Cable conduit for turbine engine bypass

A gas turbine engine comprising:

• a compressor section configured to compress a gas;
• a combustor section aft of the compressor section and configured to combust the gas;
• a fan section configured to produce a bypass flow;
• an outer case having an inner surface and an inner case having an outer surface defining a bypass flow duct there between;
• and
• a cable conduit, disposed within the bypass flow duct, comprising:
• a head end, a sleeve having a foot end, a boot, and a split grommet,
• wherein the head end is coupled to the sleeve opposite the foot end,
• wherein the boot comprises a first flange and a neck,
• wherein the neck is coupled to a flared portion of the foot end,
• wherein the head end comprises a second flange having and a cutout penetrating into an interior volume of the sleeve,
• wherein the split grommet is coupled within the interior volume of the sleeve, and
• wherein the second flange is coupled the inner case and the first flange is coupled to the outer case.