A vertical adjustment system for an aircraft seat, comprising: a swivel assembly, the swivel assembly comprising: a swivel plate including integrally-formed connecting members, the integrally-formed connecting members configured to couple to a portion of the aircraft seat; and a swivel mechanism configured to rotate the aircraft seat about a central axis of the aircraft seat; a tracking assembly, the tracking assembly comprising: a plurality of slide tubes configured to slide the aircraft seat one of side-to-side or fore-and-aft; a plurality of slide bearings configured to receive a portion of the plurality of slide tubes; and a tracking plate coupled to the plurality of slide bearings; and an actuation assembly, the actuation assembly comprising: an actuator configured to provide a vertical height adjustment for the aircraft seat, the actuator configured to arrest relative motion between a base assembly (212, 312) of the aircraft seat and an upper portion of the aircraft seat; a release mechanism, the release mechanism configured to couple to a rotatory portion of the swivel plate, the release mechanism configured to release the actuator; a plurality of vertical stabilizer rods coupled to a portion of the tracking plate; and a pillow block assembly, the pillow block assembly comprising: a plurality of pillow blocks coupled to a portion of the swivel plate; and a plurality of rollers coupled to a portion of the plurality of pillow blocks, the plurality of rollers configured to receive a portion of the plurality of stabilizer rods, the plurality of rollers configured to provide stability along the vertical stabilizer rods when the actuator provides the vertical height adjustment. a swivel assembly, the swivel assembly comprising: a swivel plate including integrally-formed connecting members, the integrally-formed connecting members configured to couple to a portion of the aircraft seat; and a swivel mechanism configured to rotate the aircraft seat about a central axis of the aircraft seat; a swivel plate including integrally-formed connecting members, the integrally-formed connecting members configured to couple to a portion of the aircraft seat; and a swivel mechanism configured to rotate the aircraft seat about a central axis of the aircraft seat; a tracking assembly, the tracking assembly comprising: a plurality of slide tubes configured to slide the aircraft seat one of side-to-side or fore-and-aft; a plurality of slide bearings configured to receive a portion of the plurality of slide tubes; and a tracking plate coupled to the plurality of slide bearings; and a plurality of slide tubes configured to slide the aircraft seat one of side-to-side or fore-and-aft; a plurality of slide bearings configured to receive a portion of the plurality of slide tubes; and a tracking plate coupled to the plurality of slide bearings; and an actuation assembly, the actuation assembly comprising: an actuator configured to provide a vertical height adjustment for the aircraft seat, the actuator configured to arrest relative motion between a base assembly (212, 312) of the aircraft seat and an upper portion of the aircraft seat; a release mechanism, the release mechanism configured to couple to a rotatory portion of the swivel plate, the release mechanism configured to release the actuator; a plurality of vertical stabilizer rods coupled to a portion of the tracking plate; and a pillow block assembly, the pillow block assembly comprising: a plurality of pillow blocks coupled to a portion of the swivel plate; and a plurality of rollers coupled to a portion of the plurality of pillow blocks, the plurality of rollers configured to receive a portion of the plurality of stabilizer rods, the plurality of rollers configured to provide stability along the vertical stabilizer rods when the actuator provides the vertical height adjustment. an actuator configured to provide a vertical height adjustment for the aircraft seat, the actuator configured to arrest relative motion between a base assembly (212, 312) of the aircraft seat and an upper portion of the aircraft seat; a release mechanism, the release mechanism configured to couple to a rotatory portion of the swivel plate, the release mechanism configured to release the actuator; a plurality of vertical stabilizer rods coupled to a portion of the tracking plate; and a pillow block assembly, the pillow block assembly comprising: a plurality of pillow blocks coupled to a portion of the swivel plate; and a plurality of rollers coupled to a portion of the plurality of pillow blocks, the plurality of rollers configured to receive a portion of the plurality of stabilizer rods, the plurality of rollers configured to provide stability along the vertical stabilizer rods when the actuator provides the vertical height adjustment. a plurality of pillow blocks coupled to a portion of the swivel plate; and a plurality of rollers coupled to a portion of the plurality of pillow blocks, the plurality of rollers configured to receive a portion of the plurality of stabilizer rods, the plurality of rollers configured to provide stability along the vertical stabilizer rods when the actuator provides the vertical height adjustment.