N61802

Substantial
Minor

Air Tractor AT-502BS/N: 502b-0392

Accident Details

Date
Tuesday, February 18, 2003
NTSB Number
FTW03LA098
Location
Holly Grove, AR
Event ID
20030219X00235
Coordinates
34.583332, -91.165832
Aircraft Damage
Substantial
Highest Injury
Minor
Fatalities
0
Serious Injuries
0
Minor Injuries
1
Uninjured
0
Total Aboard
1

Probable Cause and Findings

The pilot's failure to abort the takeoff.

Aircraft Information

Registration
N61802
Make
AIR TRACTOR
Serial Number
502b-0392
Engine Type
Turbo-shaft
Year Built
1996
Model / ICAO
AT-502BAT5T
Aircraft Type
Fixed Wing Single Engine
No. of Engines
1

Registered Owner (Historical)

Name
SALE REPORTED
Address
120 GROUBY AIRPORT RD
Status
Deregistered
City
PRATTVILLE
State / Zip Code
AL 36067-7048
Country
United States

Analysis

On February 18, 2003, at 0830 central standard time, an Air Tractor AT-502B turbine powered agricultural airplane, N61802, was substantially damaged upon collision with a fence while attempting to takeoff from runway 15 at the Holly Grove Municipal Airport (2A6), near Holly Grove, Arkansas. The non-instrument rated commercial pilot, sole occupant of the aircraft, sustained minor injuries. The airplane was registered to Philips County Flying Service, Inc., of Marvell, Arkansas, and was being operated by Hill Flying Service, Inc., of Holly Grove, Arkansas. Visual meteorological conditions prevailed for the Title 14 Code of Federal Regulations Part 137 flight for which a flight plan was not filed. The local aerial application flight was originating at the time of the accident.

The pilot reported to the FAA inspector, who responded to the accident site, that the scheduled local aerial application of fertilizer was the first flight of the day. The airplane was topped off with fuel and the hopper was also filled with fertilizer. The pilot stated that he configured the airplane with full flaps for a full-length takeoff from runway 15 (4,500 feet by 50 feet wide).

During the takeoff roll, the airplane collided with a threshold light and overran the departure end of the runway. The airplane then impacted a support post for a 10-foot high airport perimeter fence. The airplane came to rest in the inverted position entangled in the fence. There was no fire and no fuel was spilled. The hopper was not compromised. Detailed examination of the airplane by the FAA inspector revealed structural damage to the fuselage and both wings. The empennage remained connected to the fuselage only by the control cables. The propeller remained attached to the engine mounts, and the turbine engine remained attached to the airframe.

The last annual inspection for the airframe and the engine was completed on January 29, 2003, at 3,071 aircraft hours, approximately 6 hours prior to the accident. In a telephone interview, the 16,000-hour pilot reported to the NTSB investigator-in-charge that the engine was producing full takeoff power at the start of his takeoff roll; however, he suspected that "the engine power had decayed during the latter part of the takeoff roll, which he was not able to detect in time to abort the flight."

Data Source

Data provided by the National Transportation Safety Board (NTSB). For more information on this event, visit the NTSB Records Search website. NTSB# FTW03LA098