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June 22, 2005 · Garlick Helicopters OH-58A+ · N372NS

Graham, TX

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
June 22, 2005
Injury Outcomes
1 injury (1 serious injury)
Location
Graham, TX
Aircraft
Garlick Helicopters OH-58A+
Tail Number
N372NS
Operator
Northstar Helicopters
Injuries
Serious
Aircraft Damage
Substantial
NTSB Number
DFW05CA172

After 3 hours of flying, the agricultural helicopter collided with high tension wires and impacted the ground while maneuvering during aerial application of pesticides. The 10,000-hour pilot completed spraying a pasture and was trimming the edges when the helicopter struck the wires during a pull-up maneuver. Evidence at the accident site showed that the tail boom struck the top wire of the high tension string and separated in-flight. After the tail boom separated, the helicopter descended uncontrolled to ground impact. The wires did not have fixed aerial obstruction features (orange balls, etc.) installed.

NTSB Probable Cause

The pilot's failure to maintain clearance with the wire while maneuvering during an aerial application flight. Low altitude flight is a contributing factor.

Full Narrative

On June 22, 2005, approximately 0845 central daylight time, a Garlick Helicopters Inc., OH-58A+ helicopter, N372NS, registered to and operated by Northstar Helicopters, Inc., of Jasper, Texas, collided with high tension wires and impacted the ground while maneuvering during aerial application of pesticides in the vicinity of Graham, Texas. The commercial pilot, sole occupant of the helicopter, was seriously injured. Visual meteorological conditions prevailed throughout the area and a flight plan was not filed for the Title 14 Code of Federal Regulations Part 137 aerial application flight. The local flight originated at 0545 from a nearby private facility. According to the operator, the 10,000-hour pilot had completed spraying a pasture and was trimming the edges when the helicopter struck the wires during a pull-up maneuver. Examination of the helicopter by an FAA inspector, who traveled to the accident site, revealed evidence of tail boom contact with the guide of a high tension string with subsequent in-flight tail boom separation. After the tail boom separated, the helicopter descended uncontrolled to ground impact. The wires were not equipped with fixed aerial obstruction features (orange balls, etc.).

Flight

Event TypeAccident
Event Time08:45 CDT
Nearest Airport0nm
Flight Plan FiledNone
Flight Plan ActivatedUnknown
Aircraft FireNo

Aircraft

AircraftGarlick Helicopters OH-58A+
Tail NumberN372NS
Aircraft CategoryHeli
DamageSubstantial
OperatorNorthstar Helicopters
Operating RulePart 137
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · C20C · Turboshaft · 400
Seats1

People & Injuries

Injury Summary1 injury (1 serious injury)
Fatal0
Serious1
Minor0
Uninjured0
Total1
Crew 1Age 49 · Second Class · Serious

Conditions

ConditionsVMC
LightDaylight
Wind160° @ 3 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point61 F
Altimeter30.13 inHg
Weather SourcePILO

Appendix: Source Data