The invention discloses a metal part production and forming process for the aviation field, relates to the technical field of metal part production and manufacturing, and aims to solve the problems that in the heating stage of a casting, if equipment breaks down, no emergency treatment measures exist, and the alloy plasticity of the casting is easily affected in the existing metal part production and forming process for the aviation field. The process comprises the following steps of, 1, preparing a titanium ingot, reducing titanium ore into pure titanium tetroxide through chlorination and distillation, refining the pure titanium tetroxide into a sponge titanium raw material by virtue of vacuum separation, removing impurities, and obtaining the titanium ingot through electrode welding; 2, carrying out end face pretreatment, specifically, cleaning one end face of the titanium ingot, spraying an anti-oxidation coating after cleaning is completed, and marking an ingot number; and 3, carrying out pretreatment on the titanium ingot, placing the face, with the ingot number, of the titanium ingot on an adsorption base of a cleaning and spraying all-in-one machine, and fixing the titanium ingot to the adsorption base through suction force generated by a vacuum generator.