FUEL ASSEMBLY FOR A GAS TURBINE ENGINE

A fuel assembly (32) for a gas turbine engine (10) includes a fuel supply tube, a fuel port (60), a fuel manifold (52), and a fuel manifold adapter (64). The fuel supply tube is configured to convey a fuel. The fuel port (60) is fluidly coupled to the fuel supply tube and configured to receive the fuel from the fuel supply tube. The fuel manifold (52) includes a fuel inlet (86) and a plurality of fuel outlets (88). The fuel inlet (86) is fluidly coupled to the fuel port (60) and configured to receive the fuel from the fuel port (60). The fuel manifold adapter (64) includes a first mount portion (108) and a second mount portion (110). The first mount portion (108) is connected to the fuel port. The first mount portion is moveable relative to the second mount portion.