BS EN 4338:2001

What is BS EN 4338 – Heat-resisting alloy NI-WH8901 (NiCr16Ti3Mn2) for Filler metal about?  

BS EN 4338 is an international standard used for the Aerospace series. This helps in manufacturing good quality Heat-resisting alloy NI-WH8901 (NiCr16Ti3Mn2) used in aerospace applications.  

BS EN 4338 specifies the requirements relating to Heat resisting alloy NI-WH3902 (NiCr25Mo10C) Filler metal for welding Wire and rod for aerospace applications. 

Who is BS EN 4338 – Heat-resisting alloy NI-WH8901 (NiCr16Ti3Mn2) for Filler metal for? 

BS EN 4338 on Heat resisting alloy NI-WH8901 (NiCr16Ti3Mn2) for Filler metal is useful for: 

• The aerospace and defence industry   
• Manufacturers of aerospace equipment and components   
• Vendors / Manufacturers and suppliers of sheet and strip steel for aerospace  
• Purchase divisions/component sourcing personnel  
• Product design engineers   
• Aeronautical engineers   

Why should you use BS EN 4338 – Heat-resisting alloy NI-WH8901 (NiCr16Ti3Mn2) for Filler metal?  

Filler metal can be used to join most magnesium wrought alloys.  The filler has the best weldability and weld strength for magnesium alloys.  

BS EN 4338 specifies the requirement related to Heat-resisting alloy NI-WH8901 (NiCr16Ti3Mn2) used for welding wire and rods in aerospace applications. This helps in identifying the hazardous substances used in the manufacturing process. With the help of  BS EN 4338, you can ensure the sustainability of these requirements in different climatic conditions.  

By applying BS EN 4338, you can standardize the manufacturing process which results in producing good quality Heat-resisting alloy NI-WH8901 (NiCr16Ti3Mn2) for Filler metal used in Aerospace applications.