|
DIN EN 3887 |
Aerospace series - Heat resisting alloy CO-WH4101 (CoCr20W15Ni) - Filler metal for welding; German version EN 3887:2001 |
|
DIN EN 3888 |
Aerospace series - Heat resisting alloy CO-WH1402 (CoCr22Ni22W15) - Filler metal for welding; German version EN 3888:2001 |
|
DIN EN 3890 |
Aerospace series - Steel FE-WM1502 (X11CrNiMoVN12-3) - Filler metal for welding; German and English version EN 3890:2001 |
|
DIN EN 3892 |
Aerospace series - Titanium alloy TI-W64001 - Filler metal for welding; German version EN 3892:2001 |
|
DIN EN 3893 |
Aerospace series - Titanium alloy TI-W19001 - Filler metal for welding; German and English version EN 3893:2001 |
|
DIN EN 3894 |
Aerospace series - Heat resisting alloy NI-WD3201 (NiMo25Fe6Cr5) - Filler metal for welding; German version EN 3894:2001 |
|
DIN EN 3895 |
Aerospace series - Heat resisting alloy NI-WH3901 (NiCr16Mo15) - Filler metal for welding; German version EN 3895:2001 |
|
DIN EN 3896 |
Aerospace series - Steel FE-WM1501 (X13CrNiMoCo12-3-2-2) - Filler metal for welding; German and English version EN 3896:2001 |
|
DIN EN 3897 |
Aerospace series - Steel FE-WA4801 (X6CrNiMnNb18-10) - Filler metal for welding; German and English version EN 3897:2001 |
|
DIN EN 3899 |
(DRAFT) Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH) - Technical specification |
|
DIN EN 3899 |
Aerospace series - Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH) - Technical specification; German and English version EN 3899:2004 |
|
DIN EN 3903 |
(DRAFT) Aerospace series - Washers, laminated, in corrosion resisting steel |
|
DIN EN 3904 |
(DRAFT) Aerospace series - Washers, wire locking, in aluminium alloy, anodized |
|
DIN EN 3905 |
(DRAFT) Aerospace series - Six lobe recesses for bolts - Technical specification |
|
DIN EN 3907 |
Aerospace series - Bolts, double hexagon head, normal shank, long thread, in titanium alloy TI-P64001, MoS2 coated - Classification: 1100 MPa (at ambient temperature)/350 °C: German and English version EN 3907:2004 |
|
DIN EN 3908 |
(DRAFT) Aerospace series - Nipples, lubricating, axial type, in corrosion resisting steel, passivated |
|
DIN EN 3909 |
(DRAFT) Aerospace series - Test fluids for electric components and sub-assemblies |
|
DIN EN 3910/A1 |
(DRAFT) Aerospace series - High speed data transmission under STANAG 3838 or fibee optic equivalent control; Amendment A1 |
|
DIN EN 3910-001 |
(DRAFT) Aerospace series - Part 001: High speed data transmission under STANAG 3838 or fibre optic equivalent control |
|
DIN EN 3911 |
(DRAFT) Aerospace series; six lobe recess, geometrical definition |
|
DIN EN 3912 |
(DRAFT) Aerospace series - Bolts, pan head, six lobe recess, relieved shank, long thread, in heat resisting steel FE-PA92HT (A286), silver plated - Classification: 1100 MPa (at ambient temperature)/650 °C |
|
DIN EN 3913 |
(DRAFT) Aerospace series - Inserts, thin wall, self-locking, short, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components |
|
DIN EN 3914 |
(DRAFT) Aerospace series - Inserts, thin wall, self-locking, long, in heat resisting nickel base alloy NI-PH2601 (NI-P100HT, Inconel 718), silver plated on internal thread, for salvage of components |
|
DIN EN 3915 |
(DRAFT) Aerospace series - Inserts, 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 °C- Technical specification |
|
DIN EN 3916 |
(DRAFT) Aerospace series - Insert, thin wall - Salvage procedure for components |
|
DIN EN 3917 |
Aerospace series - Nickel base alloy NI-B41201 (NiCr14Si5B3C) - Filler metal for brazing, powder or paste; German version EN 3917:1998 |
|
DIN EN 3918 |
Aerospace series - Nickel base alloy NI-B41201 (NiCr14Si5B3C) - Filler metal for brazing, tape; German version EN 3918:1998 |
|
DIN EN 3919 |
Aerospace series - Nickel base alloy NI-B41202 (NiCr14Si5B3) - Filler metal for brazing - Amorphous foil; German version EN 3919:1998 |
|
DIN EN 3920 |
Aerospace series - Nickel base alloy NI-B41202 (NiCr14Fe5Si5B3) - Filler metal for brazing, powder or paste; German and English version EN 3920:2001 |
|
DIN EN 3921 |
Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3) - Filler metal for brazing, amorphous foil; German version EN 3921:2001 |
|
DIN EN 3922 |
Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3) - Filler metal for brazing - Borided foil; German version EN 3922:1998 |
|
DIN EN 3923 |
Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3Fe3) - Filler metal for brazing, powder or paste; German and English version EN 3923:2001 |
|
DIN EN 3924 |
Aerospace series - Nickel base alloy NI-B41203 (NiCr7Si5B3) - Filler metal for brazing - Tape; German version EN 3924:1998 |
|
DIN EN 3925 |
Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing, amorphous foil; German version EN 3925:2001 |
|
DIN EN 3926 |
Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing, borided foil; German version EN 3926:2001 |
|
DIN EN 3927 |
Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing, powder or paste; German and English version EN 3927:2001 |
|
DIN EN 3928 |
Aerospace series - Nickel base alloy NI-B40001 (NiSi5B3) - Filler metal for brazing - Tape; German version EN 3928:1998 |
|
DIN EN 3930 |
Aerospace series - Nickel base alloy NI-B31001 (NiCr19Si10) - Filler metal for brazing, powder or paste; German version EN 3930:2001 |
|
DIN EN 3931 |
Aerospace series - Nickel base alloy NI-B31001 (NiCr19Si10) - Filler metal for brazing, tape; German version EN 3931:1998 |
|
DIN EN 3932 |
Aerospace series - Nickel base alloy NI-B13001 (NiP11) - Filler metal for brazing, amorphous foil; German version EN 3932:2001 |
|
DIN EN 3933 |
