N4888X

Substantial
Minor

Rockwell International S-2RS/N: 2072R

Accident Details

Date
Thursday, June 28, 2001
NTSB Number
FTW01LA156
Location
Sabinal, TX
Event ID
20010628X01287
Coordinates
29.349891, -99.150276
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

a loss of engine power due to a crack in the #9 cylinder, which result in the failure of the connecting rod during the aerial application flight. A contributing factor was the lack of suitable terrain for the forced landing.

Aircraft Information

Registration
N4888X
Make
ROCKWELL INTERNATIONAL
Serial Number
2072R
Engine Type
Reciprocating
Year Built
1974
Model / ICAO
S-2RNAL2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
LINDEMAN RUSTY L
Address
101 FLIGHTLINE DR
Status
Deregistered
City
HONDO
State / Zip Code
TX 78861-2048
Country
United States

Analysis

On June 28, 2001, at 0635 central daylight time, a Rockwell International S-2R agricultural airplane, N4888X, was substantially damaged during a forced landing following a loss of engine power while maneuvering near Sabinal, Texas. The commercial pilot, sole occupant of the airplane, received minor injuries. The airplane was owned and operated by a private individual doing business as Rusty's Flying Service of Hondo, Texas. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 137 aerial application flight. The flight originated from the Hondo Municipal Airport, near Hondo, Texas, at 0610.

While maneuvering after completing a spray pass, the pilot heard a "loud pop," and the engine lost power. The pilot executed a forced landing to a clearing in a field. During the forced landing, the airplane touched down and bounced, nosed over, and came to rest inverted.

According to the operator, the airplane's canopy and roll cage were crushed, the vertical stabilizer separated, and the wing's leading edges sustained substantial damage. The operator stated that an examination of the engine revealed that #9 cylinder had cracked, and subsequently, a connecting rod failed.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW01LA156