This paper suggests the latest manufacturing design approach of a helicopter frame, mainly involving its pattern plane creating, fabric sourcing ratio, blank design continuous layout, as well as pinpointing the pressure center point and tool design. It starts by the creation of a pattern plane where the particular geometry of each frame is specifically identified and optimal material can be identified. It entails doing a detailed research on the material qualifying- characteristics and structure- requirements while making a good use of resources without sacrificing structural integrity. Among the other vital aspects, the material utilization is an important one. The objectives of this stage are the utilization of material in the best way which leads to the waste reduction, even though the requirements need for the product should not be affected. For what now,blank layout can be discussed. On this stage a tangible form of a pattern plane is translated with the resulting piece as underpinnings for a fabrication process of a proposed object. Instead of that, properties of the materials, manufacturing restrictions, and critical parameters are studied for the blank optimizing. Another important design element, where the center point of pressure is determined, is pressure point assembly of the frame for the helicopter. Next off the paper is to design the tooling of the machines used to make the helicopter frame. This in addition to the molding, forming, and assembling of parts using dies, jigs, and fixtures creates long lasting assemblies with less error rates. Overall it can be claimed that this article has given a clear procedure of a helicopter undercarriage design, putting the utilization of material to the highest priority, strengthening structure, and the ability to boost efficiency of production through improved tool design.