Abstract: A bench seat assembly that includes a first seat that includes a seat portion and a back, a second seat that includes a seat portion and a back, and a center portion positioned between the first and second seats. The first seat is bifurcated by a first vertical plane, the second seat is bifurcated by a second vertical plane, and the center portion is bifurcated by a center vertical plane. The first seat is angled outwardly such that the first plane defines a first acute angle with the center plane and the second seat is angled outwardly such that the second plane defines a second acute angle with the center plane. The first acute angle and the second acute angle are approximately the same.

Abstract: A hinge assembly for an aircraft overhead storage bin that includes a housing having a hinge space and a hinge opening defined therein, an arm pivotably connected to the housing within the hinge space, and a dampener. The hinge opening communicates the hinge space with an exterior of the housing. The arm is pivotable between a closed position and an open position and extends through the hinge opening such that the first end of the arm is positioned outside of the housing. The dampener includes first and second ends. The first end is connected to the housing and the second end is connected to the arm. The dampener biases the arm from the closed position to the open position.

Abstract: A hinge assembly for an aircraft overhead storage bin that includes a housing having a hinge space and a hinge opening defined therein, an arm pivotably connected to the housing within the hinge space, and a dampener. The hinge opening communicates the hinge space with an exterior of the housing. The arm is pivotable between a closed position and an open position and extends through the hinge opening such that the first end of the arm is positioned outside of the housing. The dampener includes first and second ends. The first end is connected to the housing and the second end is connected to the arm. The dampener biases the arm from the closed position to the open position.

Abstract: A hinge assembly for an aircraft overhead storage bin that includes a housing having a hinge space and a hinge opening defined therein, an arm pivotably connected to the housing within the hinge space, and a dampener. The hinge opening communicates the hinge space with an exterior of the housing. The arm is pivotable between a closed position and an open position and extends through the hinge opening such that the first end of the arm is positioned outside of the housing. The dampener includes first and second ends. The first end is connected to the housing and the second end is connected to the arm. The dampener biases the arm from the closed position to the open position.

Abstract: A bench seat assembly that includes a first seat that includes a seat portion and a back, a second seat that includes a seat portion and a back, and a center portion positioned between the first and second seats. The first seat is bifurcated by a first vertical plane, the second seat is bifurcated by a second vertical plane, and the center portion is bifurcated by a center vertical plane. The first seat is angled outwardly such that the first plane defines a first acute angle with the center plane and the second seat is angled outwardly such that the second plane defines a second acute angle with the center plane. The first acute angle and the second acute angle are approximately the same.

Abstract: An aircraft that includes a cabin interior that is bifurcated into first and second sides and includes a pilot zone and a passenger zone aft of the pilot zone, a pilot seat positioned in the pilot zone and on a first side of the cabin interior, and first and second rows positioned in the passenger zone. The front row includes first and second front seats positioned on first and second sides of the cabin interior, respectively. The first and second front seats are angled away from one another and the second front seat is positioned forwardly of the first front seat. The back row includes first and second back seats positioned on first and second sides of the cabin interior, respectively.

Abstract: An aircraft that includes a body that defines a cabin interior, front and back rows of seats positioned in the passenger zone, a forward door that is pivotable between a closed position and an open position, and an aft door that is pivotable between a closed position and an open position. The cabin interior includes a pilot zone, a passenger zone positioned aft of the pilot zone, and a cargo zone positioned aft of the passenger zone. The pilot zone and the front row of seats are accessible and the back row and cargo zone are inaccessible from an exterior of the body when the aft door is in the closed position and the forward door is in the open position. The back row and cargo zone are accessible and the pilot zone and the front row of seats are inaccessible from the exterior of the body when the aft door is in the open position and the forward door is in the closed position.

Abstract: A hinge assembly for an aircraft overhead storage bin that includes a housing having a hinge space and a hinge opening defined therein, an arm pivotably connected to the housing within the hinge space, and a dampener. The hinge opening communicates the hinge space with an exterior of the housing. The arm is pivotable between a closed position and an open position and extends through the hinge opening such that the first end of the arm is positioned outside of the housing. The dampener includes first and second ends. The first end is connected to the housing and the second end is connected to the arm. The dampener biases the arm from the closed position to the open position.

