A passenger door arrangement for an aircraft segment, which arrangement comprises a passenger door that is configured to assume a raised state and a lowered state, and a girt bar for arming and disarming an escape slide, the girt bar not altering its position relative to the passenger door in the transition from disarming to arming when the passenger door is in the lowered state. Also an aircraft segment, which comprises the passenger door portion and a fuselage portion, an external engagement means being fixed to the fuselage portion.

A privacy door assembly for installation in an aircraft relative to a flight deck door of the aircraft includes a door frame having a first post and a second post, where the second post comprises a latch recess. The privacy door comprises a latch positioned on an edge of the privacy door and arranged to engage the latch recess when the privacy door is in a closed position within the door frame. An access door is positioned in the privacy door, where the access door is rotatable from a closed position to an open position in a forward direction. A first mechanical door handle system including a mechanical combination lock is positioned on an aft side of the privacy door and coupled to the latch, and a second mechanical door handle system is positioned on a forward side of the privacy door and coupled to the latch.

A privacy door assembly for installation in an aircraft relative to a flight deck door of the aircraft includes a door frame having a first post and a second post, where the second post comprises a latch recess. The privacy door comprises a latch positioned on an edge of the privacy door and arranged to engage the latch recess when the privacy door is in a closed position within the door frame. An access door is positioned in the privacy door, where the access door is rotatable from a closed position to an open position in a forward direction. A first mechanical door handle system including a mechanical combination lock is positioned on an aft side of the privacy door and coupled to the latch, and a second mechanical door handle system is positioned on a forward side of the privacy door and coupled to the latch.

An aircraft is equipped with an auxiliary access control barrier (AACB) to prevent access to an area of the aircraft. The AACB includes laterally extendable door panels that are slidably attached to each other to vary a width of the AACB, a hinge by which the door panels are pivotably attached to the aircraft, such that the door panels are pivotable between a deployed position, in which the door panels are positioned across the opening to prevent passage through the opening and in which the AACB has a first width, and a stowed position, in which the door panels are positioned to allow passage through the opening and in which the AACB has a second width, and one or more locks to prevent relative motion between the door panels to fix the width of the AACB and/or to secure the AACB within the opening in the bulkhead.

A windowed structure includes a body having a frame with an outer wall extending between a first end and a second end. An inner wall extends from the outer wall. The inner wall is connected to the outer wall at the first end to define a proximal joint of the body delimiting a window opening extending through the body. A window element covers the window opening and defines an outer window surface and an inner window surface. The window element has an overlap segment overlaying the outer wall and attached thereto. An unobstructed portion of the window element is defined between the overlap segment and is unobstructed by the frame between the proximal joint.

A bifold door includes a first hinge and a second hinge configured to rotatably couple the bifold door to a doorframe. The bifold door includes a slider configured to slide within a track of the doorframe as the bifold door is opened and closed. At least one of the first hinge, the second hinge, and the slider includes a spherical bearing and a pin.

Aircraft door (1) having: an opening panel (2) provided with engagement abutments (26); a frame (3) intended to be attached to the fuselage (4) of the aircraft and including engagement counter-abutments (27); a hinge arm (5); a lifting lever (10); and a rotary control lever (20) which can be operated in a disengagement direction in order to unlock the opening panel (2). The door includes a one-way operating rod (18) which connects the control lever (20) to the lifting lever (10) and is designed to drive the lifting lever (10) only when the control lever (20) is actuated in the direction of disengagement.

Aircraft door (1) including an opening (4), a frame (3), a hinge structure (5) and a circular translation guide device designed to maintain the orientation of the opening (4) during the opening or closing thereof. The hinge structure (5) is connected to the opening (4) by a lifting arm (8) allowing a lifting movement of the opening (4) relative to the hinge structure (5). The circular translation guide device includes a single link (11) connected to the frame (3) by one of the ends thereof and by the other of the ends thereof to a lever (13) which is attached to the hinge structure (5).

A privacy panel assembly for a passenger cabin environment including a flexible privacy panel having a leading edge and a trailing edge, the flexible privacy panel moveable between a stowed position leaving open an opening between spaced structures and a deployed position closing the opening, wherein the leading edge of the flexible privacy panel, when the flexible privacy panel is in the deployed position, is moveable out of a plane of the opening by way of force against the flexible privacy panel. A passenger suite configuration including a suite entrance formed between spaced walls and a flexible privacy panel moveable between a stowed position leaving open the suite entrance and a deployed position closing the suite entrance, wherein a portion of the flexible privacy panel is moveable out of a plane of the opening by way of force against the flexible privacy panel, for example, during emergency exit from the suite.

A system for detecting overpressure in an aircraft including a door with a door frame and a door leaf with a first and second door leaf face. The door is mountable in an aircraft where the first door leaf face faces the interior and the second door leaf face faces the surroundings of the aircraft. The door leaf is movably attached to the door frame and selectively movable between an opened position where a door opening defined by the door frame is accessible and a closed position where the door leaf closes off the door opening. The door has a pair of contact faces including a first contact face on the door leaf and a second contact face on the door frame. In the closed position, the first contact face bears on the second contact face such that, when a compressive force is applied to the first door leaf face in the direction of the second door leaf face, movement of the door leaf is counteracted and contact force between the first contact face and the second contact face of each pair increases as the compressive force increases.