Fuel manifold fitting with integral support for a gas turbine engine and method of mounting a fuel supply manifold assembly

摘要

A manifold fitting (120) for a gas turbine engine includes a manifold tee (152) including a first manifold port (160), a second manifold port (162) and a pigtail port (164). A support (154) extends from the manifold tee (152). The support (154) defines a support aperture (170) along a mount axis (W). A support tab (156) extends from the support (154).