GAA18CA512

NTSB accident investigation · Bell 206 · Battle Mountain, NV · August 18, 2018

Accident · No injuriesClass 4 · Data collectionFinal report
Date
August 18, 2018, 13:45 local (20:45 UTC)
Place
Battle Mountain, NV
Injuries
3 uninjured
Damage
Destroyed
Phase of flight
Maneuvering
Aircraft
N8052GBell 206
Defining event
Maneuvering-low-alt flying: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report March 20, 2020
Report
Approved by Office Director
Investigation class
Class 4 - Basic report with no Prelim publish
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20180818018519A
Case key
98112

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 failure to maintain the proper altitude and airspeed while flying in a canyon in gusting wind conditions.

Findings · 5

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.

Performance/control parameters: altitudeAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell 206B: 20 casesAll aircraft: 1,310 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotBell 206B: 45 casesAll aircraft: 9,295 casesProbable cause
Performance/control parameters: airspeedAircraft › Aircraft oper/perf/capability · Not attained/maintainedBell 206B: 2 casesAll aircraft: 1,681 casesProbable cause
Wind: gustsEnvironmental issues › Conditions/weather/phenomena · Effect on operationBell 206B: 4 casesAll aircraft: 1,199 casesProbable cause
Terrain: mountainous/hilly terrainEnvironmental issues › Physical environment · Effect on operationBell 206B: 4 casesAll aircraft: 329 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 helicopter pilot reported that, while climbing out of a canyon at 30 knots indicated airspeed, about 50 ft above ground level, he felt a "hard vibration" in the cyclic and collective controls. He then saw that the airspeed gauge was reading 0 knots and felt the helicopter being pushed down. The torque indicator rose to 120% without any cyclic or collective control input. He applied right cyclic, lowered the collective, applied right pedal to counter the torque, and turned the helicopter downslope into the wind. He applied forward cyclic to better match the downslope of the terrain and raised the collective, but the skids impacted the ground, followed by the main rotor blades. The helicopter rotated 180º to the right before coming to rest downhill on its right side. Shortly after, a postimpact fire ensued, which destroyed the helicopter. The pilot reported that there were no preaccident mechanical failures or malfunctions with the helicopter that would have precluded normal operation. The pilot reported that the winds were gusting to 30 knots in the canyon and "changing direction every minute or so."

Factual narrative

The helicopter pilot reported that while climbing out of a canyon at 30 knots indicated airspeed, about 50 ft above the ground, he felt a "hard vibration" in the cyclic and collective controls. He then saw that the airspeed gauge was reading zero knots and he felt the helicopter was being pushed down. The torque indicator rose to 120% without any cyclic and collective control input. He applied right cyclic, lowered the collective, applied right pedal to counter the torque, and turned the helicopter downslope and into the wind. He applied forward cyclic to better match the downslope of the terrain and raised collective, but the helicopter impacted terrain. The skids impacted the ground first followed by the main rotor blades. The helicopter rotated 180º to the right before coming to rest downhill, on its right side. Shortly after, a post impact fire ensued. The helicopter was destroyed during the postimpact fire. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation. The pilot reported that the winds were gusting up to 30 knots in the canyon, "changing direction every minute or so."

Aircraft

Registration
N8052G
Reported as
Bell 206 (B)
Category
Helicopter
Serial number
4050
Built
1989
Engine
Rolls Royve 250-C20R, turbo shaft
Damage
Destroyed
Fire
On-Ground
Flight
Aerial observation · Part 91
Operator
El Aero Services Llc
Registered owner
El Aero Services Llc
Airworthiness certificate
Standard, Normal
Departed
BAM · Battle Mountain, NV
Destination
BAM · Battle Mountain, NV
Flight plan
Company VFR
Equipment
Satellite tracking device, Electronic flight bag or handheld 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
43
Injuries
Minor
Certificates
Flight instructor, Commercial
Medical
Class 2, With waivers/limitations
Seat
Front
Restraint
4-point
Flight hours
4,060 total · 1,500 in this make and model · 3,975 as pilot in command

Weather

Conditions
Visual (VMC) · Day
Wind
10° at 8 knots
Visibility
7 statute miles
Lowest ceiling
None
Temperature
90 °F, dew point 16 °F
Altimeter
30.22 inHg
Observed at
KBAM, 11 nm away
METAR
KBAM 182055Z AUTO 01008KT 7SM CLR 32/M09 A3022 RMK AO1

Docket · 2

The files NTSB released with the investigation on December 5, 2019, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.3 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.