A fuel manifold may be provided for use in a turbine engine. The fuel manifold may include four discrete segments including a first segment, a second segment, a third segment, and a fourth segment. The fuel manifold may also include a first line coupled to the first segment and the second segment and a second line coupled to the third segment and the fourth segment. The first line may be configured to supply a first portion of the fuel to the first segment and a second portion of the fuel to the second segment. The second line may be configured to supply a third portion of fuel to the third line and a fourth portion of fuel to the fourth segment.