Laminated composites are rapidly finding uses indifferent engineering applications like Aviation, Sportsequipment, Marine technology, Aerospace and Electronics. Thisis due to their versatile engineering properties. Bolting andBonding are the widely used joining techniques in composites.However bonding has added advantages over bolting in terms ofweight reduction and strength .This paper explores the fatiguestrength of single lap epoxy bonded joint between compositelaminates. The experimental results are compared with FEA(Finite Element Analysis) results