N20130 accident

NTSB CEN11CA022 · 2010-10-16 · Englewood, CO · near APA

Docket — crew, injuries and powerplant

Summary

The student pilot was landing the helicopter in a field on his third solo landing of the day. During landing, the helicopter began to yaw and he added engine power in an attempt to correct. The helicopter began to spin and after two to three 360-degree rotations, the student pilot reduced collective input and reduced the engine throttle in an attempt to perform an autorotation from a hover. The helicopter landed hard and came to rest in an upright position. The helicopter’s fuselage sustained structural damage during the mishap. The student pilot reported no malfunctions or defects with the helicopter.

Full narrative

The student pilot, with approximately four hours of solo flight time, was landing the single-engine helicopter in a field. On his third solo landing of the day the helicopter began to yaw. As the student pilot added engine power in an attempt to correct for the yaw, the helicopter started to spin. After two to three 360 degree rotations, the student pilot reduced collective input and rolled off the engine throttle to attempt a hovering auto landing. The helicopter landed hard and came to rest in an upright position. The student pilot shut down the helicopter and was able to exit unassisted. The helicopter’s fuselage sustained structural damage during the mishap. No malfunctions or defects with the helicopter’s controls or other systems were reported.

Probable cause

The student pilot’s failure to maintain directional control of the helicopter during landing. 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
Sky condition
NONE
Ceiling (ft)
0
Visibility (sm)
10
Wind direction
360
Wind speed (kt)
5
Temperature (F)
54
Nearest airport
Centennial Airport
Distance from field
0.0
Airport elevation
5885

Aircraft

RegistrationMakeModelDamageFAR part
N20130 — — SUBS 091

Sequence of events

#OccurrencePhase
1 Landing-flare/touchdown Loss of control in flight defining Cruise
2 Landing Hard landing Cruise

Findings

Finding
Personnel issues-Task performance-Use of equip/info-Aircraft control-Student pilot cause
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained cause