49.030 : Fasteners for aerospace construction

49.030.01

Fasteners in general

49.030.10

Screw threads

49.030.20

Bolts, screws, studs

49.030.30

Nuts

49.030.40

Pins, nails

49.030.50

Washers and other locking elements

49.030.60

Rivets

49.030.99

Other fasteners
BS EN 4123:2003

BS EN 4123:2003

Superseded Historical

Aerospace series. Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH2601 (Inconel 718), silver plated on thread. Classification: 1550 MPa (at ambient temperature)/600°C

€165.00

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BS EN 3907:2003

BS EN 3907:2003

Superseded Historical

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

€165.00

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BS EN 4124:2003

BS EN 4124:2003

Superseded Historical

Aerospace series. Shank nuts, self-locking, in heat resisting nickel base alloy NI-PH-1302 (Waspaloy), silver plated on thread, for 60 swage. Classification: 1210 MPa (at ambient temperature)/730°C

€165.00

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BS EN 4323:2003

BS EN 4323:2003

Superseded Historical

Aerospace series. Screws, 100° countersunk head, six lobe recess, threaded to head, in titanium alloy TI-P64001, anodized, MoS2 coated. Classification: 900 MPa (at ambient temperature)/350°C

€165.00

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BS EN 4322:2003

BS EN 4322:2003

Superseded Historical

Aerospace series. Bolts, double hexagon head with lockwire holes, relieved shank, long thread, in titanium alloy TI-P64001, anodized, MoS2 coated. Strength class: 1100 MPa (at ambient temperature)

€165.00

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DIN EN 4114:2003-03

DIN EN 4114:2003-03

Superseded Historical

Aerospace series - Clamps, loop ("P" type) in aluminium alloy with rubber cushioning - Dimensions, masses; German and English version EN 4114:2001

€105.42

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DIN EN 4113:2003-03

DIN EN 4113:2003-03

Superseded Historical

Aerospace series - Clamps, loop ("P" type) in corrosion resisting steel, passivated, with rubber cushioning - Dimensions, masses; German and English version EN 4113:2001

€105.42

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BS EN 3831:2003

BS EN 3831:2003

Superseded Historical

Aerospace series. Inserts, thickwall, self-locking, in heat resisting steel FE-PM3801 (17-4PH), MoS2 coated

€165.00

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BS EN 3832:2003

BS EN 3832:2003

Superseded Historical

Aerospace series. Bolts, double hexagon head, relieved shank, long thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification: 1550 MPa (at ambient temperature) / 650°C

€165.00

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BS EN 3833:2003

BS EN 3833:2003

Superseded Historical

Aerospace series. Bolts, MJ threads, in heat resisting nickel base alloy NI-PH2601 (Inconel 718). Classification: 1550 MPa (at ambient temperature) / 650°C. Technical specifications

€269.00

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BS EN 3899:2003

BS EN 3899:2003

Superseded Historical

Aerospace series. Inserts, thickwall, self-locking, MJ threads, in heat resisting steel FE-PM3801 (17-4PH). Technical specification

€193.00

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BS EN 4009:2003

BS EN 4009:2003

Superseded Historical

Aerospace series. Bolts, double hexagon head, close tolerance shank, medium length thread, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Classification: 1550 MPa (at ambient temperature)/650 °C

€165.00

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BS EN 3752:2003

BS EN 3752:2003

Superseded Historical

Aerospace series. Nuts, self-locking, MJ threads, in heat resisting steel FE-PA92HT (A286), MoS2 coated. Classification: 1100 MPa (at ambient temperature) / 425°C. Technical specification

€193.00

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BS EN 4012:2003

BS EN 4012:2003

Superseded Historical

Aerospace series. Nuts, bihexagonal, self-locking, in heat resisting nickel base alloy NI-P100HT (Inconel 718), MoS2 coated. Classification: 1500 MPa (at ambient temperature)/425°C

€165.00

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BS EN 4014:2003

BS EN 4014:2003

Superseded Historical

Aerospace series. Inserts, thickwall, self-locking. Design standard

€165.00

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