Abstract: Systems and methods are provided for trimming and installation. One embodiment is a system for cutting out portions of a fuselage section. The system includes an Inner Mold Line (IML) tool comprising an inner gripping element configured to apply suction to a portion of the fuselage section, and further comprising an outer gripping element configured to apply suction to an area surrounding the portion, an Outer Mold Line (OML) tool configured to operate a cutter to cut the portion out from the fuselage section while suction is applied to the portion and to the area surrounding the portion, and a track that is disposed between the IML tool and the OML tool, wherein the fuselage section is configured to be pulsed in a process direction along the track, such that the fuselage section remains disposed between the IML tool and the OML tool when pulsed in the process direction.

Abstract: Systems and methods are provided for advancing a fuselage section of an aircraft. One embodiment is a system that includes a series of plates configured to be sequentially affixed along a length of the fuselage section, and a track configured to form a frictional fit with the plates. The track includes drive units configured to form nips retaining the series of plates, and that are configured to advance the fuselage section along the track in a process direction, and indexing elements that are configured to engage with indexing elements at the plates during pauses between operation of the drive units. The system also includes tools configured to perform work on the fuselage section while the indexing elements of the track are engaged.

Abstract: Systems and methods are provided for trimming and installation. One embodiment is a system for cutting out portions of a fuselage section. The system includes an Inner Mold Line (IML) tool comprising an inner gripping element configured to apply suction to a portion of the fuselage section, and further comprising an outer gripping element configured to apply suction to an area surrounding the portion, an Outer Mold Line (OML) tool configured to operate a cutter to cut the portion out from the fuselage section while suction is applied to the portion and to the area surrounding the portion, and a track that is disposed between the IML tool and the OML tool, wherein the fuselage section is configured to be pulsed in a process direction along the track, such that the fuselage section remains disposed between the IML tool and the OML tool when pulsed in the process direction.

Abstract: Systems and methods are provided for advancing a fuselage section of an aircraft. One embodiment is a system that includes a series of plates configured to be sequentially affixed along a length of the fuselage section, and a track configured to form a frictional fit with the plates. The track includes drive units configured to form nips retaining the series of plates, and that are configured to advance the fuselage section along the track in a process direction, and indexing elements that are configured to engage with indexing elements at the plates during pauses between operation of the drive units. The system also includes tools configured to perform work on the fuselage section while the indexing elements of the track are engaged.