LOCKING DEVICE

The present invention relates to a locking device designed for locking the dome of a military aircraft, the doors of civil aircraft or for a system having little room for locking but requiring an advanced security The locking device comprises a locking sub-asembly (a), an adjustment sub-assembly (B) permiting the adjustment of the cinematic parameters of the locking sub-assembly (A), both of them belonging to a locking device (c) a housing (D)and an adjustment sub-assembly (E) for adjusting the locking device depending on the geometrical necessities of the mounting space The locking mechanism (C) is detachable from housing making possible the repairment of the locking device (C) without the detachment of the entire device from the mounting place