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Aviation safety reports, made easier to study

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NTSB Report

July 8, 1999 · Bell 206B · N47122

Deadhorse, AK

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
July 8, 1999
Injury Outcomes
No injuries (4 uninjured)
Location
Deadhorse, AK
Aircraft
Bell 206B
Tail Number
N47122
Operator
U S Bureau of Land Management
Injuries
None
Aircraft Damage
Substantial
NTSB Number
ANC99TA090

The pilot for an on-demand helicopter company was beginning a flight that was being operated as a visual flight rules (VFR) U.S. Government flight by the U.S Department of Interior, Bureau of Land Management. The pilot loaded his passengers into the helicopter at a remote biological survey site. He then began an engine start, but a main rotor blade tie-down strap was still attached to one of the rotor blades. As the rotor blades began to turn, the strap struck the upper end of the vertical stabilizer, crushing the leading edge in an aft direction. The helicopter's tail boom was deformed and wrinkled, just forward of the tail rotor gear box.

NTSB Probable Cause

A failure of the pilot-in-command to perform an adequate preflight inspection, and remove a rotor blade tie-down strap.

Full Narrative

On July 8, 1999, about 1230 Alaska daylight time, a Bell 206B helicopter, N47122, sustained substantial damage during engine start-up, about 75 miles southwest of Deadhorse, Alaska. The helicopter was being operated as a visual flight rules (VFR) U.S. Government flight by the U.S Department of Interior, Bureau of Land Management, Fairbanks, Alaska, when the accident occurred. The helicopter, provided by Tundra Copters Inc., Fairbanks, Alaska, was utilized on an on-demand 14 CFR Part 135 flight. The certificated commercial pilot, and the three passengers, were not injured. Visual meteorological conditions prevailed. VFR company flight following procedures were in effect. During a telephone conversation with the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), on July 8, 1999, the director of operations for Tundra Copters Inc., reported the pilot loaded his passengers into the helicopter at a remote biological survey site. The pilot then began an engine start, but a main rotor blade tie-down strap was still attached to one of the rotor blades. As the rotor blades began to turn, the strap struck the upper end of the vertical stabilizer, crushing the leading edge in an aft direction. The helicopter's tail boom was deformed and wrinkled, just forward of the tail rotor gear box.

Flight

Event TypeAccident
Event Time12:30 AKDT
Nearest Airport0nm
Runway0
Flight Plan FiledCvfr
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBell 206B
Tail NumberN47122
Aircraft CategoryHeli
DamageSubstantial
OperatorU S Bureau of Land Management
Operating RulePart 135
Engines1
Engine TypeTurboshaft
Engine DetailsAllison · C20B · Turboshaft · 420
Seats5

People & Injuries

Injury SummaryNo injuries (4 uninjured)
Fatal0
Serious0
Minor0
Uninjured4
Total4
Crew 1Age 51 · Second Class

Conditions

ConditionsVMC
LightDaylight
Wind40° @ 3 kt
Visibility20 sm
CeilingNone
Temperature / Dew Point70 F / 0 C
Altimeter29.00 inHg
Weather SourcePILO

Appendix: Source Data