A mobile drone communication control station which has capabilities of fueling hydrogen or liquid hydrogen drone, communication control for the drone, communication to the remote pilot center and the edge computing system for analyzing the photos taken from the drone.

A mobile drone communication control station which has capabilities of fueling hydrogen or liquid hydrogen drone, communication control for the drone, communication to the remote pilot center and the edge computing system for analyzing the photos taken from the drone.

A method for repairing a part made of composite material includes producing a recessed section by removing the composite material at a damaged area, producing grooves extending on the two faces of the part from edges of the recessed section, producing orifices in the part opening out into the grooves, tree-dimensional weaving of a filling part fiber preforms including a central section having a shape corresponding to the shape of the recessed section and fiber bundles extending from the central section, placing the filling preforms respectively on either face of the part with the fiber bundles in the grooves on the faces of the part and in the orifices such that the fiber bundles open out into the grooves present on the opposite face of the part, impregnating the filling fiber preforms with a precursor resin of a matrix, transforming the resin into a matrix to obtain a filling part.

A service apparatus for use in maintaining a machine including a stator and a rotor is provided. The service apparatus includes a carriage assembly configured to couple to the rotor. The service apparatus is selectively transitionable between a stowed position in which the service apparatus is rotatable with the rotor and an extended position in which the service apparatus is extended toward the stator. The service apparatus also includes at least one maintenance device coupled to the carriage assembly. The at least one maintenance device is operable to perform a maintenance operation on a surface of the stator with the service apparatus in the extended position.

A system and method of documenting condition, repair, and overhaul of aircraft parts. The system and method include searching a database for an electronic file of an aircraft part; creating an electronic file of the aircraft part if the electronic file is not found on the database; generating a maintenance report data package that is linked to the electronic file; capturing, using a camera or a microphone, aircraft part data including a single or plurality of pictures, a video recording, and a voice recording; linking the aircraft part data to the maintenance report data package; and saving an updated version of the electronic file to the database.

A system and method of documenting condition, repair, and overhaul of aircraft parts. The system and method include searching a database for an electronic file of an aircraft part; creating an electronic file of the aircraft part if the electronic file is not found on the database; generating a maintenance report data package that is linked to the electronic file; capturing, using a camera or a microphone, aircraft part data including a single or plurality of pictures, a video recording, and a voice recording; linking the aircraft part data to the maintenance report data package; and saving an updated version of the electronic file to the database.

The device disclosed herein allows a user to maintain the outboard stabilator of a Blackhawk helicopter. The device, which comprises a kit, allows a user to remove damaged outdoor stabilator bushings from a Blackhawk. Upon removal, the device enables a user to install new outdoor stabilator bushings. Additionally, the device allows a user to ream the newly installed outdoor stabilator bushings so that the outboard stabilator may be reinstalled upon the Blackhawk and safely flown.

An easily inspected shaft assembly is provided and includes a shaft, a sleeve receptive of a portion of the shaft and an optically activatable layer including first and second sections disposed on respective exterior surfaces of the shaft and the sleeve, respectively, such that the first and second sections move relative to one another as the shaft and the sleeve move relative to one another.

A turnaround monitoring system and method are configured to monitor a turnaround of an aircraft at an airport. The turnaround monitoring system and method include receiving, by a turnaround analysis control unit, turnaround data regarding the aircraft at the airport, and determining, by the turnaround analysis control unit, a turnaround status of the aircraft based on the turnaround data.

A turnaround monitoring system and method are configured to monitor a turnaround of an aircraft at an airport. The turnaround monitoring system and method include receiving, by a turnaround analysis control unit, turnaround data regarding the aircraft at the airport, and determining, by the turnaround analysis control unit, a turnaround status of the aircraft based on the turnaround data.