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Category | Toy |
---|---|
Material | Plastic |
Batteries Required | No |
Color | Multicolor |
Age Range | 3+ |
Explains the Cyclic/Collective Pitch Mixing system and its advantages for helicopter control.
Highlights that the product is not a toy and warns of potential damage or harm from misuse.
Details the assembly of the main drive gear and autorotation mechanism.
Guides the installation of the main drive gear assembly onto the main rotor shaft.
Explains the process of mounting the engine and ensuring proper alignment.
Guides the assembly of the main rotor head hub component.
Details the assembly of the main blade holders and their bearings.
Explains how to adjust the swashplate to ensure it is level.
Guides the connection of the swashplate and washout assembly.
Details the final installation steps for the main rotor head assembly.
Guides the assembly of the tail output shaft and pulley.
Details the assembly of the tail gear case and its components.
Guides the mounting of the servos onto the helicopter frame.
Guides the installation of the gyro, receiver, switch harness, and battery pack.
Explains the 120° 3-servo CCPM system, its precision, and reduced complexity.
Provides the setup procedure for JR 10 series radios for CCPM activation.
Details the CCPM activation and setup for JR XP8103/XP8103DT radios.
Provides the CCPM activation and setup procedure for JR XP652 radios.
Stresses the importance of matching servo travel values for swashplate stability.
Emphasizes the critical need for correct servo direction for CCPM synchronization.
Details the correct wiring connections for servos in a CCPM system.
Guides servo arm mounting, centering, and preparation for CCPM setup.
Explains how to fine-tune servo centering using the radio's sub-trim function.
Guides the assembly and connection of CCPM servo linkages to control surfaces.
Details the procedure to check and adjust the swashplate for proper levelness.
Verifies that all servos are operating in the correct direction for flight control.
Explains how to adjust main rotor blade tracking for optimal flight stability.