Abstract: The invention relates to a rest module for accommodating a least one crew member of an aircraft, wherein the module comprises a first partial module. Further on the first partial module comprises a first section and a second section; wherein the first section and the second section are spatially divided. The first section comprises a first opening, a second opening and a third opening, wherein the three openings are different from each other. The first opening is adapted for providing an access from an above located area of the aircraft, the second opening is adapted for providing an access from the first section to a second partial module and the third opening is adapted for providing a separate access from the first section to the second section.

Abstract: A front portion of a fuselage of an aircraft including a cockpit, a washroom, an access corridor to the cockpit alongside the washroom, and a rest compartment with at least one berth for at least one pilot. The corridor alongside the washroom includes a mechanism separating the corridor from the cockpit and a door for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor to the cockpit, between the separation mechanism between the corridor and the cockpit and the corridor door. The washroom includes two access doors, a first access door for accessing the washroom from the access corridor to the cockpit in the area located between the separation mechanism between the corridor and the cockpit and the corridor door, and a second access door for accessing the washroom from the passenger cabin.

Abstract: According to an exemplary embodiment of the invention, a combined habitation module for the crew of an aircraft is provided, which habitation module comprises two monument units that are separated from each other by a gap such that acoustic decoupling of the two monument units from each other is provided. In this way noise propagation within the habitation module may be prevented to a large extent.

Abstract: The invention relates to a rest module for accommodating a least one crew member of an aircraft, wherein the module comprises a first partial module. Further on the first partial module comprises a first section and a second section; wherein the first section and the second section are spatially divided. The first section comprises a first opening, a second opening and a third opening, wherein the three openings are different from each other. The first opening is adapted for providing an access from an above located area of the aircraft, the second opening is adapted for providing an access from the first section to a second partial module and the third opening is adapted for providing a separate access from the first section to the second section.

Abstract: A front portion of a fuselage of an aircraft including a cockpit, a washroom, an access corridor to the cockpit alongside the washroom, and a rest compartment with at least one berth for at least one pilot. The corridor alongside the washroom includes a mechanism separating the corridor from the cockpit and a door for blocking access to the passenger cabin. The rest compartment can be accessed from the access corridor to the cockpit, between the separation mechanism between the corridor and the cockpit and the corridor door. The washroom includes two access doors, a first access door for accessing the washroom from the access corridor to the cockpit in the area located between the separation mechanism between the corridor and the cockpit and the corridor door, and a second access door for accessing the washroom from the passenger cabin.

Abstract: According to an exemplary embodiment of the invention, a combined habitation module for the crew of an aircraft is provided, which habitation module comprises two monument units that are separated from each other by a gap such that acoustic decoupling of the two monument units from each other is provided. In this way noise propagation within the habitation module may be prevented to a large extent.