N288JS

Destroyed
Fatal

SHARP SCORPION TOO S/N: SH-1

Accident Details

Date
Thursday, June 2, 1994
NTSB Number
LAX94LA236
Location
BECKWOURTH, CA
Event ID
20001206X01556
Coordinates
39.790317, -120.460906
Aircraft Damage
Destroyed
Highest Injury
Fatal
Fatalities
1
Serious Injuries
0
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

the failure of the tail rotor 'V' drive belt for undetermined reasons and the subsequent failure and separation of the tail rotor.

Aircraft Information

Registration
N288JS
Make
SHARP
Serial Number
SH-1
Engine Type
Reciprocating
Year Built
1987
Model / ICAO
SCORPION TOO BPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SHARP JIM
Address
6701 GRAYS CT
Status
Deregistered
City
SOMERSET
State / Zip Code
CA 95684
Country
United States

Analysis

On June 2, 1994, about 1300 Pacific daylight time, a homebuilt experimental Sharp Scorpion Too helicopter, N288JS, sustained an in-flight separation of the tail rotor system and crashed about 1 mile west of Beckwourth, California. The helicopter was built, owned, and operated by the pilot. Visual meteorological conditions prevailed at the time and no flight plan was filed for the operation. The helicopter was destroyed in the accident sequence. The private pilot, the sole occupant, sustained fatal injuries. The flight originated from the Beckwourth airport on the day of the accident about 1230 as a presumed local area personal flight.

Ground witnesses reported that the helicopter departed from the Beckwourth airport and was cruising about 200 feet agl when popping sounds were heard. The witnesses observed parts come off the helicopter, then it descended rapidly to ground impact. Information from individuals on the airport indicated this was the third flight of the day and that the builder/pilot may have been performing test flights.

A Federal Aviation Administration (FAA) inspector from the Reno, Nevada, Flight Standards District Office responded to the accident site and examined the wreckage. He reported that the tail rotor assembly was found about 90 yards from the main wreckage along with portions of a 'V' drive belt, apparently used to power the tail rotor. Color transfers similar to the drive belt material were found on the blades. The inspector was unable to determine the mode of failure of the drive belt.

According to FAA records, the pilot held a private pilot certificate with an airplane single-engine land rating. The pilot did not hold a rotorcraft category rating and no evidence was found of a solo endorsement for helicopters. The last medical certificate issued to the pilot was dated March 8, 1988. No information was available concerning the last periodic inspection performed on the helicopter. FAA records disclosed that the helicopter was first issued an experimental airworthiness certificate in the amateur built category on December 27, 1987. The helicopter reportedly had accrued a total time of 66 hours.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# LAX94LA236