Incident Overview
During an aerial application operation, a helicopter sustained a main rotor system hub failure. The pilot in command (PIC) reported that the complete rotor head, blades, and paddles had just been reinstalled. After a flight of less than one mile, the failure occurred, rendering the PIC unable to control the aircraft. An uncontrolled descent followed, and the helicopter struck the terrain.
Damage and Injuries
The helicopter was substantially damaged. The PIC suffered minor injuries.
Pilot Statement
The PIC stated that the linkage pin that goes through the mast and pitch change mechanism was not aligned, causing the failure.
Conclusion
The investigation determined that the main rotor hub failure resulted from a misaligned linkage pin. No other causal factors were identified.