The invention provides a
sediment discharge valve of an
aircraft fuel system, which belongs to the field of aircraft fuel systems and is characterized in that an oil passing hole is formed in the middle of a shell, and a stop part mounting groove is formed in the lower part; the arch-bridge-shaped elastic steel sheet and the stop part form a stop
assembly which is mounted in the stop part mounting groove; the
piston rod is of a multi-section variable-
diameter cylindrical structure and is arranged in the shell, the middle of the
piston rod is in sealing fit, the
piston rod is limited in the shell through an end cover, the upper portion of the
piston rod is sleeved with a spring and always compressed, the lower portion of the
piston rod is matched with a stop circular bead to achieve upward movement of the
piston rod to the opening position to be locked, and fuel flows out of the
fuel tank through a fuel hole. The self-locking oil drainage device can realize self-locking and unlocking at an opening position, can be mounted in a narrow space blocked by a multi-layer structure in an
airplane, and can realize a self-locking oil drainage function under the condition that the self-locking oil drainage device is invisible to an operator.