Inserts, thin wall, self-locking, MJ threads, in heat resisting nickel base alloy NI-P100HT (Inconel 718). Technical specification
€193.00
Inserts, thin wall, self-locking, short, in heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plated internal thread
€165.00
Installation holes for inserts, screw thread, helical coil, self-locking. Design standard
Inserts, screw thread, helical coil, self-locking. Technical specification
Inserts, thin wall, self-locking. Installation and removal procedure
Inserts, screw thread, helical coil, self-locking, in corrosion resisting steel FE-PA3004
Inserts, screw thread, helical coil, self-locking, in heat resisting nickel base alloy NI-PH2801 (Inconel X750)
Nuts, hexagonal, self-locking, ball seat, in alloy steel, cadmium plated, MoS2 lubricated. Classification: 900 MPa (at ambient temperature)/235°C
€95.00
Aerospace series — Fasteners, externally threaded, in heat resisting steel FE-PA92HT (A286) — Classification: 900 MPa/650 °C, manufacturing method optional — Technical specification
€269.00
Aerospace series — Nut, anchor, self-locking, fixed, 90° corner, reduced series, with counterbore, in heat resisting steel, MoS2 lubricated — Classification: 1 100 MPa (at ambient temperature) / 315 °C
BS EN 3240 Aerospace series — Nut, self-locking, clip, in heat resisting steel FE-PA2601 (A286), uncoated — Classification: 1 100 MPa (at ambient temperature) / 425 °C
€23.00
BS EN 3241 Aerospace series — Nut, self-locking, clip, in heat resisting steel FE-PA 92 HT (A 286), silver coated — Classification: 1 100 MPa (at ambient temperature) / 425 °C
BS EN 3004 Aerospace series - Nuts, self-locking, MJ threads, in heat resisting steel FE-PA2601 (A286), classification: 1 100 MPa (at ambient temperature)/650 °C - Technical specification
BS EN 4048 Aerospace series - Nuts, self-locking, MJ threads, in heat-resisting nickel base alloy NI-PH2601 (Inconel 718), MoS2 coated - Classification: 1 550 MPa (at ambient temperature)/425 °C - Technical specification
Aerospace series. Pipe coupling 8°30' in titanium alloy. Thrust wire nut
