- Date
- July 8, 1999, 12:30 local (20:30 UTC)
- Place
- Deadhorse, AK
- Injuries
- 4 uninjured
- Damage
- Substantial damage
- Phase of flight
- Standing
- Aircraft
- N47122Bell 206B
- Weather
- Visual (VMC) · Day
- Status
- Completed · report November 30, 2000
- Report
- Approved by Office Director
- NTSB office
- Alaska Regional Office
- FAA report
- 19990708008519A
- Case key
- 46774
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
A failure of the pilot-in-command to perform an adequate preflight inspection, and remove a rotor blade tie-down strap.
Sequence of events
NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.
Analysis
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.
Factual 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.
Aircraft
- Registration
- N47122
- Reported as
- Bell 206B
- Category
- Helicopter
- Serial number
- 971
- Airframe hours
- 6,274
- Engine
- Allison C20B, 420 horsepower, turbo shaft
- Damage
- Substantial damage
- Flight
- Part 135
- Operator
- U.S. Bureau Of Land Management
- Registered owner
- Tundra Copters Inc.
- Airworthiness certificate
- Standard, Normal
- Flight plan
- Company VFR
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
- 51
- Certificates
- Flight instructor, Commercial
- Airplane ratings
- Single-engine land, Multi-engine land
- Instrument ratings
- Airplane
- Medical
- Class 2, Valid Medical--w/ waivers/lim
- Seat
- Right
- Flight hours
- 6,500 total · 1,100 in this make and model · 6,000 as pilot in command
Weather
- Conditions
- Visual (VMC) · Day
- Wind
- 40° at 3 knots
- Visibility
- 20 statute miles
- Lowest ceiling
- None
- Temperature
- 70 °F
- Altimeter
- 29.00 inHg
FAA reports on this event · 1
The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.