Turbine engine having an engine core and a bleed air conduit

A turbine engine comprising:

• an engine core comprising
• a compressor section,
• a combustor section, and
• a turbine section in serial flow arrangement and defining a stator, a rotor, and a fire zone;
• a fan section rotationally coupled to the rotor;
• a bleed air conduit fluidly coupled to at least one of the fan section or the compressor section and having a gravitational low point within the fire zone;
• and
• a drain assembly provided along the bleed air conduit at a junction, the drain assembly including
• a weep hole fluidly coupled to the gravitational low point,
• an area between the junction and the weep hole in which condensation is configured to pool, and
• a drain conduit fluidly coupled to the weep hole and having a drain conduit outlet exterior the fire zone;
• wherein the weep hole comprises a funnel at an inlet of the weep hole and an expander at an outlet of the weep hole.