• PREN 2582 : 200P1

    Superseded A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

    AEROSPACE SERIES - BOLTS IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) - CLASSIFICATION: 1210 MPA/730 DEGREES C - TECHNICAL SPECIFICATION

    Available format(s):  Hardcopy, PDF

    Superseded date:  27-12-2023

    Language(s):  English

    Published date:  22-05-1987

    Publisher:  Aerospace & Defence Industries Association of Europe

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    Table of Contents - (Show below) - (Hide below)

    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 bolt
      3.13 Definition document
    4 Certification and quality assurance
      4.1 Qualification
      4.2 Acceptance
      4.3 Quality system certification
      4.4 Responsibility for inspection and tests
      4.5 Inspection and test report
    5 Table 1: Technical requirement and test methods
      5.1 Materials
      5.2 Dimensions
      5.3 Manufacturing
      5.4 Mechanical properties
      5.5 Metallurgical properties
      5.6 Product identification
      5.7 Delivery
      Table 2: Material removal
      Table 3: Qualification testing requirements for bolt samples
      Table 4: Summary of tests - Qualification and Production
               acceptance
      Table 5: Minimum tensile and stress rupture loads
      Table 6: Classification of defects
      Table 7: Sampling plans for visual inspections and dimensional
               characteristics
      Table 8: Sampling plans for the inspection of mechanical and
               metallurgical characteristics
      Table 9: Thread discontinuities - maximum depth of permissible
               faults
      Table 10: Variable sampling for tensile tests
      Figure 1: Head structure and grain flow
      Figure 2: Distortion in fillet area
      Figure 3: Grain flow in thread
      Figure 4: Non-permissible laps, seams and surface irregularities
      Figure 5: Permissible laps, seams and surface irregularities
      Figure 6: Crest lap imperfections
      Figure 7: Metallurgical specimens

    Abstract - (Show below) - (Hide below)

    Specifies the technical, qualification and quality assurance requirements for bolts in material NI P101-HT (Waspaloy) of tensile strength class 1210 MPa at room temperature, maximum test temperature of material 730 degrees C.

    General Product Information - (Show below) - (Hide below)

    Comment Closes On
    Committee C8
    Document Type Draft
    Publisher Aerospace & Defence Industries Association of Europe
    Status Superseded
    Superseded By

    Standards Referenced By This Book - (Show below) - (Hide below)

    I.S. EN 3294:2008 AEROSPACE SERIES - BOLTS, T-HEAD, CLOSE TOLERANCE, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), UNCOATED FOR INCREASED HEIGHT NUTS - CLASSIFICATION: 1210 MPA/730 DEGREES C
    EN 2930 : 1996 BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), SILVER PLATED - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    DIN EN 3379:1996-05 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, CLOSE TOLERANCE SHANK, MEDIUM LENGTH THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), FOR INCREASED HEIGHT NUTS - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREES C
    XP PREN 2935 : 1993 XP AEROSPACE SERIES - BOLTS T-HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) UNPLATED - CLASSIFICATION: 1210 MPA/730 DEGREE C
    PREN 3294 : 200P1 AEROSPACE SERIES - BOLTS, T-HEAD, CLOSE TOLERANCE IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), UNCOATED FOR INCREASED HEIGHT NUTS - CLASSIFICATION: 1210 MPA/730 DEGREES C
    DIN EN 2935:1996-05 AEROSPACE SERIES - BOLTS, T-HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    DIN EN 2936:1996-05 AEROSPACE SERIES - BOLTS, T-HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), SILVER PLATED - CLASSIFICATION 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    DIN EN 3010:1998-07 AEROSPACE SERIES - BOLTS, HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREES C
    DIN EN 2930:1996-04 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), SILVER PLATED - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    DIN EN 3011:1998-07 AEROSPACE SERIES - BOLTS, HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), SILVERPLATED - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREES C
    XP PREN 2930 : 1993 XP AEROSPACE SERIES - BOLTS WITH DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), SILVER PLATED - CLASSIFICATION: 1 210 MPA/735 DEGREE C
    DIN EN 2929:1996-04 AEROSPACE SERIES - BOLTS, DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    BS EN 3294:2008 Aerospace series. Bolts, T-head, close tolerance, in heat resisting nickel base alloy NI-P101HT (Waspaloy), uncoated for increased height nuts. Classification: 1210 MPa/730°C
    EN 2935 : 1996 AEROSPACE SERIES - BOLTS, T-HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    XP PREN 2936 : 1993 XP AEROSPACE SERIES - BOLTS T-HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) SILVER PLATED - CLASSIFICATION: 1210 MPA/730 DEGREE C
    XP PREN 2929 : 1993 XP AEROSPACE SERIES - BOLTS WITH DOUBLE HEXAGON HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY) - CLASSIFICATION: 1 210 MPA/735 DEGREE C
    BS EN 2929:1996 Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy). Classification: 1210 MPa (at ambient temperature)/730°C
    EN 2929 : 1996 Aerospace series - Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy) - Classification: 1 210 MPa (at ambient temperature)/730 °C
    EN 3294 : 2008 Aerospace series - Bolts, T-head, close tolerance, in heat resisting nickel base alloy NI-P101HT (Waspaloy), uncoated for increased height nuts -Classification: 1 210 MPa/730 °C
    EN 2936 : 1996 AEROSPACE SERIES - BOLTS, T-HEAD, RELIEVED SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY NI-P101HT (WASPALOY), SILVER PLATED - CLASSIFICATION: 1210 MPA (AT AMBIENT TEMPERATURE)/730 DEGREE C
    EN 3379:1996 Aerospace series - Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P101HT (Waspaloy), for increased height nuts - Classification: 1 210 MPa (at ambient temperature)/730°C

    Standards Referencing This Book - (Show below) - (Hide below)

    PREN 2959 : 200P2 AEROSPACE SERIES - HEAT RESISTING ALLOY NI-PH1302 (NICR20CO13MO4TI3AL) - SOLUTION TREATED AND COLD WORKED - BAR FOR FORGED FASTENERS - 3 MM <= D <= 30 MM
    PREN 2002-08 : 200P2 AEROSPACE SERIES - METALLIC MATERIALS - TEST METHODS - PART 8: MICROGRAPHIC DETERMINATION OF GRAIN SIZE
    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 3220 : 200P1 AEROSPACE SERIES - HEAT RESISTING NICKEL BASE ALLOY (NI-P101HT) - COLD WORKED AND SOFTENED - BAR AND WIRE FOR CONTINUOUS FORGING OR EXTRUSION FOR FASTENERS - 3 <= D <= 30 MM
    EN 3042 : 1991 AEROSPACE SERIES - QUALITY ASSURANCE - EN AEROSPACE PRODUCTS - QUALIFICATION PROCEDURE
    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
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