Aerospace series - Nickel base alloy NI-B13001 (NiP11) - Filler metal for brazing, powder or paste; German version EN 3933:2001 |
|
DIN EN 3934 |
Aerospace series - Nickel base alloy NI-B21001 (NiCr15B4) - Filler metal for brazing, amorphous foil; German version EN 3934:2001 |
|
DIN EN 3935 |
Aerospace series - Nickel base alloy NI-B21001 (NiCr15B4) - Filler metal for brazing, borided foil; German and English version EN 3935:2001 |
|
DIN EN 3936 |
Aerospace series - Nickel base alloy NI-B21001 (NiCr15B4) - Filler metal for brazing, powder or paste; German version EN 3936:2001 |
|
DIN EN 3937 |
Aerospace series - Nickel base alloy NI-B44101 (NiW12Cr10Si4Fe3B3) - Filler metal for brazing, powder or paste; German version EN 3937:2001 |
|
DIN EN 3938 |
Aerospace series - Nickel base alloy NI-B46001 (NiCo20Si5B3) - Filler metal for brazing, amorphous foil; German version EN 3938:2001 |
|
DIN EN 3939 |
Aerospace series - Nickel base alloy NI-B46001 (NiCo20Si5B3) - Filler metal for brazing, powder or paste; German and English version EN 3939:2001 |
|
DIN EN 3940 |
Aerospace series - Nickel base alloy NI-B46001 (NiCo20Si5B3) - Filler metal for brazing - Tape; German version EN 3940:1998 |
|
DIN EN 3941 |
Aerospace series - Nickel base alloy NI-B41204 (NiCr13Si4B3) - Filler metal for brazing, amorphous foil; German version EN 3941:2001 |
|
DIN EN 3942 |
Aerospace series - Nickel base alloy NI-B41204 (NiCr13Si4B3) - Filler metal for brazing, borided foil; German version EN 3942:2001 |
|
DIN EN 3943 |
Aerospace series - Nickel base alloy NI-B41204 (NiCr13Fe4Si4B3) - Filler metal for brazing, powder or paste; German and English version EN 3943:2001 |
|
DIN EN 3944 |
Aerospace series - Nickel base alloy NI-B41204 (NiCr13Si4B3) - Filler metal for brazing - Tape; German version EN 3944:1998 |
|
DIN EN 3945 |
Aerospace series - Nickel base alloy NI-B48801 (NiMn19Si6Cu4B) - Filler metal for brazing, powder or paste; German and English version EN 3945:2001 |
|
DIN EN 3946 |
Aerospace series - Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing, powder or paste; German and English version EN 3946:2001 |
|
DIN EN 3947 |
Aerospace series - Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Rolled foil; German version EN 3947:1998 |
|
DIN EN 3948 |
Aerospace series - Nickel base alloy NI-B15701 (NiPd34Au30) - Filler metal for brazing - Wire; German version EN 3948:1998 |
|
DIN EN 3952 |
Aerospace series - Silver base alloy AG-B10001 (AgCu28) - Filler metal for brazing, wire; German version EN 3952:2001 |
|
DIN EN 3953 |
Aerospace series - Silver base alloy AG-B12401 (AgCu40Zn5Ni) - Filler metal for brazing, wire; German version EN 3953:2001 |
|
DIN EN 3955 |
Aerospace series - Silver base alloy AG-B12401 (AgCu40Zn5Ni) - Filler metal for brazing, rolled foil; German version EN 3955:2001 |
|
DIN EN 3956 |
Aerospace series - Silver base alloy AG-B14001 (AgCu42Ni2) - Filler metal for brazing, wire; German version EN 3956:2001 |
|
DIN EN 3958 |
Aerospace series - Silver base alloy AG-B14001 (AgCu42Ni2) - Filler metal for brazing, rolled foil; German version EN 3958:2001 |
|
DIN EN 3959 |
Aerospace series - Cobalt base alloy CO-B41601 (CoCr19Ni17Si8W4) - Filler metal for brazing, powder or paste; German version EN 3959:2001 |
|
DIN EN 3961 |
Aerospace series - Gold base alloy AU-B40001 - Filler metal for brazing, rolled foil; German version EN 3961:2001 |
|
DIN EN 3962 |
Aerospace series - Gold base alloy AU-B40001 - Filler metal for brazing, wire; German version EN 3962:2001 |
|
DIN EN 3963 |
Aerospace series - Copper CU-BU9001 - Filler metal for brazing, rolled foil; German version EN 3963:2001 |
|
DIN EN 3964 |
Aerospace series - Copper CU-BU9001 - Filler metal for brazing, wire; German version EN 3964:2001 |
|
DIN EN 3965 |
Aerospace series - Titanium alloy TI-B17001 - Filler metal for brazing, rolled foil; German version EN 3965:2001 |
|
DIN EN 3969 |
Aerospace series - Steel FE-PL1507 (40CrMoV12) - Air melted - Annealed - Forging stock - a or D = 350 mm; German and English version EN 3969:2006 |
|
DIN EN 3971 |
Aerospace series - Steel FE-PL1507 (40CrMoV12) - Consumable electrode remelted - Annealed - Forging stock - a or D = 350 mm; German and English version EN 3971:2006 |
|
DIN EN 3972 |
Aerospace series - Steel FE-PL1507 (40CrMoV12) - Consumable electrode remelted - Hardened and tempered - Bar for machining - D e = 50 mm - 1250 MPa = Rm = 1400 MPa; German and English version EN 3972:2006 |
|
DIN EN 3973 |
Aerospace series - Steel FE-CM3801 (X5CrNiCuNb16-4) - Homogenized, solution treated and precipitation hardened - Investment casting - De = 50 mm - Rm = 1030 MPa; German and English version EN 3973:2006 |
|
DIN EN 3974 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH8001 (NiCr20Ti) - Annealed; seamless drawn capillary tube 0,6 mm ≤ D ≤ 2,0 mm |
|
DIN EN 3976 |
Aerospace series - Titanium and titanium alloys - Test method - Chemical analysis for the determination of hydrogen content; German and English version EN 3976:2006 |
|
DIN EN 3979 |
Aerospace series - Aluminium alloy AL-P8090-O2 - Sheet for superplastic forming (SPF) - 0,8 mm ≤ a ≤ 6 mm; German and English version EN 3979:2005 |
|
DIN EN 3982 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7050-T7451 - Plate 6 mm < a ≤ 160 mm |
|
DIN EN 3983 |
(DRAFT) Aerospace series - Aluminium alloy AL-P7050-T7651 - Plate 6 mm < a ≤ 160 mm |
|
DIN EN 3989 |
(DRAFT) Aerospace series - Steel FE-PA2801 (X60NiMnCr13-5-3), cold worked and stress relieved - Bar for machining De ≤30 mm, Rm ≥ 850 MPa |
|
DIN EN 3991 |
(DRAFT) Aerospace series - Steel FE-PA2801 (X60NiMnCr13-5-3), non heat treated - Forging stock a or D ≤ 350 mm |
|
DIN EN 3992 |
