A method for embedding fasteners in sealant wherein the fasteners are used to secure a skin (17, 18, 22, 23) of a wing (11, 12) of an aircraft to a side of body chord of the aircraft, the side of body chord including a first plate and a second plate that extend outward from a wall, the fasteners connecting the skin to the first plate with portions of the fasteners disposed between the two plates and between the wall of the side of body chord and a structural member of the wing, the method comprising: providing a first containment member configured to extend between the first and second plates and a second containment member configured to extend between first and second plates, the first and second containment members each comprising structure-engaging ends (43, 44) for engaging the structural member of the wing and enclosure ends (46, 47) for connecting the first and second containment members together in a spaced-apart relationship, at least one of the first and second containment members comprising at least one injection port that is in communication with at least one distribution passageway that comprises at least one distribution port; providing an alignment member configured to extend between the first and second plates and further configured to align and connect the enclosure ends of the first and second containment members together; connecting the first and second containment members to the alignment member and engaging the structure-engaging ends of the first and second containment members with the structural member to provide a confined space between the first and second containment members, between the first and second plates and between the structural member and the alignment member; and injecting sealant into the at least one injection port and out through the at least one distribution port and into the confined space. providing a first containment member configured to extend between the first and second plates and a second containment member configured to extend between first and second plates, the first and second containment members each comprising structure-engaging ends (43, 44) for engaging the structural member of the wing and enclosure ends (46, 47) for connecting the first and second containment members together in a spaced-apart relationship, at least one of the first and second containment members comprising at least one injection port that is in communication with at least one distribution passageway that comprises at least one distribution port; providing an alignment member configured to extend between the first and second plates and further configured to align and connect the enclosure ends of the first and second containment members together; connecting the first and second containment members to the alignment member and engaging the structure-engaging ends of the first and second containment members with the structural member to provide a confined space between the first and second containment members, between the first and second plates and between the structural member and the alignment member; and injecting sealant into the at least one injection port and out through the at least one distribution port and into the confined space.