Abstract: A mount assembly for mounting a cabin attendant seat to a support structure may comprise a first strap configured to plastically deform in response to a deflection of the support structure. The first strap may comprise a first perforation, a second perforation, and a third perforation located between the first perforation and the second perforation. The perforations may be configured to allow the strap to plastically deform.

Abstract: A stowable seat for an aircraft may comprise a housing and a backrest support configured to rotate relative to the housing. A locking mechanism comprising a first latch may be coupled to the backrest support. A releasing member may be in operable communication with the first latch. The releasing member may be configured to rotate the first latch relative to the backrest support. The releasing member may be located behind a cushion coupled to the backrest support.

Abstract: A retrofit seat back assembly is disclosed. In various embodiments, the assembly includes a supplemental recline panel having an upper end and a lower end; a pivot member disposed proximate the upper end and configured to pivotally engage a seat back frame of a stowable seat; an actuator disposed proximate the lower end and configured to operably engage the seat back frame and move the supplemental recline panel between a retracted position and a deployed position; and a bias element disposed between the supplemental recline panel and the seat back frame and configured to urge the supplemental recline panel toward the seat back frame.

Abstract: A retrofit seat back assembly is disclosed. In various embodiments, the assembly includes a supplemental recline panel having an upper end and a lower end; a pivot member disposed proximate the upper end and configured to pivotally engage a seat back frame of a stowable seat; an actuator disposed proximate the lower end and configured to operably engage the seat back frame and move the supplemental recline panel between a retracted position and a deployed position; and a bias element disposed between the supplemental recline panel and the seat back frame and configured to urge the supplemental recline panel toward the seat back frame.

Abstract: A mount assembly for mounting a cabin attendant seat to a support structure may comprise a first strap configured to plastically deform in response to a deflection of the support structure. The first strap may comprise a first perforation, a second perforation, and a third perforation located between the first perforation and the second perforation. The perforations may be configured to allow the strap to plastically deform.

Abstract: An inertia reel interface for stowable seats is provided. The inertia reel interface may allow for simple access and replacement of inertia reels during maintenance. The inertia reel interface may comprise an inertia reel beam, a payout tube, and one or more inertia reels coupled to the inertia reel beam. The inertia reel beam may deploy a shoulder harness webbing over the payout tube. The payout tube may pivot to a first access position or a second access position to allow for maintenance of the inertia reel interface components.

Abstract: A stowable seat for an aircraft may comprise a housing and a backrest support configured to rotate relative to the housing. A locking mechanism comprising a first latch may be coupled to the backrest support. A releasing member may be in operable communication with the first latch. The releasing member may be configured to rotate the first latch relative to the backrest support. The releasing member may be located behind a cushion coupled to the backrest support.

Abstract: An inertia reel interface for stowable seats is provided. The inertia reel interface may allow for simple access and replacement of inertia reels during maintenance. The inertia reel interface may comprise an inertia reel beam, a payout tube, and one or more inertia reels coupled to the inertia reel beam. The inertia reel beam may deploy a shoulder harness webbing over the payout tube. The payout tube may pivot to a first access position or a second access position to allow for maintenance of the inertia reel interface components.

Abstract: A stowable seat for an aircraft may comprise a housing and a backrest support configured to rotate relative to the housing. A locking mechanism comprising a first latch may be coupled to the backrest support. A releasing member may be in operable communication with the first latch. The releasing member may be configured to rotate the first latch relative to the backrest support. The releasing member may be located behind a cushion coupled to the backrest support.

Abstract: An inertia reel interface for stowable seats is provided. The inertia reel interface may allow for simple access and replacement of inertia reels during maintenance. The inertia reel interface may comprise an inertia reel beam, a payout tube, and one or more inertia reels coupled to the inertia reel beam. The inertia reel beam may deploy a shoulder harness webbing over the payout tube. The payout tube may pivot to a first access position or a second access position to allow for maintenance of the inertia reel interface components.

Abstract: A stowable seat for an aircraft may comprise a housing and a backrest support configured to rotate relative to the housing. A locking mechanism comprising a first latch may be coupled to the backrest support. A releasing member may be in operable communication with the first latch. The releasing member may be configured to rotate the first latch relative to the backrest support. The releasing member may be located behind a cushion coupled to the backrest support.

Abstract: An inertia reel interface for stowable seats is provided. The inertia reel interface may allow for simple access and replacement of inertia reels during maintenance. The inertia reel interface may comprise an inertia reel beam, a payout tube, and one or more inertia reels coupled to the inertia reel beam. The inertia reel beam may deploy a shoulder harness webbing over the payout tube. The payout tube may pivot to a first access position or a second access position to allow for maintenance of the inertia reel interface components.