(DRAFT) Aerospace series - Steel FE-PA2801 (X60NiMnCr13-5-3), softened - Forgings De ≤ 150 mm, 620 MPa ≤ Rm ≤ 900 MPa |
|
DIN EN 3993 |
(DRAFT) Aerospace series - Steel FE-CM1501 (X13CrNiMoCo12-3-2-2), hardened and tempered - Precision and sand castings De ≤ 150 mm, Rm ≥ 925 MPa |
|
DIN EN 3994 |
(DRAFT) Aerospace series - Steel FE-CM1501 (X13CrNiMoCo12-3-2-2), non heat treated - Remelting stock |
|
DIN EN 3996 |
(DRAFT) Aerospace series; aluminium alloy AL-P1100-H14; sheet and strip, 0,3 mm ≤ a ≤ 6 mm |
|
DIN EN 3997 |
(DRAFT) Aerospace series; aluminium alloy AL-P2024-T3; sheet and strip, 0,4 mm ≤ a ≤ 6 mm |
|
DIN EN 3997 |
Aerospace series - Aluminium alloy AL-P2024-T3 - Sheet and strip 0,4 mm = a = 6 mm; German and English version EN 3997:2007 |
|
DIN EN 3998 |
(DRAFT) Aerospace series; aluminium alloy AL-P2024-T42; sheet and strip, 0,4 mm ≤ a ≤ 6 mm |
|
DIN EN 3998 |
Aerospace series - Aluminium alloy AL-P2024-T4 or T42 - Sheet and strip 0,3 mm = a = 6 mm; German and English version EN 3998:2007 |
|
DIN EN 3999 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2024-T351 - Sheet and strip; chemical milling quality, 0,8 mm ≤ (kursiv)a ≤ 6 mm |
|
DIN EN 4000 |
Aerospace series - Metallic materials - Rules for the drafting and presentation of dimensional standards for metallic semi-finished products; German and English version EN 4000:2001 |
|
DIN EN 4001 |
(DRAFT) Aerospace series - Aluminium alloy AL-P2024-T351 - Clad sheet and strip; chemical milling quality 0,8 mm ≤ a ≤ 6 mm |
|
DIN EN 4001 |
Aerospace series - Aluminium alloy AL-P2024-T351 - Clad sheet and strip with improved chemical milling capability 1,6 mm = (kursiv)a = 6 mm; German and English version EN 4001:2007 |
|
DIN EN 4003 |
Aerospace series - Aluminium alloy AL-P2219-T87 - Sheet and strip 0,5 mm = a = 6 mm; German and English version EN 4003:2006 |
|
DIN EN 4004 |
(DRAFT) Aerospace series; aluminium alloy AL-P3103-H16; sheet and strip, 0,4 mm ≤ a ≤ 6 mm |
|
DIN EN 4004 |
Aerospace series - Aluminium alloy AL-P3103-H16 - Sheet and strip 0,4 mm = (kursiv)a = 6 mm; German and English version EN 4004:2007 |
|
DIN EN 4005 |
(DRAFT) Aerospace series; aluminium alloy AL-P5052-0; sheet and strip, 0,3 mm ≤ a ≤ 6 mm |
|
DIN EN 4005 |
Aerospace series - Aluminium alloy AL-P5052-O - Sheet and strip 0,3 mm = (kursiv)a = 6 mm; German and English version EN 4005:2007 |
|
DIN EN 4006 |
(DRAFT) Aerospace series; aluminium alloy AL-P6082-T4 or T42; sheet and strip, 0,4 mm ≤ a ≤ 6 mm |
|
DIN EN 4006 |
Aerospace series - Aluminium alloy AL-P6082-T4 or T42 - Sheet and strip 0,4 mm = a = 6 mm; German and English version EN 4006:2007 |
|
DIN EN 4007 |
Aerospace series - Aluminium alloy AL-P6082-T6 or T62 - Sheet and strip - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 4007:2005 |
|
DIN EN 4008-001 |
(DRAFT) Aerospace series - Elements of electrical and optical connection; crimping tools and associated accessories - Part 001: Technical specification |
|
DIN EN 4008-002 |
(DRAFT) Aerospace series - Elements of electrical and optical connection; crimping tools and associated accessories - Part 002: List of product standards |
|
DIN EN 4008-006 |
(DRAFT) Aerospace series - Elements of electrical and optical connection; crimping tools and associated accessories - Part 006: Positioner for crimping tool M22520/7; product standard |
|
DIN EN 4008-008 |
(DRAFT) Aerospace series - Elements of electrical and optical connection; crimping tools and associated accessories - Part 008: Positioner for crimping tool M22520/7-01; product standard |
|
DIN EN 4009 |
Aerospace series - Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-PH2601 (Inconel 718) - Classification: 1550 MPa (at ambient temperature)/650 °C; German and English version EN 4009:2004 |
|
DIN EN 4011 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1550 MPa (at ambient temperature)/600 °C; German and English version EN 4011:2004 |
|
DIN EN 4012 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1550 MPa (at ambient temperature)/425 °C; German and English version EN 4012:2004 |
|
DIN EN 4013 |
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1550 MPa (at ambient temperature)/600 °C; German and English version EN 4013:2004 |
|
DIN EN 4014 |
Aerospace series - Inserts, thickwall, self-locking - Design standard; German and English version EN 4014:2004 |
|
DIN EN 4015 |
Aerospace series - Inserts, thickwall, self-locking - Installation and removal procedure; German and English version EN 4015:2004 |
|
DIN EN 4016 |
(DRAFT) Aerospace series - Oversized bolts |
|
DIN EN 4017 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90°; German version EN 4017:2001 |
|
DIN EN 4018 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbow 90°, with thrust wire nut; German version EN 4018:2001 |
|
DIN EN 4021 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90°, bulkhead; German version EN 4021:2001 |
|
DIN EN 4022 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90°, bulkhead, welded end; German version EN 4022:2001 |
|
DIN EN 4023 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 45°; German version EN 4023:2001 |
|
DIN EN 4025 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 45°, bulkhead; German and English version EN 4025:2001 |
|
DIN EN 4026 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees; German version EN 4026:2001 |
|
DIN EN 4027 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, branch, with thrust wire nut; German version EN 4027:2001 |
|
DIN EN 4028 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees with thrust wire nut on run; German and English version EN 4028:2001 |
|