Abstract: A method of pivoting an aircraft storage bin that includes a bucket that pivots with respect to an upper housing. The method includes pivoting the bucket from a closed position to an intermediate position and placing weight that exceeds a predetermined weight threshold in the bucket, thereby causing the bucket to move to an open position. Movement of the bucket to the open position causes a lift assist unit to activate. A first end of the lift assist unit is connected to the bucket and a second end of the lift assist unit is connected to the upper housing. The method also includes pivoting the bucket from the open position to the closed position. The lift assist unit provides assistance as the bucket is pivoting from the open position to the closed position.

Abstract: An aircraft that includes a body that defines a cabin interior and a longitudinal axis, and a front row positioned in the cabin interior. The front row includes a first front seat and a second front seat. The first and second front seats are angled away from one another. The first front seat is angled outwardly such that it forms a first acute angle with the longitudinal axis and the second front seat is angled outwardly such that it forms a second acute angle with the longitudinal axis. The first and second acute angles are approximately the same.

Abstract: An aircraft that includes a body that defines a cabin interior, a divider member that divides the cabin interior into a cargo hold and a passenger cabin, front and back rows of seats positioned in the passenger cabin, a forward door that is pivotable between a closed position and an open position, and an aft door that is pivotable between a closed position and an open position. Pivoting one of the forward door or the aft door from the closed to the open position causes the other of the forward door or the aft door to pivot from the closed position to the open position.

Abstract: An aircraft that includes a cabin interior that is bifurcated into first and second sides and includes a pilot zone and a passenger zone aft of the pilot zone, a pilot seat positioned in the pilot zone and on a first side of the cabin interior, and first and second rows positioned in the passenger zone. The front row includes first and second front seats positioned on first and second sides of the cabin interior, respectively. The first and second front seats are angled away from one another and the second front seat is positioned forwardly of the first front seat. The back row includes first and second back seats positioned on first and second sides of the cabin interior, respectively.

Abstract: An aircraft that includes a body that defines a cabin interior, a divider member that divides the cabin interior into a cargo hold and a passenger cabin, front and back rows of seats positioned in the passenger cabin, a forward door that is pivotable between a closed position and an open position, and an aft door that is pivotable between a closed position and an open position. Pivoting one of the forward door or the aft door from the closed to the open position causes the other of the forward door or the aft door to pivot from the closed position to the open position.

Abstract: An aircraft that includes a body that defines a cabin interior and a longitudinal axis, and a front row positioned in the cabin interior. The front row includes a first front seat and a second front seat. The first and second front seats are angled away from one another. The first front seat is angled outwardly such that it forms a first acute angle with the longitudinal axis and the second front seat is angled outwardly such that it forms a second acute angle with the longitudinal axis. The first and second acute angles are approximately the same.

Abstract: An aircraft that includes a body that defines a cabin interior, front and back rows of seats positioned in the passenger zone, a forward door that is pivotable between a closed position and an open position, and an aft door that is pivotable between a closed position and an open position. The cabin interior includes a pilot zone, a passenger zone positioned aft of the pilot zone, and a cargo zone positioned aft of the passenger zone. The pilot zone and the front row of seats are accessible and the back row and cargo zone are inaccessible from an exterior of the body when the aft door is in the closed position and the forward door is in the open position. The back row and cargo zone are accessible and the pilot zone and the front row of seats are inaccessible from the exterior of the body when the aft door is in the open position and the forward door is in the closed position.

Abstract: A divider assembly that includes a main body portion having a lower section and an upper section and a removable panel having front and back surfaces. The upper section tapers in width in an upward direction and the main body portion includes front and back surfaces. The removable panel is removably secured to the upper section on the front surface of the main body portion.

Abstract: A method of pivoting an aircraft storage bin that includes a bucket that pivots with respect to an upper housing. The method includes pivoting the bucket from a closed position to an intermediate position and placing weight that exceeds a predetermined weight threshold in the bucket, thereby causing the bucket to move to an open position. Movement of the bucket to the open position causes a lift assist unit to activate. A first end of the lift assist unit is connected to the bucket and a second end of the lift assist unit is connected to the upper housing. The method also includes pivoting the bucket from the open position to the closed position. The lift assist unit provides assistance as the bucket is pivoting from the open position to the closed position.

Abstract: A divider assembly that includes a main body portion having a lower section and an upper section and a removable panel having front and back surfaces. The upper section tapers in width in an upward direction and the main body portion includes front and back surfaces. The removable panel is removably secured to the upper section on the front surface of the main body portion.