Crash of a Beechcraft King Air C90 in Springdale: 2 killed

Date & Time: Nov 1, 2013 at 1742 LT
Type of aircraft:
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Pine Bluff - Bentonville
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Aircraft impacted terrain 4 miles southeast of the Springdale Municipal Airport, Springdale, Arkansas. The private pilot and passenger were fatally injured. The airplane was destroyed. The airplane was registered to J&G Aviation, LLC, and operated by the pilot, both of Camden, Arkansas, under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight, and no flight plan had been filed. The flight originated from Pine Bluff, Arkansas, about 1700. According to the Federal Aviation Administration (FAA), the pilot contacted Fort Smith, Arkansas (FSM), and advised he was en route from Pine Bluff (PBF), Arkansas, to Bentonville (VBT), Arkansas. He was given flight following services. Later, the pilot said he wanted to change his destination to Fayetteville (KFYV), Arkansas. When the FSM controller asked the reason for the destination change and if he required any assistance, the pilot stated he was low on fuel. He requested the distance to FYV, and the controller told him it was 9 miles away. The pilot said he needed something closer. The controller advised that Springdale Airport (ASG) was at his 12 o'clock position and 4 miles away. The pilot said he had ASG in sight and was familiar with the airport. The controller issued the pilot a frequency change to ASG tower. The pilot contacted ASG tower and reported he was low on fuel. The ASG controller issued the wind conditions and altimeter setting and cleared the pilot to land on runway 36. Approximately 30 seconds later, the pilot advised ASG that he was not going to make the airport. The ASG controller attempted to get the aircraft's position. No further transmissions were received from the pilot. A witness saw the airplane descend, pull up abruptly, and impact the ground in a right wing-low, noselow attitude. There were power lines about 300 feet short of the impact point. The on-scene examination revealed no ground scars, only impact ground gouges. Control continuity was established from the flight controls to the center of the airplane. The right wing was destroyed. No fuel was observed in the left wing or nacelle tanks. The landing gear and flaps were retracted. Propeller signatures indicate the propellers were not feathered.