N142NV

Substantial
None

Gerald Dan Coppock Bade-ES/N: GDC1

Accident Details

Date
Thursday, August 2, 2018
NTSB Number
CEN18LA307
Location
Escanaba, MI
Event ID
20180802X95630
Coordinates
45.722778, -87.093612
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of control during the landing rollout for reasons that could not be determined based on the available evidence, which resulted in a ground loop and runway excursion.

Aircraft Information

Registration
Make
GERALD DAN COPPOCK
Serial Number
GDC1
Engine Type
Reciprocating
Year Built
2014
Model / ICAO
Bade-EBPAT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
BABE-E

Registered Owner (Current)

Name
COPPOCK GERALD D
Address
4101 AIRPORT RD
City
ESCANABA
State / Zip Code
MI 49829-1097
Country
United States

Analysis

On August 02, 2018, about 1900 eastern daylight time, a Gerald Dan Coppock BABE-E homebuilt experimental airplane, N142NV, registered to the pilot/builder, sustained substantial damage during a runway excursion following a loss of directional control while landing at the Delta County Airport (ESC), Escanaba, Michigan. The pilot was not injured. Visual meteorological conditions prevailed and a flight plan was not filed. The local personal flight was being conducted under the provisions of Title 14 Federal Code of Regulations Part 91. The flight originated from ESC about 1830.

According to the pilot, he was landing on runway 01 at ESC and the airplane touched down normally. During the rollout, the airplane veered to the left once the tailwheel contacted the runway. Both wingtips contacted the runway surface and the airplane ground-looped. The forward section of the fuselage was buckled upward and substantially damaged. The airplane came to rest, nose down and the pilot exited the airplane. According to ESC METAR weather, reported winds about the time of the accident were 330 at 5 knots.

Inspection of the airplane after the accident revealed that the right steering cable chain was broken and hanging from the tailwheel. It could not be determined if the cable break was caused prior to or during the accident sequence. NTSB Form 6120 was not received from the pilot for additional information.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN18LA307