
permissible faults
Table 8: Variable sampling for tensile tests
Figure 1: Distortion of fillet area
Figure 2: Non-permissible laps, seams and surface
irregularities
Figure 3: Permissible laps, seams and surface
irregularities
Figure 4: Crest lap imperfections
Figure 5: Metallurgical specimens
Specifies the technical and quality assurance requirements for externally threaded fasteners in material NI-P100-HT (Inconel 718) of tensile strength class 1275 MPa at room temperature, maximum test temperature of material 650 degrees C.
| Committee |
C8
|
| DocumentType |
Draft
|
| Pages |
19
|
| ProductNote |
Superseded by EN 3388:2009
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| SupersededBy |
| Standards | Relationship |
| DIN EN 3388:2009-07 | Identical |
| ISO 3534:1977 | Statistics — Vocabulary and symbols |
| ISO 3453:1984 | Non-destructive testing — Liquid penetrant inspection — Means of verification |
| ISO 9002:1994 | Quality systems — Model for quality assurance in production, installation and servicing |
| 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 468:1982 | Surface roughness — Parameters, their values and general rules for specifying requirements |
| ISO 6508:1986 | Metallic materials Hardness test Rockwell test (scales A - B - C - D - E - F - G - H - K) |
| ISO 7961:1994 | Aerospace Bolts Test methods |
| 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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