N6331D accident

NTSB ERA13LA308 · 2013-06-29 · Florence, AL

Docket — crew, injuries and powerplant

Summary

The student pilot was attempting to land the helicopter on a trailer in order to transport it to another location. A witness reported that, while the helicopter was hovering above the trailer, it started to drift backwards. Subsequently, the nose of the helicopter rose, the tail struck the ground, the helicopter rolled to the right, the main rotor blades struck the ground, and the helicopter came to rest on the right side of the fuselage, which resulted in substantial damage. A postaccident examination of the helicopter did not reveal any mechanical malfunctions or abnormalities that would have precluded normal operation.

Full narrative

On June 29, 2013, about 1130 central daylight time, a Hiller UH-12A, N6331D, impacted terrain during an attempted landing on a tow trailer near Florence, Alabama. The student pilot was seriously injured. The helicopter was registered to River Cleaning Inc., and operated under the provisions of Title 14 Code of Federal Regulations Part 91, as a positioning flight. Visual meteorological conditions prevailed for the flight and no flight plan was filed. The flight originated from a parking area in the vicinity of the tow trailer just prior to the accident.According to a Federal Aviation Administration (FAA) inspector, who conducted an interview with an eyewitness, the student pilot was attempting to land the helicopter on the trailer in order to transport it to another location. He stated that the helicopter was hovering above the trailer when it started to drift backward. As the helicopter moved back, the nose of the helicopter started to rise and the tail subsequently struck the ground. The helicopter then rolled to the right, the main rotor blades struck the ground, and the helicopter came to rest on the right side of the fuselage, which resulted in substantial damage.

According to the FAA inspector, numerous attempts to interview the pilot were unsuccessful as the pilot has no recollection of the events surrounding the accident and that the pilot's flight experience was about 38 total flight hours. Examination of the helicopter at the accident location revealed that it had come to rest on its right side in the immediate vicinity of the trailer. The helicopter sustained substantial damage to the main rotor blades, skids, and fuselage. No mechanical malfunctions or abnormalities were noted that would have precluded normal operation.

Probable cause

The student pilot’s failure to maintain control of the helicopter while landing, which resulted in a tail rotor ground strike and collision with terrain. The National Transportation Safety Board determined the probable cause of this accident.

Circumstances

Event type
Accident
Highest injury
Serious
Weather conditions
Visual Meteorological Cond
Light condition
Day
Sky condition
NONE
Ceiling (ft)
0
Visibility (sm)
10
Wind direction
320
Wind speed (kt)
9
Temperature (F)
86
Distance from field
0.0

Aircraft

RegistrationMakeModelDamageFAR part
N6331D — — SUBS 091

Sequence of events

#OccurrencePhase
1 Landing-flare/touchdown Tailstrike defining Cruise
2 Landing-flare/touchdown Collision with terr/obj (non-CFIT) Cruise

Findings

Finding
Personnel issues-Task performance-Use of equip/info-Aircraft control-Student pilot cause
Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Student pilot cause
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Incorrect use/operation cause
Personnel issues-Experience/knowledge-Experience/qualifications-Total experience-Student/instructed pilot factor