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December 1, 2007 · Bell 206-L4 · N95CH

Talladega, AL

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 1, 2007
Injury Outcomes
No injuries (4 uninjured)
Location
Talladega, AL
Aircraft
Bell 206-L4
Tail Number
N95CH
Injuries
None
Aircraft Damage
Substantial
NTSB Number
NYC08LA050

The pilot performed an off-airport landing in the helicopter, to pick up a patient for transport to a nearby hospital. During the subsequent takeoff, the helicopter's tail rotor struck a wire that was located about 30 feet above the ground, oriented perpendicular to its flight path. The pilot immediately landed without further incident. Neither the pilot, nor the crew were previously informed of the wire, which was not observed until just prior to contact. The helicopter sustained damage to the tail rotor, vertical stabilizer, and left aft storage compartment door.

NTSB Probable Cause

The pilot's inadequate visual lookout, which resulted in an in-flight collision with a wire.

Full Narrative

On December 1, 2007, about 1310 central standard time, a Bell 206-L4 helicopter, N95CH, was substantially damaged when it struck a wire during takeoff from a field in Talladega, Alabama. The certificated commercial pilot, two crew members, and a passenger were not injured. Visual meteorological conditions prevailed and a company visual flight rules flight plan was filed for the planned flight to a hospital in Ironton, Alabama. The air ambulance flight was conducted under 14 Code of Federal Regulations Part 135. According to the operator, the flight previously departed from Anniston, Alabama, and the pilot performed an off-airport landing to pick up a patient for transport to a nearby hospital. During the subsequent takeoff, the helicopter's tail rotor struck a wire that was located about 30 feet above the ground, oriented perpendicular to its flight path. The pilot immediately landed without further incident. Neither the pilot, nor the crew were previously informed of the wire, which was not observed until just prior to contact. The helicopter sustained damage to the tail rotor, vertical stabilizer, and left aft storage compartment door. The pilot did not report any mechanical problems with the helicopter. He reported 11,166 hours of total rotorcraft flight experience, which included 480 hours in the same make and model as the accident helicopter.

Flight

Event TypeAccident
Event Time13:10 CST
Nearest Airport0nm
Flight Plan FiledCvfr
Flight Plan ActivatedYes
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206-L4
Tail NumberN95CH
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsRolls-Royce · 250-C30P · Turboshaft · 600
Seats4

People & Injuries

Injury SummaryNo injuries (4 uninjured)
Fatal0
Serious0
Minor0
Uninjured4
Total4
Crew 1Age 61 · Second Class · None

Conditions

ConditionsVMC
LightDaylight
Wind130° @ 7 kt
Visibility9 sm
CeilingNone
Temperature / Dew Point66 F / 34 C
Altimeter30.28 inHg
Observation Time18:53
Weather SourceWFAC

Appendix: Source Data