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August 12, 2006 · Bell 206L-1 · N601GM

Ozona, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
August 12, 2006
Injury Outcomes
No injuries (1 uninjured)
Location
Ozona, TX
Aircraft
Bell 206L-1
Tail Number
N601GM
Operator
Silver State Helicopters
Injuries
None
Aircraft Damage
Substantial
NTSB Number
DFW06LA197

The operator reported that the helicopter was in the area performing long-line external load operations in support of seismic activities. After landing on an uphill rocky slope, the pilot rolled the throttle to idle and checked the control for stability of the landing surface. The 1,263-hour commercial pilot, who reported having accumulated a total of 48 hours in the same make and model, then exited the helicopter in an attempt to re-hook another external load bag. While the pilot was outside the helicopter, the aircraft began to slide backwards and the pilot attempted to compensate by pushing down on the toe of the landing gear skid to stop the slide. The helicopter continued to slide until the tail rotor blades made contact with a large rock outcrop. The pilot subsequently entered the helicopter and retarded the engine. The tail rotor gear box and the aft portion of the tailboom separated from the tailboom. Both tail rotor blades sustained structural damage; however, they remained attached to the tail rotor gear box. The helicopter remained in the upright position and there was no fire. The pilot reported that at the time of the mishap, the weather was clear, with winds from the southeast at 10 to 15 knots, and a temperature of 90 degrees Fahrenheit.

NTSB Probable Cause

The pilot's selection of an unsuitable terrain for landing. A contributing factor was the lack of suitable terrain.

Full Narrative

On August 12, 2006, at 1830 central daylight time, a single-engine Bell 206L-1 helicopter, N601GM, was substantially damaged while landing near Ozona, Texas. The commercial pilot, sole occupant of the helicopter, was not injured. The helicopter was registered to Vista Helicopter Services, Inc., of North Las Vegas, Nevada, and was being operated by Silver State helicopters, also of North Las Vegas, Nevada. Visual meteorological conditions prevailed for the 14 Code of Federal Regulations Part 133 flight. A flight plan was not filed for the external load flight. The local flight originated from a nearby ranch at time unknown. The operator reported that the helicopter was in the area performing long-line (100-foot) external load operations in support of seismic activities. After landing on a uphill rocky slope, the pilot rolled the throttle to idle, friction the controls and checked the control for stability of the landing surface. The 1,263-hour commercial, who reported having accumulated a total of 48 hours in the same make and model, then exited the helicopter in an attempt to hook-up another external load bag. While the pilot was outside the running helicopter, the aircraft began to slide backwards and the pilot attempted to compensate by stepping on the toe of the landing gear skid to stop the slide. The helicopter continued to slide until the tail rotor blades made contact with a large rock outcrop. The pilot subsequently entered the helicopter, shut down the engine, and applied the rotor brake to bring the main rotors to a stop. The operator reported that the tail rotor gear box and the aft portion of the tailboom separated from the tailboom. Both tail rotor blades sustained structural damage; however, they remained attached to the tail rotor gear box. The main rotor blades were not damaged. The helicopter remained in the upright position and there was no fire. The pilot reported that at the time of the mishap, the weather was clear, with winds from the southeast at 10 to 15 knots, and a temperature of 90 degrees Fahrenheit.

Flight

Event TypeAccident
Event Time18:30 CDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedNo
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206L-1
Tail NumberN601GM
Aircraft CategoryHeli
DamageSubstantial
OperatorSilver State Helicopters
Operating RulePart 133
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · 250-C28B · Turboshaft · 435
Seats4

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 30 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind135° @ 12 kt
Visibility10 sm
CeilingNone
Altimeter0
Weather SourcePILO

Appendix: Source Data