Abstract: A flight attendant seat arrangement comprises a monument which is suitable for installation in an aircraft cabin, a first receiving recess being constructed in a wall of said monument. A flight attendant seat has a backrest element and also a seat element. The backrest element and seat element are at least partially received within the first receiving recess constructed in the wall of the monument. The wall of the monument is of a double-walled design comprising a support wall which forms the rear wall of the first receiving recess and extends from said first receiving recess as far as an end of the monument on a floor side, and an outer wall which is oriented substantially parallel to the support wall, and wherein the backrest element and the seat element of the flight attendant seat are fastened to the support wall.

Abstract: A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements.

Abstract: A flight attendant seat arrangement comprises a monument which is suitable for installation in an aircraft cabin, a first receiving recess being constructed in a wall of said monument. A flight attendant seat has a backrest element and also a seat element. The backrest element and seat element are at least partially received within the first receiving recess constructed in the wall of the monument.

Abstract: A system for mounting aircraft system components in the crown area of an aircraft comprising a first longitudinal carrier element, a second longitudinal carrier element and a bridging element which connects the first longitudinal carrier element to the second longitudinal carrier element. The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier elements extend substantially parallel to the longitudinal axis of the aircraft. A plurality of cable ducts for accommodating electrical lines is provided on the first and/or the second longitudinal carrier elements.