At present, all the high-temperature cured structural adhesive film are imported for the domestic civil aircraft projects. With the further application of domestic prepreg/composite materials in the field of civil aircraft, it is particularly important to develop the domestic high-temperature cured structural adhesive film. The structural adhesive film ACTECH1302F, which was independently developed and cured at high temperature (180 ℃), was tested and analyzed by infrared, gel time, rheological test and DSC in the paper. Test results indicate that the system of ACTECH1302F adhesive film and BA3202W prepreg have good compatibility. Besides, the mechanical properties of the adhesive film, such as double-lap shear strength and mode I interlaminar fracture toughness (GIC) were significantly better than the index values of high-temperature cured structural adhesive film used for civil aircraft composite materials. The structural adhesive film ACTECH1302F could match the system of domestic high temperature curing prepreg BA3202W, initially meeting the key technical requirements of high-temperature cured structure adhesive film for civil aircraft composites.