In the recent trends, several researches are happening in the area of Composite Materials especially in the case of hybrid composites to avail the higher properties of the hybridized fibres. It has become more challenging in the Aerospace industry as it is essential to develop a material which satisfies all property strength and to attain better strength to weight ratio. In this line of research, properties such as tensile, compression, shear and flexural are considered for the materials with the hybridization of E-glass in Kevlar 49 fibres at different orientation. Initially experimental analyses were done on these materials at a constant volume fraction of varying orientation and obtained the property strength values as per ASTM standard of composite material test procedure. In continuation to this experimental work, detailed Finite Element Analysis on same configuration is conducted using ANSYS. The primary objective is to do static structural analysis of the hybrid composites under tensile, compression, shear and flexural load and to validate with the experimental results. © IAEME Publication Scopus Indexed.