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General| Brand | CELIER AVIATION |
|---|---|
| Model | Xenon 2 RST |
| Category | Aircrafts |
| Language | English |
Details the regulatory basis and classification of the gyrocopter as an ultralight aircraft.
Lists key geometric and weight specifications for the gyrocopter.
Introduces the various control systems of the gyrocopter.
Covers procedures for assembling and dismantling the gyrocopter's rotor assembly.
Details the assembly schema and components of the rotor hub.
Provides step-by-step instructions for safely dismantling the rotor assembly.
Describes the process of assembling, aligning, and checking the rotor.
Outlines the procedure for fitting the assembled rotor onto the gyrocopter.
Illustrates the assembly schema and components of the rotor head.
Provides the assembly schema for the gyrocopter's rotor control system.
Details the assembly schema for the directional control system of the gyrocopter.
Outlines the procedure for replacing the master bearing in the rotor head.
Details overhaul intervals based on flight hours (25, 50, 100 hours).
Outlines overhaul intervals based on calendar time (e.g., half-yearly, yearly).
Specifies initial checks and tasks to be performed after the first 10 or 25 flight hours.
Presents a detailed table of tasks for 25, 50, and 100-hour overhauls.
Lists the recommended operational time limits for various structural units and components.
Specifies the design deflection and tilt angles for the rotor head.
