Abstract: A boarding system and a computer-implemented method for boarding a plurality of passengers onto an aircraft, the aircraft having a plurality of seats and each passenger having an assigned seat from amongst the plurality of seats. The boarding system comprises a passenger monitoring system comprising a plurality of monitoring devices, the monitoring devices being configured to determine an occupancy of each of the plurality of seats and/or to determine an occupancy of one or more aisle or boarding tunnel; and a scheduling system configured to control a boarding schedule, the boarding schedule assigning each seat to one of a plurality of groups of seats, and comprising a pre-determined boarding sequence for the plurality of groups of seats.

Abstract: An oven comprising an injection nozzle includes a nozzle member that has a fluid inlet and a first fluid outlet that is in communication with the inlet The nozzle member is movable between: (i) a first position, in which the first fluid outlet is arranged so as to direct fluid towards and onto a component of the oven to be cleaned; and (ii) a second position, in which the first fluid outlet is blocked or otherwise arranged so as not to direct fluid towards and onto said component.

Abstract: A galley insert system for an aircraft galley comprises a galley support structure, a galley insert configured to be coupled to the support structure, and a latch mechanism for coupling the insert to the support structure, the latch mechanism configured to automatically engage to couple the insert to the support structure when the insert is moved into a latching position on the support structure, wherein the latch mechanism comprises a control mechanism configured to be actuated to disengage the latch mechanism.

Abstract: There is provided herein an aircraft galley container including a door, a latch mechanism, and a lock. The latch mechanism is positionable in a latched position preventing opening of the door and an unlatched position permitting opening of the door. The latch mechanism includes a handle, a pair of rods and a rotatable plate. The rotatable plate is coupled to the handle and configured to be rotated by the handle and to convert rotational movement of the handle to linear movement of the pair of rods to place the latch mechanism in the latched and unlatched positions. The lock is configured to selectively prevent the rotatable plate from rotation to maintain the latch mechanism in the latched position.

Abstract: There is provided herein an aircraft including at least one aircraft galley container and a controller. Each one of the at least one aircraft galley container includes a safety feature having a first mode and a second mode, and a controller for automatically selecting one of the first mode and second mode of the safety feature and placing the safety feature in the selected mode. The automatic selection of the mode is dependent on a condition of the aircraft satisfying or failing to satisfy a predetermined condition. There is also provided a method of operating a safety feature of an aircraft galley container.