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NTSB Report

December 23, 2006 · Belcher Helicycle · N6912B

Boulder City, NV

Overview

Report Status
Final with probable cause
Event Type
Accident
Date
December 23, 2006
Injury Outcomes
No injuries (1 uninjured)
Location
Boulder City, NV
Aircraft
Belcher Helicycle
Tail Number
N6912B
Injuries
None
Aircraft Damage
Substantial
NTSB Number
LAX07CA063

The amateur-built experimental helicopter landed hard following a loss of engine power while in a 6-foot hover. The pilot said the helicopter was equipped with a 150-horsepower turbo shaft engine. The engine was originally developed for a military application and the manufacturer has since introduced it for sale to amateur builders. The pilot reported that he was in a hover 6 feet above the taxiway after landing when the engine lost power. He attempted a hovering autorotation; however, the helicopter landed hard. He examined the engine and related systems. He said the loss of power was due to a fractured and separated solid fuel line that went from the fuel manifold to one of the injectors. He stated that the crack was near a joint in the line and appeared to be from fatigue.

NTSB Probable Cause

a loss of engine power due to a fractured fuel line.

Full Narrative

On December 23, 2006, at 1245 Pacific standard time, a Belcher Helicycle, N6912B, an amateur-built experimental helicopter, landed hard following a loss of engine power while in a hover at 6 feet above ground level (agl) at the Boulder City, Nevada, airport. The helicopter was owned and operated by the pilot under the provisions of 14 CFR Part 91 of the Federal Aviation Regulations. The helicopter sustained substantial damage to the tail boom, vertical stabilizer, and skids and skid attach points. The private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the local area personal flight that originated at Jean, Nevada, at 1210, destined for Boulder City. The pilot said the helicopter was equipped with a Solar T62-32, a 150-horsepower turbo shaft engine. The engine was originally developed for a military application and the manufacturer has since introduced it for sale to amateur builders. The pilot reported that he was in a hover 6 feet above the taxiway when the engine lost power. He attempted a hovering autorotation; however, the helicopter landed hard. He examined the engine and related systems. He said the loss of power was due to a fractured and separated solid fuel line that went from the fuel manifold to one of the injectors. He stated that the crack was near a joint in the line and appeared to be from fatigue.

Flight

Event TypeAccident
Event Time12:45 PST
Nearest AirportBoulder City Municipal (0nm)
Runway9R
Runway Length4800 ft
Runway Width75 ft
Flight Plan FiledNone
Aircraft FireNo
Aircraft ExplosionNo

Aircraft

AircraftBelcher Helicycle
Tail NumberN6912B
Aircraft CategoryHeli
DamageSubstantial
Operating RulePart 91
Engines1
Engine TypeTurboshaft
Engine DetailsSolar · T-62-32 · Turboshaft · 150
Seats1

People & Injuries

Injury SummaryNo injuries (1 uninjured)
Fatal0
Serious0
Minor0
Uninjured1
Total1
Crew 1Age 37 · Third Class · None

Conditions

ConditionsVMC
LightDaylight
Wind4 kt
Visibility10 sm
CeilingNone
Temperature / Dew Point52 / 12 C
Altimeter30.34 inHg
Observation Time20:56
Weather SourceWFAC

Appendix: Source Data