AIRCRAFT CABIN DEVICE

The invention relates to an aircraft cabin device comprising at least one first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h), which comprises at least two aircraft seats (16a, 18a, 20a; 16b; 16c; 16d;16e, 18e; 16g, 18g, 20g; 16h) arranged next to one another, and comprising at least one second aircraft seat row (26a; 26b; 26c; 26d; 26e; 26f; 26g; 26h), which is arranged directly in front of the first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h) and which comprises at least one aircraft seat (28a, 30a, 32a; 28b, 30b; 28c, 30c; 28d; 28e; 28f, 30f, 28g, 30g, 32g, 74g; 30h), wherein the aircraft seats (16a, 18a, 20a, 28a, 30a, 32a; 16b, 28b, 30b; 16c, 28c, 30c; 16d, 28d;16e, 18e, 28e; 16g, 18g, 20g, 20g, 72g, 28g, 30g, 32g, 74g; 16h, 30h) of the first and second aircraft seat row (12a, 26a; 12b, 26b; 12c, 26c; 12d, 26d; 12e, 26e; 12f, 26f; 12g, 26g; 12h, 26h) have substantially the same seat direction. According to the invention, at least one sub-region (44a; 44b; 44c; 44d; 44e; 44f; 44g; 44h) of the front second aircraft seat row (26a; 26b; 26c; 26d; 26e; 26f; 26g; 26h) is designed to form a common use area (46a; 26b; 46c; 46d; 46e; 46f; 46g; 46h) together with the first aircraft seat (16a; 16b; 16c; 16d; 16e; 16f; 16g; 16h) of the rear first aircraft seat row (12a; 12b; 12c; 12d; 12e; 12f; 12g; 12h) arranged directly behind said sub-region.