EXHAUST PLUG FOR AN AIRCRAFT TURBOJET ENGINE

摘要

This exhaust plug (1) for an aircraft turbojet engine, comprising a front part (5) intended for attachment to a rear part (7), each having an outer skin (21, 29), is characterised in that the front part and the rear part are connected by at least one connecting flange (31) common to these two parts and on which the outer skins are arranged side by side.