DIN EN 4029 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, bulkhead branch; German version EN 4029:2001 |
|
DIN EN 4030 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, bulkhead on run; German version EN 4030:2001 |
|
DIN EN 4031 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Nuts for welded ferrule; German version EN 4031:2001 |
|
DIN EN 4032 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Thrust wires; German and English version EN 4032:2001 + AC:2003 |
|
DIN EN 4033 |
(DRAFT) Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel - Diameter series 8 and 9, reduced internal radial clearance; Dimensions and loads |
|
DIN EN 4034 |
(DRAFT) Aerospace series - Bearings, airframe rolling - Double row self-aligning ball bearings with flanged outer ring in corrosion resisting steel, reduced internal radial clearance; Dimensions and loads |
|
DIN EN 4036 |
Aerospace series - Rod ends, adjustable with self-aligning double row ball bearing and threaded shank in corrosion resisting steel, reduced internal radial clearance - Dimensions and loads; German and English version EN 4036:2006 |
|
DIN EN 4037 |
(DRAFT) Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner, reduced starting torque - Light series - Dimensions and loads |
|
DIN EN 4038 |
(DRAFT) Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner, reduced starting torque - normal narrow series - Dimensions and loads |
|
DIN EN 4039 |
(DRAFT) Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner, reduced starting torque - normal wide series - Dimensions and loads |
|
DIN EN 4040 |
Aerospace series - Bearings, spherical plain in corrosion resisting steel with self-lubricating liner with wide inner ring - Elevated loads at ambient temperature - Dimensions and loads; German and English version EN 4040:2006 |
|
DIN EN 4041 |
Aerospace series - Bearings, airframe rolling - Rigid single row ball bearings in corrosion resisting steel, with extended inner ring and flanged alignment bush - Dimensions and loads; German and English version EN 4041:2006 |
|
DIN EN 4045 |
Aerospace series - Capillary tubes, seamless, in heat resisting alloys - Diameter 0,6 mm ≤ D ≤ 2 mm; Dimensions; German and English version EN 4045:2001 |
|
DIN EN 4047 |
Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated - Classification: 1 550 MPa (at ambient temperature)/600 °C - Technical specification; German and English version EN 4047:2004 |
|
DIN EN 4048 |
Aerospace series - Nuts, self-locking, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1550 MPa (at ambient temperature) / 425 °C - Technical specification; German and English version EN 4048:2004 |
|
DIN EN 4049-002 |
Aerospace series - Thermocouple extension cable - Operating temperatures between -65 °C to 260 °C - Part 002: General; German and English version EN 4049-002:2005 |
|
DIN EN 4050-2 |
(DRAFT) Aerospace series - Test method for metallic materials; ultrasonic inspection of bars, plates, forging stock and forgings - Part 2: Performance of test |
|
DIN EN 4050-3 |
(DRAFT) Aerospace series - Test method for metallic materials; ultrasonic inspection of bars, plates, forging stock and forgings - Part 3: Reference blocks |
|
DIN EN 4051 |
Aerospace series - Pipe couplings, 60°, spherical, in titanium alloy TI-P64001 - Port connection; German and English version EN 4051:2002 |
|
DIN EN 4054 |
Aerospace series - Pipe couplings, loose flanges and seals - Seals in fluorocarbon rubber and armature in aluminium alloy - Technical specification; German and English version EN 4054:2004 |
|
DIN EN 4057-100 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 100: General |
|
DIN EN 4057-201 |
Aerospace series - Cable ties for harnesses - Test methods - Part 201: Visual examination; German and English version EN 4057-201:2005 |
|
DIN EN 4057-202 |
Aerospace series - Cable ties for harnesses - Test methods - Part 202: Examination of mass and dimensions; German and English version EN 4057-202:2005 |
|
DIN EN 4057-302 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 302: Flammability |
|
DIN EN 4057-303 |
Aerospace series - Cable ties for harnesses - Test methods - Part 303: Resistance to fluids; German and English version EN 4057-303:2005 |
|
DIN EN 4057-304 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 304: Loop tensile strength at maximum working temperature |
|
DIN EN 4057-305 |
Aerospace series - Cable ties for harnesses - Test methods - Part 305: Colour fastness; German and English version EN 4057-305:2005 |
|
DIN EN 4057-306 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 306: Heat ageing test |
|
DIN EN 4057-307 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 307: Resistance to ultra violet radiation |
|
DIN EN 4057-401 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 401: Loop tensile strength |
|
DIN EN 4057-402 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 402: Life cycle |
|
DIN EN 4057-404 |
(DRAFT) Aerospace series - Cable ties for harnesses; Test methods - Part 404: Low temperature installation |
|
DIN EN 4058 |
Aerospace series - Filler rods and filler wires for welding in titanium and titanium alloys - Diameter 0,5 mm ≤ D ≤ 5,0 mm; Dimensions; German and English version EN 4058:2001 |
|
DIN EN 4059 |
Aerospace series - Filler rods and filler wires for welding in steel - Diameter 0,5 mm ≤ D ≤ 5,0 mm; Dimensions; German and English version EN 4059:2001 |
|
DIN EN 4060 |
Aerospace series - Filler rods and filler wires for welding in heat resisting alloys - Diameter 0,5 mm ≤ D ≤ 5,0 mm; Dimensions; German and English version EN 4060:2001 |
|
DIN EN 4061 |
(DRAFT) Aerospace series - Amorphous foil in filler metal for brazing; thickness 25 µm ≤ a ≤ 64 µm; dimensions |
