49.030.60 - Rivets

This document specifies the dimensions, tolerances and mass of rivets with 100° medium flush head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and masses of rivets with 100° normal flush head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with universal head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with 100° reduced flush head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and masses of rivets with 100° normal flush head, close tolerance, inch series, for aerospace applications.

This document specifies the dimensions, tolerances and mass of rivets with 100° medium flush head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with universal head, close tolerance, inch series, for aerospace application.

This document specifies the dimensions, tolerances and mass of rivets with 100° reduced flush head, close tolerance, inch series, for aerospace applications.

This document defines the requirements for qualification, acceptance, delivery and inspection of 100° countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear type in aluminium alloy 7050T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061T7 for use as permanent fasteners in aerospace applications.

This document defines the requirements for qualification, acceptance, delivery and inspection of 100° countersunk head, 100° countersunk reduced head and protruding head close tolerance pins, shear type in aluminium alloy 7050-T73 and collars of aluminium alloy 3003 and of aluminium alloy 6061-T7 for use as permanent fasteners in aerospace applications.

This document specifies the requirements relating to:
Steel FE-PA11
Softened and cold drawn
Wires for rivets
1 mm ≤ D ≤ 10 mm
for aerospace applications.

This standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with protruding head, for aerospace application.

TC - mistake in drawing

TC - mistake in drawing

This standard specifies the configuration, dimension, tolerances and mass of a stainless steel blind bolt with protruding head, for aerospace application.

ISO 12289:2016 specifies the characteristics and quality assurance requirements for solid rivets made in corrosion-resisting steel for aerospace construction. It is applicable whenever it is referenced in a definition document.

This European Standard specifies the requirements for ultrasonic inspection of tubes in metallic materials with an external diameter  5 mm.
For other cases, the use of this standard is by agreement between the manufacturer and the purchaser.
The purpose of the ultrasonic inspection is the detection of defects within the wall thickness and at the outer and inner surfaces of the tube. The method will detect two dimensional defects in the longitudinal and circumferential directions perpendicular to the tube wall. Where inspection for other types of defects is required, this requirements shall be stated on the order.

This European Standard defines the characteristics of solid rivets, with universal head, metric series, in nickel base alloy, for maximum operating temperature 650 °C.

This European Standard defines the characteristics of solid rivets, with universal head, metric series, in nickel base alloy, for maximum operating temperature 650 °C.

This standard specifies the requirements for shear testing rivet wire and rivets in metallic materials for aerospace applications.
It shall be applied when referred to in the EN technical specification or material standard unless otherwise specified on the drawing, order or inspection schedule.

This standard specifies the performance and test requirements for corrosion and heat resisting solid steel rivets intended for aerospace applications. It applies whenever it is specified in the document defining the rivet.
Its use, after agreement between the customer and the supplier, for solid rivets made from other materials, requires determination, case by case, of the minimum tensile and double shear loads.

This standard specifies the performance and test requirements for solid rivets in the nickel alloys quoted below, intended for aerospace applications. It applies wherever it is specified in the document defining the rivet.
Its use, after agreement between the customer and the supplier, for solid rivets made from other materials, requires determination, case by case, of the minimum tensile and double shear loads.

This standard specifies the performance and test requirements for solid rivets in the nickel alloys quoted below, intended for aerospace applications. It applies wherever it is specified in the document defining the rivet.
Its use, after agreement between the customer and the supplier, for solid rivets made from other materials, requires determination, case by case, of the minimum tensile and double shear loads.

This standard specifies the performance and test requirements for corrosion and heat resisting solid steel rivets intended for aerospace applications. It applies whenever it is specified in the document defining the rivet.
Its use, after agreement between the customer and the supplier, for solid rivets made from other materials, requires determination, case by case, of the minimum tensile and double shear loads.

