N6133T

Substantial
None

Ayres S2R-G6S/N: G6-136

Accident Details

Date
Wednesday, June 14, 2006
NTSB Number
ATL06LA093
Location
Selma, AL
Event ID
20060621X00783
Coordinates
32.374721, -87.102500
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The loss of engine power during the approach to land due to an uncontained turbine failure, which resulted in an in-flight fire.

Aircraft Information

Registration
N6133T
Make
AYRES
Serial Number
G6-136
Engine Type
Turbo-shaft
Model / ICAO
S2R-G6A660
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
MILLS AG SERVICE
Address
13145 E 3100 NORTH RD
Status
Deregistered
City
POTOMAC
State / Zip Code
IL 61865-6654
Country
United States

Analysis

On June 13, 2006, at 2017 central daylight time, a Ayres S2R-G6, N6133T, registered to and operated by Hills Flying Service, Inc., as a 14 CFR Part 137 aerial application flight, experience an uncontained engine failure and in-flight fire while on final approach to runway 24, at the Skyharbor Airport Selma, Alabama. Visual meteorological conditions prevailed and no flight plan was filed. The commercial pilot reported no injuries and the airplane was substantially damaged. The flight originated from Skyharbor airport, Selma, Alabama on June 13, 2006, at 1800.

According to the pilot, he departed Skyharbor airport to spray 75 acres of beans. However, due to rain showers he was unable to complete the mission, and returned to the airport. When he was on short final to land on runway 24, during power reduction, "the engine exploded and fire and shrapnel shot through the engine cowlings." Upon landing, he quickly exited the airplane, and ran to his office for help. On scene examination of the airplane by an FAA inspector found the airplane consumed by fire from the propeller aft to the cockpit. Examination of the engine found a large hole in the turbine section with most of the internal turbine components missing. The missing components were not located. Examination of the engine logbooks found that the last hot section inspection was performed on March 17, 2003 at a total time of 3,963.1 hours, and the last annual inspection was performed on February 14, 2006, at a total time of 5,406.3 hours. Time since the last hot section inspection was 1,445.2 hours. The engine total time since new was 7,840.2, hours, and had accumulated 2,280.0 hours since overhaul.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# ATL06LA093