|
DIN EN 4062 |
(DRAFT) Aerospace series - Rolled foil in filler metal for brazing; thickness a ≤ 1 mm; dimensions |
|
DIN EN 4064 |
(DRAFT) Aerospace series - Tape in filler metal for brazing; thickness 0,075 mm ≤ a ≤ 1,5 mm; dimensions |
|
DIN EN 4066 |
(DRAFT) Aerospace series - Borided foil in filler metal for brazing; thickness 25 µm ≤ a ≤ 100 µm; dimensions |
|
DIN EN 4067-001 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire resistant, operating temperature 260 °C peak - Part 001: Technical specification |
|
DIN EN 4067-002 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire resistant, operating temperature 260 °C peak - Part 002: Specification of performance and contact arrangements |
|
DIN EN 4067-003 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 003: Square flange receptacle; product standard |
|
DIN EN 4067-004 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 004: Jam-nut mounted receptacle; product standard |
|
DIN EN 4067-005 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 005: Hermetic square flange receptacle; product standard |
|
DIN EN 4067-006 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 006: Hermetic jam-nut mounted receptacle; product standard |
|
DIN EN 4067-007 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 007: Hermetic receptacle with round flange attached by soldering or brazing; product standard |
|
DIN EN 4067-008 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 008: Plug; product standard |
|
DIN EN 4067-009 |
(DRAFT) Aerospace series - Connectors, electrical, circular, scoop-proof, coupled by threaded ring, fire-resistant, operating temperature 260 °C peak - Part 009: Protective cover for plug; Product standard |
|
DIN EN 4068-001 |
(DRAFT) Aerospace series - Transformer rectifier units for aircraft - Part 001: Technical specification |
|
DIN EN 4069 |
Aerospace series - Nuts, hexagon, plain, reduced height, reduced across flats, in heat resisting steel, passivated - Classification: 600 MPa (at ambient temperature)/650 °C; German version EN 4069:1996 |
|
DIN EN 4071 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4072 |
(DRAFT) Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4073 |
(DRAFT) Aerospace series - Screws, pan head six lobe recess, coarse tolerance normal shank medium length thread, in alloy steel, cadmium plated - Classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4074 |
(DRAFT) Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4075 |
(DRAFT) Aerospace series - Screws, pan head, offset cruciform recess, threaded to head, in corrosion resisting steel, passivated - Classification: 490 MPa (at ambient temperature)/425 °C |
|
DIN EN 4076 |
(DRAFT) Aerospace series - Screws, pan head, slotted, threaded to head, in corrosion resisting steel, passivated - Classification: 490 MPa (at ambient temperature)/425 °C |
|
DIN EN 4077 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, threaded to head, in heat and corrosion resisting steel, passivated - Classification: 900 MPa (at ambient temperature)/650 °C |
|
DIN EN 4079 |
(DRAFT) Aerospace series - Screws, 100° countersunk normal head, offset cruciform recess, threaded to head, in alloy steel, cadmium plated; classification: 900 MPa (at ambient temperature)/235 °C |
|
DIN EN 4080 |
(DRAFT) Aerospace series - Screws, pan head, offset cruciform recess, threaded to head, in alloy steel, cadmium plated - Classification: 900 MPa (at ambient temperature)/235 °C |
|
DIN EN 4082 |
(DRAFT) Aerospace series - Screws, pan head, slotted, threaded to head, in corrosion resisting steel, passivated - Classification: 900 MPa (at ambient temperature)/650 °C |
|
DIN EN 4083 |
(DRAFT) Aerospace series - Nuts, bihexagonal, self-locking, reduced height, with counterbore, in heat resisting steel, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4084 |
(DRAFT) Aerospace series; nuts, anchor, self-locking; fixed, two lug, with counterbore; in alloy steel, cadmium plated, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4085 |
Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing; Amorphous foil; German version EN 4085:2001 |
|
DIN EN 4086 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PD2101 (NiCo14Nb5Ti2), non heat treated - Forging stock a or D ≤ 360 mm |
|
DIN EN 4087 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PD2101 (NiCo14Nb5Ti2) - Solution treated and precipitation treated, forgings, De ≤ 75 mm Rm ≥ 1210 MPa |
|
DIN EN 4088 |
(DRAFT) Aerospace series - Steel FE-PL1501 (13MoCrNiV4-4-3-1), vacuum induction melted and vacuum arc remelted, carburized, hardened, sub-zero treated and tempered - Bar for machining De ≤ 30 mm, 1315 MPa ≤ Rm ≤ 1650 MPa |
|
DIN EN 4089 |
(DRAFT) Aerospace series - Steel FE-PL5101 (13MoCrNiV4-4-3-1), vacuum induction melted and vacuum arc remelted, softened - Forging stock a or D ≤ 150 mm |
|
DIN EN 4090 |
(DRAFT) Aerospace series - Steel FE-PL5101 (13MoCrNiV4-4-3-1), vacuum induction melted and vacuum arc remelted, carburized, hardened, sub-zero treated and tempered - Forgings, De ≤ 30 mm, 1315 MPa ≤ Rm ≤ 1650 MPa |
|
DIN EN 4092 |
(DRAFT) Aerospace series - Heat resisting alloy NI- PH3901 (NiCr25Mo10) - Air melted and vacuum refined, annealed; sheet and strip; 0,25 mm ≤ a ≤ 3 mm |
|
DIN EN 4093 |
(DRAFT) Aerospace series - Heat resisting alloy NI- PH3901 (NiCr25Mo10) - Air melted and vacuum refined, annealed; sheet, strip and plate; a > 3 mm |
|
DIN EN 4094 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CH1305 (NiCr16Co10Mo8Al4Ti4) vacuum melted, non heat treated - Remelting stock |
|
