N4907X

Substantial
None

Rockwell S 2RS/N: 2099R

Accident Details

Date
Saturday, May 25, 2019
NTSB Number
CEN19LA156
Location
Oakes, ND
Event ID
20190528X53638
Coordinates
46.096942, -97.919441
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The failure of the helical cam gear of the engine assembly due to fatigue cracks in the gear teeth, which resulted in a total loss of engine power.

Aircraft Information

Registration
N4907X
Make
ROCKWELL
Serial Number
2099R
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
S 2RSA02
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
PLATH AVIATION
Address
4875 158TH AVE SE
Status
Deregistered
City
DAVENPORT
State / Zip Code
ND 58021-9761
Country
United States

Analysis

On May 25, 2019, about 1430 central daylight time, a Rockwell S2R-10 airplane, N4907X, sustained substantial damage when it was involved in an accident near Oakes, North Dakota. The commercial pilot was not injured. The airplane was operated as a Title 14 Code of Federal Regulations Part 137 aerial application flight.

The pilot reported that he was spraying a field about 10 miles southeast of his home airport. After completing 15 spray runs, the pilot maneuvered the airplane for another spray run when the engine lost total power and the pilot could not maintain altitude. The pilot maneuvered the airplane for a forced landing in a field, during which the fuselage and wings were substantially damaged. The pilot exited the airplane without injuries.

The engine had about 485 hours of time in service since its most recent overhaul, and about 12 hours since its most recent annual inspection. The engine was successfully operated in a test cell at idle power. After the engine run, the front section of the engine was disassembled and examined. The helical cam gear was found with its gear teeth fractured and smeared. Several of the gear teeth cracks showed fatigue signatures during metallurgical examination. The helical cam gear assembly did not show any pre-existing installation anomalies and no other pre-impact anomalies were found with the engine.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN19LA156