- 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.
On this page
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.
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.