DIN EN 4095 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CH1305 (NiCr16Co10Mo8Al4Ti4) vacuum melted, non heat treated - Precision castings |
|
DIN EN 4096 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CD1401 (NiCo10W10Cr9Al6Ta3) vacuum melted, non heat treated - Remelting stock |
|
DIN EN 4097 |
(DRAFT) Aerospace series - Heat resisting alloy NI-CD1401 (NiCo10W10Cr9Al6Ta3) vacuum melted, precipitation treated - Precision castings |
|
DIN EN 4098 |
(DRAFT) Aerospace series - Steel FE-PL1507 (40CrMoV12)- Remelted; hardened and tempered; forgings De = 50 mm, 1250 MPa = Rm = 1400 MPa |
|
DIN EN 4099 |
Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Clad sheet and strip - 0,5 mm ≤ a ≤ 6 mm; German and English version EN 4099:2005 |
|
DIN EN 4100 |
Aerospace series - Aluminium alloy AL-P2219-T6 or T62 - Sheet and strip - 0,5 mm ≤ a ≤ 6 mm; German and English version EN 4100:2005 |
|
DIN EN 4101 |
Aerospace series - Aluminium alloy AL-P2024-T4 - Sheet and strip with improved stretch forming capability - 0,4 mm ≤ a ≤ 6 mm; German and English version EN 4101:2005 |
|
DIN EN 4102 |
Aerospace series - Aluminium alloy AL-P2219-T81 - Clad sheet and strip - 0,5 mm ≤ a ≤ 6 mm; German and English version EN 4102:2005 |
|
DIN EN 4103 |
Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing, Borided foil; German and English version EN 4103:2001 |
|
DIN EN 4104 |
Aerospace series - Nickel base alloy NI-B40002 - Filler metal for brazing; Powder or paste; German and English version EN 4102:2001 |
|
DIN EN 4105 |
Aerospace series - Nickel base alloy NI-B40002 (NiSi4B2) - Filler metal for brazing - Tape; German version EN 4105:1998 |
|
DIN EN 4108 |
(DRAFT) Aerospace series - Wrenches, crow foot, attachment socket, socket drive |
|
DIN EN 4110 |
(DRAFT) Aerospace series - Wrenches, open end, box |
|
DIN EN 4111 |
Aerospace series - Wrenches, splined, socket for pipe fittings - Technical specification; German and English version EN 4111:2006 |
|
DIN EN 4112 |
(DRAFT) Aerospace series - Pins, parallel, in corrosion resisting steel, passivated |
|
DIN EN 4113 |
Aerospace series - Clamps, loop ( |
|
DIN EN 4114 |
Aerospace series - Clamps, loop ( |
|
DIN EN 4115 |
Aerospace series - Cushion, rubber, for clamps - Dimensions, masses; German and English version EN 4115:2001 |
|
DIN EN 4116 |
Aerospace series - Nuts, hexagonal, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1100 MPa (at ambient temperature) / 425 °C; German and English version EN 4116:2004 |
|
DIN EN 4117 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread - Classification: 1550 MPa (at ambient temperature) / 600 °C; German and English version EN 4117:2004 |
|
DIN EN 4118 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1100 MPa (at ambient temperature) / 650 °C; German and English version EN 4118:2004 |
|
DIN EN 4119 |
Aerospace series - Nuts, bihexagonal, self-locking, deep counterbore, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1100 MPa (at ambient temperature) / 650 °C; German and English version EN 4119:2004 |
|
DIN EN 4120 |
Aerospace series - Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread - Classification: 1210 MPa (at ambient temperature)/730 °C; German and English version EN 4120:2004 |
|
DIN EN 4121 |
Aerospace series - Shank nuts, serrated, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1100 MPa (at ambient temperature)/650 °C; German and English version EN 4121:2004 |
|
DIN EN 4122 |
Aerospace series - Shank nuts, self-locking, in heat resisting steel FE-PA2601 (A286), silver plated on thread - Classification: 1100 MPa (at ambient temperature)/650 °C; German and English version EN 4122:2004 |
|
DIN EN 4124 |
Aerospace series - Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH1302 (Waspaloy), silver plated on thread, for 60° swage - Classification: 1210 MPa (at ambient temperature) / 730 °C; German and English version EN 4124:2004 |
|
DIN EN 4125 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, fixed, two lug, reduced series, with incremental counterbore, in heat resisting steel, MoS2 lubricated; classification: 900 MPa (at ambient temperature)/315 °C |
|
DIN EN 4126 |
(DRAFT) Aerospace series; nuts, anchor, self-locking, floating, two lug, reduced series, with incremental counterbore, in heat resisting steel, MoS2 lubricated; classification: 900 MPa (at ambient temperature)/315 °C |
|
DIN EN 4127 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4128 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, short thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1250 MPa (at ambient temperature)/425 °C |
|
DIN EN 4129 |
(DRAFT) Aerospace series; bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4130 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4131 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, medium length thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1250 MPa (at ambient temperature)/425 °C |
|
DIN EN 4132 |
(DRAFT) Aerospace series; bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4133 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in titanium alloy, aluminium IVD coated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4134 |
(DRAFT) Aerospace series - Bolts, normal hexagonal head, coarse tolerance normal shank, long thread, in heat resisting nickel base alloy, aluminium IVD coated - Classification: 1250 MPa (at ambient temperature)/425 °C |
|
DIN EN 4135 |
(DRAFT) Aerospace series; bolts, normal bi-hexagonal head, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4136 |
(DRAFT) Aerospace series; bolts, normal bi-hexagonal head, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4137 |
