Abstract: Methods are disclosed for replacing expired or unserviceable aircraft emergency slides (“slides”) in an aircraft. The disclosed methods utilize containers that are configured to securely retain both unserviceable slides and serviceable slides at different times in different configurations as installation tools. The container can be placed on an aircraft through the main door of the aircraft, and are further configured to be easily transported within the aircraft from a staging area of the aircraft to a slide installation and removal point at either the main door or an emergency exit door of the aircraft. The containers can be aligned with the installation and removal point to facilitate replacing an unserviceable slide with a new, serviceable slide. The disclosed methods and containers improve personnel safety concerning lifting and handling of the slides, which are heavy.

Abstract: An aircraft wheel hub protector is adapted to engage an aircraft wheel including an aircraft tire on a rim. The aircraft wheel hub protector having two or more cover sections with a protective protrusion and coupling mechanism guide extending from the a first cover section and passing through a bearing race and internal surface within a hub of the rim of the aircraft wheel in such a fashion so as to provide a void within the protective protrusion. The second cover section is engaged with an opposed side of the aircraft wheel from the first cover section. A coupling mechanism passes through the void in the protective protrusion without having contact with the bearing race and internal surfaces within the hub of the rim and coupling the first cover section and securing the aircraft wheel hub protector to the aircraft wheel.

Abstract: An aircraft wheel hub protector is adapted to engage an aircraft wheel including an aircraft tire on a rim. The aircraft wheel hub protector having two or more cover sections with a protective protrusion and coupling mechanism guide extending from the a first cover section and passing through a bearing race and internal surface within a hub of the rim of the aircraft wheel in such a fashion so as to provide a void within the protective protrusion. The second cover section is engaged with an opposed side of the aircraft wheel from the first cover section. A coupling mechanism passes through the void in the protective protrusion without having contact with the bearing race and internal surfaces within the hub of the rim and coupling the first cover section and securing the aircraft wheel hub protector to the aircraft wheel.

Abstract: Containers and methods are disclosed for replacing expired or unserviceable aircraft emergency slides (“slides”) in an aircraft. The disclosed containers are configured to securely retain both unserviceable slides and serviceable slides. The containers can be placed on an aircraft through the main door of the aircraft, and are further configured to be easily transported within the aircraft from a staging area of the aircraft to a slide installation and removal point at either the main door or an emergency exit door of the aircraft. The containers can be aligned with the installation and removal point to facilitate replacing an unserviceable slide with a new, serviceable slide. The disclosed containers and methods improve personnel safety concerning lifting and handling of the slides, which are heavy.

Abstract: An aircraft wheel hub protector is adapted to engage an aircraft wheel including an aircraft tire on a rim. The aircraft wheel hub protector having two or more cover sections with a protective protrusion and coupling mechanism guide extending from the a first cover section and passing through a bearing race and internal surface within a hub of the rim of the aircraft wheel in such a fashion so as to provide a void within the protective protrusion. The second cover section is engaged with an opposed side of the aircraft wheel from the first cover section. A coupling mechanism passes through the void in the protective protrusion without having contact with the bearing race and internal surfaces within the hub of the rim and coupling the first cover section and securing the aircraft wheel hub protector to the aircraft wheel.

Abstract: An aircraft brake assembly container having a base or container portion with feet extending therefrom. A further base portion is provided and mounted atop the base portion. A spacing is provided between the base and further base portions and this spacing is filled by a spacing container portion or member. The spacing container portion allows for lower profile base and further base portions while accommodating larger diameter new and used brake assemblies. A method of using same is also provided.

Abstract: An aircraft brake assembly container having a base or container portion with feet extending therefrom. A further base portion is provided and mounted atop the base portion. A spacing is provided between the base and further base portions and this spacing is filled by a spacing container portion or member. The spacing container portion allows for lower profile base and further base portions while accommodating larger diameter new and used brake assemblies. A method of using same is also provided.

Abstract: An aircraft brake assembly container having a base or container portion with feet extending therefrom. A further base portion is provided and mounted atop the base portion. A spacing is provided between the base and further base portions and this spacing is filled by a spacing container portion or member. The spacing container portion allows for lower profile base and further base portions while accommodating larger diameter new and used brake assemblies. A method of using same is also provided.

Abstract: Containers and methods are disclosed for replacing expired or unserviceable aircraft emergency slides (“slides”) in an aircraft. The disclosed containers are configured to securely retain both unserviceable slides and serviceable slides. The containers can be placed on an aircraft through the main door of the aircraft, and are further configured to be easily transported within the aircraft from a staging area of the aircraft to a slide installation and removal point at either the main door or an emergency exit door of the aircraft. The containers can be aligned with the installation and removal point to facilitate replacing an unserviceable slide with a new, serviceable slide. The disclosed containers and methods improve personnel safety concerning lifting and handling of the slides, which are heavy.

Abstract: A method for using an aircraft brake assembly in servicing an aircraft, with the container having at least two identical container portions, at least one of the at least two container portions having an at least one sliding channel therein, an at least one cradle member having an at least one sliding portion engaging with said at least one sliding channel holding the cargo in a horizontal orientation, and at least one securement device securing the at least two identical container portions.

Abstract: An aircraft brake assembly container and a method for using an aircraft brake assembly in servicing an aircraft, with the container having at least two identical container portions, at least one of the at least two container portions having an at least one sliding channel therein, an at least one cradle member having an at least one sliding portion engaging with the at least one sliding channel, and at least one securement device securing the at least two identical container portions.

Abstract: A container suitable for storing and transporting hazardous materials such as alkali wet cell batteries in an aviation environment includes a container body and a hinged lid made of cross linked polyethylene, latches, and a triple tongue-in-groove seal around the rim of the container opening. The triple tongue-in-groove seal includes two smaller tongue-in-groove seals with a larger tongue-in-groove seal disposed therebetween. The larger tongue-in-groove structure provides structural strength to help prevent the lid from skewing when the container suffers stress such as an impact at a corner, and also helps to guide the lid and base into proper alignment when the lid is being closed. The smaller tongue-in-groove seals provide double redundant sealing to help contain hazardous materials inside the container without making the rim of the container excessively wide.

Abstract: A container suitable for storing and transporting hazardous materials such as alkali wet cell batteries in an aviation environment includes a container body and a hinged lid made of cross linked polyethylene, latches, and a triple tongue-in-groove seal around the rim of the container opening. The triple tongue-in-groove seal includes two smaller tongue-in-groove seals with a larger tongue-in-groove seal disposed therebetween. The larger tongue-in-groove structure provides structural strength to help prevent the lid from skewing when the container suffers stress such as an impact at a corner, and also helps to guide the lid and base into proper alignment when the lid is being closed. The smaller tongue-in-groove seals provide double redundant sealing to help contain hazardous materials inside the container without making the rim of the container excessively wide.

Abstract: A universal airplane jet engine turbine blade packing case assembly for securely holding a matched turbine blade pair of various shapes, sizes, and profiles for safe shipping and storage includes a molded housing having a base and a hinged lid, with the housing being partitioned into two sections, one section for each turbine blade. Each section includes a dial rotatably affixed to the inside of the base, with a tapered slot in the dial for slidably receiving and engaging a turbine blade root when the slot is in a vertical loading position. When the root has been slid into the dial, rotating the turbine blade causes the dial to also rotate, which causes the slot opening to rotate behind a portion of the housing such that the turbine root is now positively held within the dial. The turbine blade and dial are rotated further until the turbine blade chord is aligned vertically in a stow position.