Aerospace series. Specification for aluminium alloy nuts (Unified hexagons and Unified threads) (ordinary and slotted) for aircraft
€165.00
Aerospace series. Nuts, self-locking, clip, in heat resisting steel FE-P A 92 HT (A 286), silver coated. Classification: 1100 MPa (at ambient temperature) / 425 °C
Aerospace series. Shaft-nuts, self-locking, left-hand thread, in heat resisting steel FE-PA92HT (A286), silver plated
Aerospace series. Insert, 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
Aerospace series. Shank nuts, self-locking, flange restrained. Installation procedure
Specification for general requirements for bolts and free running nuts of tensile strength not exceeding 1249 MPa
€269.00
Aerospace series. Inserts, UNJ threads, self-locking, with self-broaching keys Installation and removal procedure
€193.00
Aerospace series. Inserts, UNJ threads, self-locking, with self-broaching keys Design standard
Aerospace series. Inserts, UNJ threads, self-locking, with self-broaching keys In heat resisting nickel base alloy NI-P100HT (Inconel 718), silver plating
Aerospace series. Inserts, UNJ threads, self-locking, with self-broaching keys In heat resisting nickel base alloy NI-P101HT (WASPALOY), silver plating
Aerospace series. Inserts, UNJ threads, self-locking, with self-broaching keys In heat resisting steel FE-PA2601 (A286), MoS2 coated
Aerospace series. Inserts, UNJ threads, self-locking, with self-broaching keys Technical specification
Nuts, barrel, self-locking, floating, with MJ threads, classifications. 900 MPa (at ambient temperature)/235°C, 1100 MPa (at ambient temperature)/235°C, 1250 MPa (at ambient temperature)/235°C, 1550 MPa (at ambient temperature)/235°C. Dimensions
Nuts, self-locking, with maximum operating temperature less than or equal to 425°C. Test methods
Aerospace. Nuts, metric. Tolerances of form and position
