N6017E

Substantial
None

AIR TRACTOR INC AT-502BS/N: 502B-0260

Accident Details

Date
Sunday, June 23, 2013
NTSB Number
CEN13LA371
Location
Campbell, NE
Event ID
20130625X62910
Coordinates
40.602222, -99.255279
Aircraft Damage
Substantial
Highest Injury
None
Fatalities
0
Serious Injuries
0
Minor Injuries
0
Uninjured
1
Total Aboard
1

Probable Cause and Findings

The pilot's decision to continue with the takeoff roll despite the airplane's difficulty becoming airborne The high-density altitude likely contributed to the airplane's reduced performance.

Aircraft Information

Registration
Make
AIR TRACTOR INC
Serial Number
502B-0260
Engine Type
Turbo-prop
Year Built
1994
Model / ICAO
AT-502BAT5T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1
Seats
1
FAA Model
AT-502B

Registered Owner (Current)

Name
GEORGES AERIAL SPRAYING SERVICE INC
Address
405 N EUCLID AVE
City
SUTTON
State / Zip Code
NE 68979-2429
Country
United States

Analysis

On June 23, 2013, about 1630 central daylight time, an Air Tractor Inc. AT-502B, N6017E, was substantially damaged when it settled into a field after takeoff near Campbell, Nebraska. The commercial pilot was not injured. The aircraft was registered to and operated by Campbell Aerial Spraying, Inc., under the provisions of 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed for the flight, which operated without a flight plan. The flight was originating at the time of the accident.

Prior to takeoff, the airplane was loaded with 170 gallons of chemicals and the fuel tanks were half full. The pilot estimated that the airplane was 7,268 pounds at the time of the accident; 732 pounds below maximum gross weight. During the takeoff roll, the airplane reached the expected point of rotation, but was "not flying yet." The pilot scanned the gauges, verified full power, and added additional flaps. The airplane became airborne but then settled to the ground. The airplane impacted a fence and rotated 180 degrees before coming to a complete stop.

According to the Federal Aviation Administration inspector who responded to the accident, during the impact with the ground, the right main landing gear separated from the airframe. The right wing was bent and wrinkled and the fuselage structure was bent and broken. According to the mechanic responsible for repairing the airplane, there was minor damage to the fuselage and substantial damage to right wing. The pilot stated that there were no mechanical anomalies with the airplane prior to the accident. Calculations of relevant meteorological data indicated that the density altitude was about 4,100 feet.

The flight manual for the Air Tractor AT-502B states that flaps should be retracted for a normal takeoff. A takeoff from a short field with a full hopper requires 10 degrees of flaps. Air Tractor does not provide performance expectations or guidance for the use of more than 10 degrees of flaps at takeoff.

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# CEN13LA371