Ami Industries, Inc.

Goodrich Corporation

Kyle David Doughty

Rob Jacobson

Rajesh A Shinde

Douglas E Hoover

Keith Michael Ferguson

Jason Michael Sharpe

Rajesh Shinde

An armrest for a seat may comprise paneling and an easy hook assembly. The easy hook assembly may include a flange and a keyhole protrusion. The flange and the keyhole protrusion may each extending beyond an exterior surface of the paneling. The flange and the keyhole protrusion may allow the armrest to be installed after the paneling is attached.

Easy hook armrest assembly for aircraft seat

A system may include a seat assembly. The seat assembly may include a seat base, a seat portion mounted to the seat base, and an armrest assembly configured to be in an up position or a down position. The armrest assembly may include a handle operable by a user to lock or unlock at least one functionality of at least one adjustable seat assembly feature. Operation of the handle may be configured at least to: unlock the at least one functionality of at least one adjustable seat assembly feature while locking the armrest assembly from moving between the up position and the down position.

Seat assembly and system

A multi-function lever actuation system includes a control lever having a neutral position and configured to be actuated in a clockwise direction and in a counterclockwise direction. The system further includes a bell crank coupled to the control lever and configured to rotate in an opposite direction from the control lever and to actuate a first controlled component in response to a first rotation of the control lever in a first direction corresponding to the clockwise direction or the counterclockwise direction. The system further includes a first cable coupled to the control lever and configured to actuate a second controlled component in response to a rotation of the control lever in a second direction corresponding to the other of the clockwise direction or the counterclockwise direction.

Short multiple function rotary actuator lever

A track fitting for securing a seat pedestal of an aircraft seat to a floor of an aircraft may comprise a strut and a lock assembly. The strut may include an aft section configured to attach to an aft foot of the seat pedestal, a forward section configured to attach to a forward foot of the seat pedestal, and a central section extending between the aft section and the forward section. The lock assembly may be located proximate the aft section of the strut.

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Colorado Springs, CO, United States of America

Kyle David Doughty