N4946X

Substantial
None

Rockwell International S-2RS/N: 5007R

Accident Details

Date
Saturday, July 23, 2005
NTSB Number
DFW05CA189
Location
Hamlin, TX
Event ID
20050802X01138
Coordinates
32.849998, -100.137779
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 propeller blade seal resulting in an oil leak. Contributing factors were the limited forward visibility and lack of suitable terrain for the precautionary landing.

Aircraft Information

Registration
N4946X
Make
ROCKWELL INTERNATIONAL
Serial Number
5007R
Engine Type
Reciprocating
Year Built
1975
Model / ICAO
S-2RNAL2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
TRI COUNTY SPRAYERS INC
Address
15994 FM 668
Status
Deregistered
City
HAMLIN
State / Zip Code
TX 79520-6606
Country
United States

Analysis

On July 23, 2005, approximately 0900 central daylight time, a tailwheel-equipped Rockwell International S-2R agricultural single-engine airplane, N4946X, registered to and operated by Tri County Sprayers, Inc., of Hamlin, Texas, was substantially damaged during a forced landing while maneuvering during an aerial application flight near Hamlin, Texas. The commercial pilot, sole occupant of the airplane, was not injured. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 137 aerial application flight. The local flight originated from the Hamlin Municipal Airport, near Hamlin, Texas, at an unknown time.

According to an Federal Aviation Administration (FAA) inspector, who responded to the accident site, the 700-hour pilot was performing an aerial application of fertilizer on a field when he noticed that the engine temperature was high and engine oil on the coating the windscreen. The pilot initiated a precautionary landing to a nearby field with "limited forward visibility."

During the landing roll, the airplane struck a berm and the right main landing gear collapsed before the airplane came to rest in the upright position.

Examination of the airplane by the FAA inspector revealed that the right main landing gear was separated from the fuselage and the firewall was bent. Examination of the propeller assembly revealed that the oil leak originated from a seal at the base of a propeller blade at the propeller hub attaching point. Oil was also observed on the windscreen and within the engine compressor inlet.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# DFW05CA189