Abstract: A buffer stop assembly for engagement within cargo aircraft to resist cargo movement. The buffer stop assembly comprises a horizontal member selectively engageable to the aircraft and a substantially vertical member resistant to movement by aircraft cargo. The members are mounted to each other. Preferably the panel mounting allows the vertical member to be moved between an extended position and a transport position overlying the horizontal member.

Abstract: A static line snap comprising an elongated body including a handle portion and an opposing C shaped portion for attachment to an anchor. The attachment portion includes a cavity with a load end and a lock end, and opposing arms defining a slot. A keeper with two gates is movably mounted adjacent the slot. The keeper has a lock position and a load position, with a first gate partitioning the load end from the lock end in the keeper load position and a second gate partitioning the load end from the lock end in the keeper lock position.

Abstract: A device and method of use for opening a container during descent so that objects within the container may be dispersed over a controlled ground area. The device includes a housing with a parachute canopy contained within. A sling is attached to the canopy within the housing and extends external to the housing. A cap is selectively engageable with the housing to close the housing. A spring within the housing exerts outward force on the cap. An actuation device is mounted to the cap to selectively disengage the cap from the housing. When the cap is disengaged from the housing the cap is ejected by the force of the spring. A lanyard connecting the cap to the canopy draws the canopy out of the housing for deployment. Deployment of the canopy transfers tension force through the slings to the container. The tension force imposed on the container by the slings opens the container, releasing objects held therein. The objects are released at a predetermined height.

Abstract: A mechanical dereefer comprises a frame having a housing end with a joining wall and spaced plates extending from the joining wall to define a L shaped bifurcated end. A latch is mounted between the plates for pivotal movement between a capture position, wherein a reefing line end is held, and a release position, wherein the reefing line end is released. The latch is maintained in the capture position by engagement with a latch lock slidable through an aperture in the joining wall to a projected position. The latch lock is maintained against a bias in the projected position by the engagement of an elbow link and a trigger link each pivotally mounted within the frame housing end. The trigger link may be actuated out of engagement with the elbow link either manually or by a trigger device.

Abstract: A low profile latch mechanism for use in existing and new parachute quick release couplings of the type having two nested members. The mechanism uses a U shaped latch connected to a lever. In an overlying position of the lever, the members are retained in the nested condition, preventing release of the coupling. A W-shaped spring biases tabs into engagement with apertures in one of the members. The lever is retained in the overlying position by connection with the W-shaped spring. Disengaging the W-shaped spring allows the lever to be pivoted, moving the U shaped latch to a position whereby the members are free to separate.

Abstract: An ejection seat buckle assembly and an arm restraint system incorporating such a buckle assembly wherein the buckle of the assembly includes latch and strike portions each having a respective cable guide ring integrally formed therewith. Arm restraint cables passing through the guide rings deploy safety nets or pull the sleeves or arms of an occupant inward toward the occupant's torso or lap to prevent arm injury during seat ejection from an aircraft. In one embodiment, the guide rings are formed integrally with the latch and strike portions by forming generally oval shaped openings in lap belt adjusters mounted to respective latch and strike engagement portions by latch hinges. In another embodiment, the cable guide rings are D-shaped rings integral with the latch and strike of the ejection seat buckle.

Abstract: A parachute quick release coupling having overlying and underlying coupling members and a latching mechanism pivotally mounted on a lower upstanding lug of the underlying coupling member to be withdrawn outwardly and downwardly from a normal latching position thereof overlying the upper coupling member to release the coupling and then eject the latching mechanism from the underlying coupling member.