Abstract: A seat system for a passenger aircraft. The seat system includes a passenger seat frame having a backrest support assembly and a seat bottom support assembly. A quadrant assembly is connected between the backrest support assembly and the seat bottom support assembly. The quadrant assembly includes a quadrant member including a pivot point adapted to pivot the backrest with respect to the seat bottom support assembly and the quadrant member. The quadrant member is attached to the backrest and adapted to break away in the event of an impact with the backrest. The quadrant assembly may further include a pivot point brake assembly attached to the pivot point and adapted to provide a controlled stop of the backrest in the event of an impact with the backrest. In addition, a seat back tray table may be attached to the back of the passenger seat frame.

Abstract: A cushion-less passenger seat. The passenger seat includes spaced left and right spreaders, each having a front and rear leg with top and bottom ends and a seating surface fanned from a flexible bottom diaphragm attached to and extending between the left and right spreaders. The passenger seat also includes a lumbar support having lower and upper sections and front and back sides formed from a flexible diaphragm. The lower section of the lumbar support is attached to and between the left and right spreaders. The lumbar support upper section extends upwardly above the seat's rear legs and seating surface.

Abstract: A cushion-less passenger seat. The passenger seat includes spaced left and right spreaders, each having a front and rear leg with top and bottom ends and a seating surface formed from a flexible bottom diaphragm attached to and extending between the left and right spreaders. The passenger seat also includes a lumbar support having lower and upper sections and front and back sides formed from a flexible diaphragm. The lower section of the lumbar support is attached to and between the left and right spreaders. The lumbar support upper section extends upwardly above the seat's rear legs and seating surface.

Abstract: An improved seating apparatus for an aircraft includes a seat assembly and a quick install track fitting assembly for securing the seat assembly to the aircraft. In a preferred embodiment, the quick install track fitting assembly is made up of a track fitting body for insertion into an aircraft seat track and a manual lever that is pivotably attached to the track fitting body. The manual lever has a lever release position and a lever lock position. A force bearing plunger is movably attached to the manual lever for transferring force to the aircraft seat track. The force bearing plunger has a track release position and a track lock position, wherein both positions correspond to the lever release and lever lock positions of the manual lever. A lock may also be provided for maintaining the plunger in the track lock position when the manual lever is in the lever lock position.

Abstract: A cushion-less passenger seat. The passenger seat includes spaced left and right spreaders, each having a front and rear leg with top and bottom ends and a seating surface formed from a flexible bottom diaphragm attached to and extending between the left and right spreaders. The passenger seat also includes a lumbar support having lower and upper sections and front and back sides formed from a flexible diaphragm. The lower section of the lumbar support is attached to and between the left and right spreaders. The lumbar support upper section extends upwardly above the seat's rear legs and seating surface.

Abstract: An improved seating apparatus for an aircraft comprising: a seat assembly; and a wedge lock device for securing the seat assembly to the aircraft without any rattle. In the preferred embodiment, the wedge lock device includes: a selectively adjustable force applicator for applying force to a force bearer; a force bearer for transferring force to an aircraft seat track; and a stud connected to the seat assembly. Also in the preferred embodiment, the seat assembly includes a seat leg.

Abstract: A seating apparatus for an aircraft comprising: a passenger seat having a seat frame and a seat back; a recline control device for selectively reclining the seat back; and a seat recline control override for disabling the recline control device. In the preferred embodiment, the passenger seat includes a seat leg supporting the seat. Also in the preferred embodiment, the seat recline control override comprises: an override lever for overriding the recline control; an actuator for remotely moving the override lever; and a linkage connecting the override lever to the actuator.