EMBLA SZM2 Cyclic Yoke - HI0304111 by Hirobo  [HI0304111]

HIROBO 0304-111 EMBLA SZM2 YOKE #0304111
Price:
CAD$28.32
Brand:
Hirobo
Model:
HI0304111
GTIN:
4512895156404
Condition:
Brand New
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EMBLA SZM2 cyclic yoke summary

This replacement yoke is made for the EMBLA SZM2 RC helicopter and links the swashplate outputs to rotor pitch control, directly affecting cyclic response and stick feel.

The text concentrates on fit and setup rather than material claims. During installation confirm alignment and secure attachment points to preserve predictable cyclic geometry. After fitting, carry out trim and endpoint checks to re-establish neutral pitch and balanced control throws.

Fit this part when restoring correct fit on an EMBLA SZM2 airframe or replacing a worn linkage. This item is an accessory component intended for model aircraft use only.

Specifications

  • Item Yoke
  • Material Not specified
  • Model Number HI0304111
  • Compatibility EMBLA SZM2

Compatibility

  • EMBLA SZM2

Choose this yoke to match original fit on EMBLA SZM2 helicopters and be sure to confirm linkage alignment and cyclic centering during final setup.

What installation checks should I perform after fitting this yoke?

After installing the yoke verify swashplate centring, ensure all fasteners are secure, set neutral blade pitch, and run incremental control checks to confirm symmetric throws before flight.

Does the package include mounting hardware?

The listing does not specify included hardware. Inspect the package contents on arrival and have suitable screws and retainers ready if they are not supplied.

How will replacing the yoke alter cyclic feel?

A correctly fitting yoke preserves intended linkage geometry, which helps maintain predictable servo travel, symmetric throws, and consistent cyclic response; incorrect fit can introduce slop or asymmetric control.

Any practical tips for aligning the yoke on the EMBLA SZM2?

Use the swashplate as a reference when setting the linkage, tighten fasteners to spec, check for free rotation without binding, and verify neutral pitch with the servos powered before final flight tests.

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