| 摘要 |
An interior configuration of a corporate aircraft, comprises an entrance compartment (100), which is situated directly next to a cockpit (C) of the aircraft, passenger compartment (200) which is adjacent to the entrance compartment (100) opposite to the cockpit (C), an en suite lavatory compartment (300) which is adjacent to the passenger compartment (200) opposite to the entrance compartment (100). The passenger compartment (200) further comprises a first functional area (210) which is adjacent to the entrance compartment (100), is used as a support staff cabin, and comprises at least one seat (S) in a first seat row arrangement (A1), a second functional area (220) which is next to the first functional area (210), is used as a high-end cabin, wherein the second functional area (220) is configurable from at least a first configuration to at least a second configuration, and a first bulkhead divider (B1) between the first functional area (210) and the second functional area (220) which comprises a first pocket door (P1) and first mounting means for allowing the first pocket door (P1) to move between an open and a closed position. |
