N372HS

Substantial
None

EUROCOPTER EC120S/N: 1460

Accident Details

Date
Monday, June 13, 2016
NTSB Number
GAA16CA318
Location
Ajo, AZ
Event ID
20160614X83429
Coordinates
32.129165, -113.485832
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's decision to exit the helicopter with the engine and rotors turning and the selection of unsuitable terrain for a landing, which resulted in a roll over.

Aircraft Information

Registration
Make
EUROCOPTER
Serial Number
1460
Engine Type
Turbo-shaft
Year Built
2007
Model / ICAO
EC120
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
5
FAA Model
EC120B

Registered Owner (Current)

Name
BROWN HELICOPTER INC
Address
10100 AILERON AVE
City
PENSACOLA
State / Zip Code
FL 32506-8223
Country
United States

Analysis

The pilot of a skid equipped helicopter reported that after landing on a volcanic rock hill top, the pilot exited the running helicopter. The pilot further reported that he heard an audible change in the sound of the main rotor and observed the ground under the right skid of the helicopter give way and the helicopter rolled to the right.

The helicopter sustained substantial damage to the tail boom.

According to the pilot there were no preimpact mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation.

The Federal Aviation Administration (FAA) has published FAA-H-8083-21A Helicopter Flying Handbook (2012). This handbook discusses pilots at the flight controls and states in part:

"Many helicopter operators have been lured into a "quick turnaround" ground operation to avoid delays at airport terminals and to minimize stop/start cycles of the engine. As part of this quick turn-around, the pilot might leave the cockpit with the engine and rotors turning. Such an operation can be extremely hazardous if a gust of wind disturbs the rotor disk, or the collective flight control moves causing lift to be generated by the rotor system. Either occurrence may cause the helicopter to roll or pitch, resulting in a rotor blade striking the tail boom or the ground. Good operating procedures dictate that, generally, pilots remain at the flight controls whenever the engine is running and the rotors are turning".

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# GAA16CA318