This standard specifies the characteristics of lockbolts with protruding head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series, for use in aerospace applications.
Classification : 1 100 MPa  / 315 °C
In both versions, i.e. with and without pintail these lockbolts fulfill the same function when installed and are statically / dynamically equivalent.
They are intended to be used with collars to EN 4174 or EN 4175.

This standard specifies the characteristics of lockbolts with 100° countersunk normal head, sheartype, close tolerance, in titanium alloy TI-P64001, anodized, metric series, for use in aerospace applications.
Classification : 1 100 MPa / 315 °C
In both versions, i.e. with and without pintail these lockbolts fulfill the same function when installed and are statically / dynamically equivalent.
They are intended to be used with collars to EN 4174 or EN 4175.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head with dome, in corrosion resisting steel FE-PA2601, passivated, inch based series, for maximum operating temperature 750 °C.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head, in corrosion resisting steel FE-PA2601, passivated, inch based series, for maximum operating temperature 750 °C.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head, in corrosion resisting steel FE-PA11, passivated, inch based series, for maximum operating temperature 700 °C.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head, in corrosion resisting steel FE-PA2601, passivated, inch based series, for maximum operating temperature 750 °C.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head with dome, in corrosion resisting steel FE-PA2601, passivated, inch based series, for maximum operating temperature 750 °C.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head, in corrosion resisting steel FE-PA11, passivated, inch based series, for maximum operating temperature 700 °C.

This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium alloy, anodized or chromated, for maximum operating temperature 120°C.

This standard specifies the characteristics of solid rivets, universal head, in titanium TI-PO2, anodized, inch based series, for maximum operating temperature 315°C.

This standard specifies the characteristics of solid rivets, with universal head, in heat resisting nickel base alloy NI-P11, inch based series, for maximum operating temperature 650 °C.

This standard specifies the characteristics of solid rivets, with 100° normal countersunk head, inch based series, in aluminium alloy, anodized or chromated, for maximum operating temperature 120 °C

This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium, for maximum operating temperature 120 °C.

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head, in titanium TI-PO2, anodized, inch based series, for maximum operating temperature 315°C.

This standard specifies the characteristics of solid rivets, with 100° normal countersunk head with dome, inch based series, in aluminium alloy, anodized or chromated, for maximum operating temperature 120 °C

This standard specifies the characteristics of solid rivets, universal head, in corrosion resisting steel FE-PA11, passivated, inch based series, for maximum operating temperature 700 °C.

This standard specifies the characteristics of solid rivets, with 100° normal countersunk head with dome, inch based series, in aluminium alloy, for maximum operating temperature 120 °C

This standard specifies the characteristics of solid rivets, with 100° countersunk normal head with dome, in titanium TI-PO2, anodized, inch based series, for maximum operating temperature 315°C.

This standard specifies hole sizes for solid rivets set by cold forming and is applicable to all materials.
It is applicable to all solid rivets in the EN series.
The purpose of the standard is to reduce the variety of drills and plug gauges used for the production of rivet holes and to ensure consistency in the performance of rivetted joints used in aerospace applications.

This standard specifies the characteristics of solid rivets, universal head, in aluminium alloy 5056A, anodized or chromated, inch based series, for maximum operating temperature 120 °C.

This standard specifies the representation of rivets on drawings for aerospace equipment.

This standard specifies the characteristics of solid rivets, with 100° normal countersunk head with dome, inch based series, in aluminium alloy, for maximum operating temperature 120 °C

This standard specifies the characteristics of solid rivets, with universal head, in heat resisting nickel base alloy NI-P11, cadmium plated, inch based series, for maximum operating temperature 235 °C.

This standard specifies the characteristics of solid rivets, universal head, in corrosion resisting steel FE-PA92HT, passivated, inch based series, for maximum operating temperature 750 °C.

This standard specifies the characteristics of solid rivets, with universal head, inch based series, in aluminium alloy, for maximum operating temperature 120°C.

This standard specifies the characteristics of solid rivets, with 100° normal countersunk head with dome, inch based series, in aluminium alloy, for maximum operating temperature 120 °C