N4992X

Substantial
None

ROCKWELL INTERNATIONAL S-2RS/N: 5037R

Accident Details

Date
Friday, July 9, 2010
NTSB Number
CEN10LA404
Location
Deshler, OH
Event ID
20100716X33311
Coordinates
41.207500, -83.901107
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

A loss of engine power for undetermined reasons.

Aircraft Information

Registration
Make
ROCKWELL INTERNATIONAL
Serial Number
5037R
Engine Type
Turbo-prop
Year Built
1975
Model / ICAO
S-2RNAL2
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
S-2R

Registered Owner (Current)

Name
RUHE SALES LLC
Address
5450 STATE ROUTE 109
City
LEIPSIC
State / Zip Code
OH 45856-9438
Country
United States

Analysis

On July 9, 2010, at 1930 eastern daylight time, a Rockwell International S-2R, N4992X, collided with trees and a ditch during an off-airport forced landing following a loss of engine power during an aerial application flight. The airline transport pilot was not injured. Both wings of the airplane received substantial damage. The aircraft was registered to Bob Ruhe Ag Service, Inc., and operated under the provisions of 14 Code of Federal Regulations Part 137. Visual meteorological conditions prevailed and no flight plan was filed. The local flight originated from Leipsic, Ohio, at 1900.

The pilot reported the engine lost power during the middle of a spray run when he was just above the height of the corn crop. He stated he turned the airplane away from the town and power lines. The airplane contacted small trees and a ditch during the forced landing in a bean field.

An on-scene examination of the engine, a Pratt & Whitney PT6A-34, revealed the power section was seized due to impact damage to the exhaust duct. The gas generator and accessory drives rotated freely by hand. All of the external lines, filters, and screens were normal. The power turbine and power turbine shroud contained light rotational rubbing. The reduction gearbox rotated smoothly by hand.

Further inspection of the engine revealed rotational signatures to the power turbine blade tips and shroud. A teardown of the engine and a functional check of the fuel control unit, high pressure fuel pump, and the propeller governor failed to reveal any failures/malfunctions that would have prevented the engine from producing power. A detailed examination report is contained in the public docket for this accident.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN10LA404