| 摘要 |
A method of installing fuel system components (6, 10, 12, 13, 14, 16) in an aircraft wing is disclosed. An aircraft wing having a plurality of structural elements such as ribs (4) which are joined together during assembly. The method includes the step of attaching at least some of the fuel system components (6, 10, 12, 13, 14, 16) to at least one of the structural elements prior to joining said structural elements together to assemble a wing. Also disclosed is a structural rib (4) for an aircraft wing, configured to receive one or more fuel system components (6, 10, 12, 13, 14, 16), and a combined structural rib and fuel system assembly. |
