N534EA

Substantial
Serious

CHRISTOPHER LORD ELA 07 SCORPIONS/N: 04175340734

Accident Details

Date
Monday, May 7, 2018
NTSB Number
ERA18TA144
Location
Sebring, FL
Event ID
20180507X30956
Coordinates
27.448610, -81.343055
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to slow the gyroplane and maintain control while exiting the runway.

Aircraft Information

Registration
Make
CHRISTOPHER LORD
Serial Number
04175340734
Engine Type
Reciprocating
Year Built
2017
Model / ICAO
ELA 07 SCORPION
Aircraft Type
Rotorcraft
No. of Engines
1
Seats
2
FAA Model
ELA 07 SCORPION

Registered Owner (Current)

Name
MICHALEK ZACKERY A
Address
105 CENTENNIAL CIR
City
MYRTLE BEACH
State / Zip Code
SC 29579-4193
Country
United States

Analysis

On May 7, 2018, about 1145 eastern daylight time, an experimental, amateur-built Ela 07 Scorpion gyroplane, N534EA, was substantially damaged during the landing rollout at Sebring Regional Airport (SEF), Sebring, Florida. The student pilot sustained serious injuries. The gyroplane was operated by the student pilot as a personal flight conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed at the time of the accident for the local flight.According to the pilot, he was flying in the pattern practicing takeoffs and landings. After landing on runway 1, during the landing roll, he began a left turn to exit the runway when the gyroplane "tipped" and rolled onto the right side.

According to a witness, after the gyroplane landed on runway 1, the rotor blades still had a "high speed" of rotation. When the aircraft started turning to a taxiway on the left, a main rotor blade struck the runway, the gyroplane spun 180° to the right, and impacted the ground, coming to rest on its right side.

Examination of the gyroplane revealed that one of the main rotor blades impacted the front of the fuselage and a section of the other main rotor blade was impact separated and located about 350 ft from the wreckage. The tail section remained attached to the fuselage. The flight controls were intact, and no binding was noted when they were operated. The pilot reported no preimpact mechanical malfunctions or failures with the gyroplane that would have precluded normal operation.

The pilot did state in the Recommendation Section of the submitted NTSB Pilot/Operator Aircraft Accident/Incident report that the accident might have been prevented by "slow[ing] down while making turns."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ERA18TA144