N90570 Hughes 269C accident

NTSB WPR13CA160 · 2013-03-25 · Rialto, CA · near L67

Docket — crew, injuries and powerplant

Summary

According to the student pilot, while in a hover before departure, he attempted a 360-degree right pedal turn. About 180 degrees into the turn, the rotation speed started to increase. The pilot thought his reaction to the increased rotation speed was not as decisive as it should have been, and the helicopter departing controlled flight. The pilot stated that he did not press on the left pedal; instead, he released pressure on the right pedal. The helicopter came to rest upright after impacting the ground, which resulted in substantial damage to the tail rotor drive shaft and boom. The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Full narrative

According to the student pilot, he reported that while in a hover prior to departure, he attempted a 360-degree right pedal turn. About 180 degrees into the turn, the rotation speed started to increase. The pilot thought his reaction to the increased rotation speed was not as decisive as it should have been, which resulted in the helicopter departing controlled flight. The pilot stated that he did not press on the left pedal; instead he released pressure on the right pedal. The helicopter came to rest upright after impacting the ground, which resulted in substantial damage to the tail rotor drive shaft and boom. The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.

Probable cause

The student pilot’s failure to maintain helicopter control while maneuvering in a hover. The National Transportation Safety Board determined the probable cause of this accident.

Circumstances

Event type
Accident
Highest injury
None
Weather conditions
Visual Meteorological Cond
Light condition
Day
Ceiling (ft)
0
Wind direction
0
Nearest airport
Rialto Municipal Airport
Distance from field
0.0
Airport elevation
1455

Aircraft

RegistrationMakeModelDamageFAR part
N90570 HUGHES 269C SUBS 091

Sequence of events

#OccurrencePhase
1 Maneuvering-hover Loss of control in flight defining Climb
2 Uncontrolled descent Collision with terr/obj (non-CFIT) Descent

Findings

Finding
Personnel issues-Task performance-Use of equip/info-Aircraft control-Student pilot cause