(DRAFT) Aerospace series; bolts, normal bi-hexagonal head, stepped shank, long thread, in titanium alloy, anodized, MoS2 lubricated; classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4138 |
(DRAFT) Aerospace series; screws, pan head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4139 |
(DRAFT) Aerospace series; screws, pan head, offset cruciform recess, threaded to head, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4153 |
(DRAFT) Aerospace series - Rivets, solid, universal head, in aluminium alloy 2218, anodized or chromated - Metric series |
|
DIN EN 4154 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head, in aluminium alloy 2119, anodized or chromated - Metric series |
|
DIN EN 4155 |
(DRAFT) Aerospace series - Rivets, solid, 100° countersunk normal head with dome, in aluminium alloy 2119, anodized or chromated - Metric series |
|
DIN EN 4156 |
(DRAFT) Aerospace series - Rod ends with self-aligning double row ball bearings and threaded shank in steel - Inner ring and balls in corrosion resisting steel; Dimensions and loads; Inch series |
|
DIN EN 4157 |
(DRAFT) Aerospace series - Rod ends with self-aligning double row ball bearings and threaded shank in steel - Dimensions and loads; Inch series |
|
DIN EN 4158 |
Aerospace series - Paints and varnishes - Test method for measurement of electrical surface resistance of conductive layers; German and English version EN 4158:2006 |
|
DIN EN 4161 |
(DRAFT) Aerospace series; screws, pan head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4162 |
(DRAFT) Aerospace series; screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, medium length thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4163 |
(DRAFT) Aerospace series; screws 100° countersunk normal head, offset cruciform recess, coarse tolerance normal shank, long thread, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4164 |
(DRAFT) Aerospace series; screws 100° countersunk normal head, offset cruciform recess, threaded to head, in alloy steel, cadmium plated; classification: 1100 MPa (at ambient temperature)/235 °C |
|
DIN EN 4166 |
Aerospace series - Clips, spring tension, three parts - PTFE bushes; German and English version EN 4166:2004 |
|
DIN EN 4167 |
Aerospace series - Clips, spring tension, three parts - Inner clips in heat resisting steel FE-PA2601 (A286); German and English version EN 4167:2004 |
|
DIN EN 4172 |
Aerospace series - Lockbolts, protruding head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series - Classification: 1100 MPa (at ambient temperature)/315 °C; German and English version EN 4172:2006 |
|
DIN EN 4173 |
Aerospace series - Lockbolts, 100° countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series - Classification: 1100 MPa (at ambient temperature)/315 °C; German and English version EN 4173:2006 |
|
DIN EN 4174 |
Aerospace series - Collars, swage locking, sheartype, in aluminium alloy 2024, anodized or chromated, metric series; German and English version EN 4174:2006 |
|
DIN EN 4175 |
Aerospace series - Collars, flanged swage locking, sheartype, in titanium TI-P99002, metric series; German and English version EN 4175:2005 |
|
DIN EN 4176 |
(DRAFT) Aerospace series - Lockbolts, 100° countersunk normal head or protruding head, tension-/sheartype, close tolerance, in titanium alloy TI-P64001, anodized or with aluminium pigmented coating collars in titanium TI-P99002 or aluminium alloy 2024, metric series; technical specification |
|
DIN EN 4176 |
Aerospace series - Lockbolts, 100° countersunk normal head or protruding head, tension-/sheartype, close tolerance, in titanium alloy TI-P64001, anodized or with aluminium pigmented coating - Collars in titanium TI-P99002 or aluminium alloy 2024 - Metric series - Technical specification; German and English version EN 4176:2005 |
|
DIN EN 4178 |
(DRAFT) Aerospace series - Screws, pan head, six lobe recess, coarse tolerance normal shank, medium length thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1100 MPa (at ambient temperature)/315 °C |
|
DIN EN 4179 |
Aerospace series - Qualification and approval of personnel for non-destructive testing; German version EN 4179:2000 |
|
DIN EN 4180 |
Aerospace series - Circular tubes, for fluids in titanium and titanium alloys - Wide tolerances; Diameter 4 mm ≤ D ≤ 40 mm; Dimensions; German and English version EN 4180:2001 |
|
DIN EN 4182 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, reduced; German version EN 4182:2001 |
|
DIN EN 4183 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90°, welded ends; German version EN 4183:2001 |
|
DIN EN 4184 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 45°, welded ends; German version EN 4184:2001 |
|
DIN EN 4186 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, cross; German version EN 4186:2001 |
|
DIN EN 4187 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90° bulkhead, long; German and English version EN 4187:2001 |
|
DIN EN 4188 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Elbows 90° bulkhead, long, welded end; German and English version EN 4188:2001 |
|
DIN EN 4189 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, bulkhead branch, long; German version EN 4189:2001 |
|
DIN EN 4190 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, reduced, with thrust nut on run; German version EN 4190:2001 |
|
DIN EN 4191 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, reduced, bulkhead branch, long; German version EN 4191:2001 |
|
DIN EN 4192 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, reduced, bulkhead branch; German version EN 4192:2001 |
|
DIN EN 4193 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, reduced, bulkhead on long run; German version EN 4193:2001 |
