Many industries including aerospace make extensive use of lightweight materials like aluminium alloys because of their extraordinary properties. Wire Arc Additive Manufacturing-Cold Metal Transfer (WAAM-CMT) as a part of modern direct energy deposition technique can be recommended for developing aerospace components of aluminium alloys. However, it is still necessary to investigate the impact of the combined change of developing parameters on some of the crucial qualities including metallurgical and mechanical properties. Therefore, in this part of research work, practically, various process parameters were tried for development of aluminium (Al-5356) alloy walls. Finaly, a specific set of parameters namely wire feed speed, scanning speed and inter layer temperature parameters with two levels of each were selected and with the assistance of these, four walls have been fabricated. Th preliminary analysis showed that low heat input accompanied by higher scanning speed of 60 cm/min and lower wire feed rate of 6 m/min was found to best suitable set of parameters for developing dimensionally stable Al wall with flaw less microstructure. The said set of parameters also showed higher hardness that also accompanied with finer grains, lower percentage towards high angle grain boundary and lower KAM. Even slight variation in these parameters that deal to high heat input can give rise of porosity and misalignment in the wall. Details of microhardness reported high hardness in the bottom part of the wall. However, in a single bead the hardness is higher in the top region, which may be owing to finer grains in the specified region. The above said set of parameters also able to deliver better tensile strength and toughness for Al-5356 alloy. The developed alloy showed improved strength in longitudinal orientation owing to intra layer failure with ductile mode of fracture in contrast to transverse orientation, where the failure mode was reported to mixed (ductile as well as brittle) owing to inter layer fracture.