REPLACEMENT AIRCRAFT PARTS COMPONENTS

Brand Owner Address Description
EVOLUTION First Aviation Services Inc. First Floor 15 Riverside Avenue Westport CT 068804214 Replacement aircraft parts and components, namely, parts for oxygen masks not for medical use and oxygen safety equipment not for medical use in the nature of oxygen bottles, oxygen cylinders, oxygen regulators and regulator valves and oxygen tanks, and parts for power supplies, namely, proprietary rechargeable battery cells; Replacement aircraft parts and components, namely, parts for aircraft lighting, namely, transformers, flash tubes, capacitors, insulators being electrical protection devices and electrical switches;Replacement aircraft parts and components, namely, electrical motors not for land vehicles, brushes for electrical motors not for land vehicles, wire harnesses for use with electric motors not for land vehicles, and hydraulic linear actuators and pneumatic linear actuators; landing gear components, namely, hydraulic valve actuators;Replacement aircraft parts and components, namely, bolts, nuts and washers made of metal;Replacement aircraft parts and components, namely, nickel wear sheaths for propellers; wear plates for propeller assemblies; landing gear components, namely, axles, bushings and bearings; replacement and alternative parts for brakes not for land vehicles;
 

Where the owner name is not linked, that owner no longer owns the brand

    
Technical Examples
  1. Methods and apparatuses for supporting aircraft components, including actuators are disclosed. An apparatus in accordance with one embodiment of the invention includes an actuator housing having an actuator receptacle that securely yet releasably receives an actuator. The actuator receptacle can include conformal walls that conform at least in part to the shape of the actuator and can accordingly squeeze the actuator and properly align the actuator. At least one of the actuator walls can further include a projection that is releasably received in a corresponding recess of the actuator. One of both of these features can releasably secure the actuator relative to the aircraft, reducing and/or eliminating the likelihood that the actuator will be misaligned and/or mispositioned relative to the aircraft during installation and/or replacement.