N165CT

Substantial
None

FLIGHT DESIGN GMBH CTSWS/N: 06-03-09

Accident Details

Date
Tuesday, May 23, 2023
NTSB Number
CEN23LA200
Location
Gregory, MI
Event ID
20230524192230
Coordinates
42.441702, -84.064361
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot’s improper landing flare that resulted in a hard, bounced landing and subsequent overstress failure of the nose landing gear.

Aircraft Information

Registration
Make
FLIGHT DESIGN GMBH
Serial Number
06-03-09
Engine Type
4-cycle
Year Built
2006
Model / ICAO
CTSWFDCT
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
2
FAA Model
CTSW

Registered Owner (Current)

Name
REGISTRATION PENDING
Address
30 N GOULD ST STE R
City
SHERIDAN
State / Zip Code
WY 82801-6317
Country
United States

Analysis

On May 23, 2023, about 0946 eastern daylight time, a Flight Design GMBH CTSW, N165CT, was substantially damaged when it was involved in an accident at Richmond Field Airport (69G), Gregory, Michigan. The pilot was not injured. The flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91 as a personal flight.

The pilot reported that after a 40-minute flight he overflew 69G to familiarize himself with the area and the condition of the turf runway before he entered a left traffic pattern for runway 36. The automated weather observing system reported the wind was nearly calm. He flew the final approach at the “appropriate speed with 40 degrees of flaps” extended. During the landing, the nose landing gear gently bounced after touchdown then the nose collapsed, and the airplane nosed over.

The responding Federal Aviation Administration inspector stated that the nose landing gear strut was found separated at the fork. A flight control continuity check was completed, and no anomalies were found. Photos of the airplane revealed the fuselage and empennage sustained substantial damage.

Metallurgical examination of the nose landing gear rotation unit revealed the fracture surfaces were consistent with shear overstress. A review of the maintenance logbooks revealed that the nose landing gear had been replaced two previous times due to hard landing events. No anomalies were noted with the airplane that would have precluded normal operation.

Recorded wind at the time of the accident was from 140° at 4 knots.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN23LA200