The invention provides an aeronautical photoelectric hybrid cable, which comprises an optical unit and an electrical unit, wherein the optical unit includes an optical fiber, a PTFE/PI/PTFE compositetape longitudinal wrap and a first outer sheath which are successively arranged from the inside out, the electrical unit includes carbon fire conductors, the optical unit and the electrical unit forma photoelectric hybrid body, and the photoelectric hybrid body is externally sleeved with an inner protective layer, a braided shielding layer and a second outer sheath in sequence. Compared with theprior art, the beneficial effects lie in that the photoelectric hybrid cable is excellent in overall performance, high temperature resistant, good in reliability and light in weight, adopts the carbonfibers to replace copper conductor for power transmission and only needs a photoelectric hybrid connector in installation through being combined with an optical cable, thereby effectively controllingthe cost. Silver-plated aramid filaments are good in strength and shielding effect and can be welded, thereby not only being capable of serving as a force bearing layer, but also being capable of serving as a shielding anti-interference layer.