Abstract: An aircraft fuselage comprising a structural wall and a floor delimiting a cabin for passengers, said wall being covered by a plurality of adjacent trim panels arranged in succession in the longitudinal direction of the fuselage and spaced from one another with a gap between two adjacent panels. Each panel is also fixed to the wall and has a concave shape adapted to the shape of the fuselage. At least one lighting device is disposed at the level of at least one of the gaps and is arranged perpendicularly to a longitudinal axis of the fuselage. The lighting device comprises a housing fixed to the wall. The housing is provided with an opening on a face oriented toward the interior of said cabin. The housing further comprises at least one lighting element making it possible to light the cabin through the gap.

Abstract: An aircraft fuselage provided with interior fit-out equipment, including a structure and decorative panels fixed to the structure one after the other at the level of at least one fixing point by a detachable link and delimiting a cabin. The fuselage further includes interior fit-out equipment disposed between two neighboring decorative panels which includes a base fixed to the fuselage, a flap mounted movably in respect of the base between a closed position in which the fixing points are hidden and inaccessible and an open position in which the fixing points are visible and accessible, and a lock that can be moved between a locked position in which the flap is kept in the closed position and an unlocked position in which the flap is free to move from the closed position into the open position and vice versa. Access to the fixing points is easy by moving the flap.

Abstract: An aircraft fuselage comprising a structural wall and a floor delimiting a cabin for passengers, said wall being covered by a plurality of adjacent trim panels arranged in succession in the longitudinal direction of the fuselage and spaced from one another with a gap between two adjacent panels. Each panel is also fixed to the wall and has a concave shape adapted to the shape of the fuselage. At least one lighting device is disposed at the level of at least one of the gaps and is arranged perpendicularly to a longitudinal axis of the fuselage. The lighting device comprises a housing fixed to the wall. The housing is provided with an opening on a face oriented toward the interior of said cabin. The housing further comprises at least one lighting element making it possible to light the cabin through the gap.