Aviation Crash Map

Buschmann Robert E HELICYCLE N3375C

19 July 2008 · Stuart, Florida, United States · Minor injuries

Summary

On 19 July 2008 at about 15:15 local time, a Buschmann Robert E HELICYCLE registered N3375C, operated by R & J Enterprises of North Carolina Inc, was involved in an accident near Stuart, Florida, United States. One person was on board and one had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 15:15
Classification
Accident
Location
Stuart, Florida, United States
Nearest airport
Witham Field (SUA)
Coordinates
27.1817, -80.2217
Aircraft
Buschmann Robert E HELICYCLE
Registration
N3375C
Category
Helicopter
Engines
1
Operator
R & J Enterprises of North Carolina Inc
Operating rule
Part 91: General Aviation
Purpose of flight
Personal
Phase of flight
Not recorded
Route
Lantana → Stuart
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
NYC08CA252

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
1 0 0 1 0

Probable cause

The pilot's improper decision to take off with a known discrepancy. Contributing to the accident was spilled fuel on the drive belts.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

According to the student pilot of the amateur-built helicycle, he made an uneventful approach to a taxiway with a calm wind. About 1 foot above the ground, the nose started yawing to the right. The pilot applied left rudder to no effect, but was able to land the helicopter without incident. All instrument readings were normal and there were no unusual vibrations. Then, in an effort to move the helicopter from the taxiway, the pilot entered into a hover and applied right pedal to turn. The pilot continued raising the collective, and applied left pedal to stop the right turn; however, the helicopter would not stop turning. After the pilot lowered the collective the right skid hit the ground and collapsed, the rotor blades impacted the ground, and the lower portion of the vertical stabilizer was bent. The pilot subsequently determined that a fuel spill on the helicopter's drive belts resulted in a loss of tail rotor effectiveness.

Quoted verbatim from the NTSB record.

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