N274DR

Substantial
Serious

Thatcher CX4S/N: 122

Accident Details

Date
Wednesday, June 24, 2020
NTSB Number
WPR20LA193
Location
Upland, CA
Event ID
20200624X54441
Coordinates
34.109443, -117.694999
Aircraft Damage
Substantial
Highest Injury
Serious
Fatalities
0
Serious Injuries
1
Minor Injuries
0
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The inflight separation of the propeller assembly due to a fatigue fracture of the crankshaft. Contributing to the accident was the pilot’s restricted visibility during landing, which resulted in an excessive approach speed, a long landing, and subsequent impact with terrain.

Aircraft Information

Registration
N274DR
Make
THATCHER
Serial Number
122
Engine Type
Reciprocating
Year Built
2017
Model / ICAO
CX4CX4
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
RESER DAVID A
Address
1316 W VALENCIA MESA DR
Status
Deregistered
City
FULLERTON
State / Zip Code
CA 92833-2223
Country
United States

Analysis

On June 24, 2020, about 1145 Pacific daylight time, a Thatcher CX4, N274DR, was substantially damaged when it was involved in an accident at Cable Airport (CCB), Upland, California. The pilot was seriously injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight.

The pilot reported that he was returning to CCB following an uneventful local flight when the propeller separated from the engine. He was about 1 mile from the airport at an altitude of about 1,100 ft above ground level (agl) at the time. The pilot said that oil covered the windscreen and canopy, restricting forward visibility; however, he continued to fly toward the airport. When the airplane crossed the threshold of the runway, it was about 50 ft agl, and “going way too fast,” as he was trying to look out to the side to keep the airplane aligned with the runway. The airplane touched down near the end of the runway and bounced. The airplane continued over a fence and collided with a dirt berm.

Postaccident examination of the airplane by the pilot revealed that both wings and fuselage were substantially damaged. The propeller assembly and a portion of the engine crankshaft were separated and not located.

The remaining portion of the crankshaft from the Hummel VW 2400CC engine was sent to the National Transportation Safety Board Materials Laboratory for further examination. Examination of the crankshaft revealed that two fractures initiated at the termination of a square keyway slot in the crankshaft. The presence of ratchet marks at the fracture origins and the presence of progressions marks along the fracture path were indicative of fatigue fracture initiation and growth.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# WPR20LA193