|
DIN EN 4194 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Tees, reduced, bulkhead; German version EN 4194:2001 |
|
DIN EN 4198 |
Aerospace series - Rod-ends, adjustable self-aligning plain bearing with self-lubricating liner and threaded shank in corrosion resisting steel - Dimensions and loads; German and English version EN 4198:2006 |
|
DIN EN 4199-002 |
Aerospace series - Bonding straps for aircraft - Part 002: Index of product standard; German and English version EN 4199-002:2006 |
|
DIN EN 4199-006 |
Aerospace series - Bonding straps for aircraft - Part 006: Round braid copper conductors for bonding straps, tin plated up to 150 °C or nickel plated up to 260 °C - Product standard; German and English version EN 4199-006:2006 |
|
DIN EN 4201 |
(DRAFT) Aerospace series - Washers, 100° dimpled, in titanium |
|
DIN EN 4202 |
Aerospace series - Aluminium alloy AL-P6082-T651 - Plate - 6 mm < a ≤ 25 mm; German and English version EN 4202:2005 |
|
DIN EN 4203 |
Aerospace series - Aluminium alloy AL-P8090-T89 - Sheet - 0,6 mm ≤ a ≤ 6 mm; German and English version EN 4203:2005 |
|
DIN EN 4204 |
Aerospace series - Aluminium alloy AL-P8090-T841 - Sheet - 0,6 mm ≤ a ≤ 6 mm; German and English version EN 4204:2005 |
|
DIN EN 4207 |
(DRAFT) Aerospace series - Aluminium alloy AL-P8090-T89 - Extruded bar and section a oder D ≤ 15 mm, with peripheral coarse grain control |
|
DIN EN 4209 |
Aerospace series - Aluminium alloy AL-P2219-T851 - Plate - 6 mm < a ≤ 50 mm; German and English version EN 4209:2005 |
|
DIN EN 4212 |
Aerospace series - Aluminium alloy AL-P5086-H111 - Plate - 6 mm < a ≤ 80 mm; German and English version EN 4212:2005 |
|
DIN EN 4213 |
Aerospace series - Aluminium alloy AL-P6061-T651 - Plate - 6 mm < a ≤ 80 mm; German and English version EN 4213:2005 |
|
DIN EN 4214 |
Aerospace series - Aluminium alloy AL-P7010-T651 - Plate - 6 mm < a ≤ 20 mm; German and English version EN 4214:2005 |
|
DIN EN 4215 |
Aerospace series - Aluminium alloy AL-P7175-T651 - Plate - 6 mm < a ≤ 80 mm; German and English version EN 4215:2005 |
|
DIN EN 4216 |
(DRAFT) Aerospace series - Steel FE-CM3801 (GX5CrNiCuNb16-4) homogenized, solution treated and precipitation hardened - Investment casting De ≤ 50 mm, Rm ≥ 900 MPa |
|
DIN EN 4219 |
(DRAFT) Aerospace series - Nuts, hexagon, self-locking by domed plastic cap, normal height, normal across flats, in corrosion resisting steel, passivated; classification: 900 MPa (at ambient temperature)/120 °C |
|
DIN EN 4222 |
(DRAFT) Aerospace series - Heat resisting alloy NI-PH1305 (NiCr22Co13Mo9Al1) - Air melted and vacuum refined, annealed; sheet and strip; 0,25 mm ≤ a ≤ 3 mm |
|
DIN EN 4233 |
Aerospace series - Pipe coupling 8°30′ in titanium alloy - Unions, welded, threaded; German version EN 4233:2001 |
|
DIN EN 4234 |
Aerospace series - Clamps, worm drive - Dimensions, masses; German and English version EN 4234:2006 |
|
DIN EN 4235-2 |
(DRAFT) Aerospace series; steel; wrought products; technical specification; part 2: plate, sheet and strip |
|
DIN EN 4238 |
(DRAFT) Aerospace series - Fibre reinforced plastics - Determination of the effect of dry heat on physical and mechanical characteristics |
|
DIN EN 4243 |
(DRAFT) Aerospace series - Cast acrylic sheets - Technical specification |
|
DIN EN 4244 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted, hardened and tempered, bar a or D, ≤ 200 mm, 1000 MPa ≤ Rm ≤ 1140 MPa |
|
DIN EN 4245 |
(DRAFT) Aerospace series - Heat resisting alloy FE-PM1708 - Vacuum arc remelted, as forged, forging stock De ≤ 300 mm |
|
DIN EN 4246 |
(DRAFT) Aerospace series - Heat resisting alloy CO-PH4101 - Vacuum melted, as forged, forging stock De ≤ 360 mm |
|
DIN EN 4247 |
Aerospace series - Aluminium alloy AL-P2024-T42 - Plate - 6 mm < a ≤ 140 mm; German and English version EN 4247:2005 |
|
DIN EN 4248 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, single lug, with counterbore in heat resisting steel, silver plated; classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4249 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, single lug, reduced series, with counterbore in heat resisting steel, silver plated; classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4250 |
Aerospace series - Nickel base alloy NI-B41001 (NiSr19Si7B) - Filler metal for brazing, amorphous foil; German version EN 4250:2001 |
|
DIN EN 4251 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, 90° corner, with counterbore, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4252 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4253 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, closed corner, reduced series, with counterbore, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4254 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, 60° corner with counterbore, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4255 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, two lug, with counterbore, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4256 |
(DRAFT) Aerospace series - Nuts, anchor, self-locking, fixed, two lug, reduced series, with counterbore, in heat resisting steel, silver plated - Classification: 1100 MPa (at ambient temperature)/425 °C |
|
DIN EN 4258 |
Aerospace series - Metallic materials - General organization of standardization; links between types of EN standards and their use; German version EN 4258:1998 |
|
DIN EN 4259 |
(DRAFT) Aerospace series - Metallic materials - Definition of general terms |
|
DIN EN 4260 |
(DRAFT) Aerospace series - Metallic materials - Rules for drafting and presentation of technical specifications |