ASD/MAT - Materials

This document specifies the dimensions and tolerances for corrosion resisting steel drawn lockwire for aerospace applications.

This standard specifies the electrolytic cadmium plating of parts in steels of tensile strength Rm (max.)

This Standard specifies the minimum requirements for the qualification and approval of personnel involved in the application of non-destructive testing (NDT). These requirements include training, experience and examination within the aerospace industry (manufacture and service).

This standard specifies the requirements relating to sheet and strip, in aluminium AL-P1050A, for use in the H14 condition 0,4 mm <= a <= 6 mm, for aerospace applications.

This standard specifies the requirements relating to extruded bars and sections in aluminium alloy AL-P7075-, for use in the T73511 condition, a ou D <= 100 mm,with peripheral coarse grain control, for aerospace applications. This standard may also be used to supply material in the T73510 or T6510 condition, if the purchaser specifies this condition on the order. In this case the designation of line 97 shall not be used.

This standard specifies ageing tests for determining resistance of adhesive bonded joints against environmental influences.

This standard specifies the test method for the determination of the peeling strength of structural adhesives on metal to honeycomb core at ambient and other temperatures.

This standard specifies the test methods for the determination of the strength of structural adhesives on metal-honeycomb structures flatwise tensile at ambient and other temperatures.

This standard specifies the dimensions of the test samples and the test method for the determination of the strength of structural adhesives in metal to metal peel at ambient and other temperatures. This test procedure is not suitable for adhesives having an average peeling strength of less than 30 N per 25 mm.

This standard specifies the requiremets relating to sheet and strip, in alluminium alloy AL-P2014A, for use in the T6 or T62 condition, 0,4mm < a < 6mm,for aerospace applications.

This standard specifies the requirements relating to sheet and strip, in aluminium alloy AL-P2014A, for use in the T4 or T42 condition, 0,4mm < a < 6mm, for aerospace applications.

This standard specifies the requirements relating to sheet and strip, in aluminium alloy AL-P5086-, for use in the H111 condition, 0,3 mm <= a <= 6 mm, for aerospace applications.

This standard specifies the requirements relating to clad sheet and strip, in aluminium alloy AL-P7075-, for use in T6 or T62 conditions, 0,4 mm <= a <= 6 mm,for aerospace applications.

This standard specifies the requirements relating to sheet and strip, in aluminium alloy AL-P6061-, for use in the T6 or T62 condition, 0,4 mm <= a <= 6 mm, for aerospace applications.

This standard specifies the requirements relating to sheet and strip, in aluminium alloy AL-P7075-, for use in the T6 or T62 condition, 0,4 mm < a < 6 mm, for aerospace applications.

This standard specifies the requirments relating to sheet and strip, in aluminium alloy AL-P6081-, for use in the T6 condition, 0,3 mm <= a <= 6mm, for aerospace applications.

This standard describes and gives the general rules for the use of the manufacturing schedule, the inspection and test report when they are contractual documents requested by the purchaser. It shall be applicable whenever referenced.