GAA16CA318

NTSB accident investigation · Eurocopter EC120 · Ajo, AZ · June 13, 2016

Accident · No injuriesData collectionFinal report
Date
June 13, 2016, 11:10 local (18:10 UTC)
Place
Ajo, AZ
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Standing
Aircraft
N372HSEurocopter EC120
Defining event
Standing-engine(s) operating: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report September 12, 2016
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
Department of Homeland Security, FAA
FAA report
20160613010319A
Case key
93390

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

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.

Findings · 4

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotEurocopter EC120B: 3 casesAll aircraft: 9,295 casesProbable cause
Action: incorrect action selectionPersonnel issues › Action/decision · PilotEurocopter EC120B: 1 caseAll aircraft: 397 casesProbable cause
Terrain: sloped/uneven terrainEnvironmental issues › Physical environment · Decision related to conditionEurocopter EC120B: 1 caseAll aircraft: 270 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

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".

Factual narrative

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".

Aircraft

Registration
N372HS
Reported as
Eurocopter EC120 (B)
Category
Helicopter
Serial number
1460
Built
2006
Airframe hours
3,563
Engine
Turbomecca Arrius 2F, 431 horsepower, turbo shaft
Damage
Substantial damage
Flight
Public aircraft - federal · Public use
Operator
Department Of Homeland Security
Registered owner
Department Of Homeland Security
Airworthiness certificate
Standard, Normal
Last inspection
100 hour · June 6, 2016
Departed
NYL · Yuma, AZ
Destination
Ajo, AZ
Flight plan
Company VFR
Equipment
Satellite tracking device

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Pilot
Age
44
Injuries
None
Certificates
Commercial, Flight instructor
Airplane ratings
Single-engine land, Multi-engine land
Instrument ratings
Airplane, Helicopter
Medical
Class 2, Without waivers/limitations
Last flight review
March 1, 2016
Seat
Right
Restraint
4-point
Flight hours
7,184 total · 1,156 in this make and model · 3,300 as pilot in command · 103 in the last 90 days · 29 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
280° at 3 knots
Visibility
10 statute miles
Temperature
88 °F, dew point 41 °F
Altimeter
29.95 inHg
Observed at
KNYL, 64 nm away

Docket · 3

The files NTSB released with the investigation on August 29, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.5 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.