Thursday, May 5, 2016

Loved ones to host 'Spring Fling' in memory of crash victim: Lancair IV-P, Art Sign Company, N401PT, fatal accident occurred January 30, 2016 at Southwest Georgia Regional Airport (KABY), Albany, Dougherty County, Georgia

On Saturday, the loved ones of Brittany Kerfoot will host a family-fun event for the community in her honor.

Albany, GA — On Saturday, the loved ones of Brittany Kerfoot will host a family-fun event for the community in her honor.

Brittany's Spring Fling will be held at the Chehaw Park stage from 10 a.m. until 8 p.m. The event in memory of Brittany Kerfoot, one of the three victims killed in the plane crash at the Southwest Georgia Regional Airport in January.

Hannah Sholar- Owens, one of the organizers of the event and Kerfoot's best friend, said that the entire event began from the passion Kerfoot had for children. Sholar-Owens said Kerfoot visited Chehaw on a field trip with her students back in November when she picked up on something that she couldn't let go.

"They didn't have any handicap accessible toys, or area, or toddler equipment. So we took it upon ourselves to talk with Chehaw about adding that equipment in her memory" said Sholar-Owens.

The proceeds from the spring fling will go to the Brittany Kerfoot Memorial Playground Project. The goal is to raise money to bring a handicap-accessible and toddler area to the playground at Chehaw, as well as refurbish the tiles at the entrance. Tiles will be sold that children can put their handprints in and will be placed into the new entrance.

"This cause is actually going to help the whole community. This is something that we definitely need and it's an area where anybody can come. Brittany loved children and she made a huge impact on over 300 children's lives just that she personally taught," said Sholar-Owens.

There will be a cornhole tournament, live music, bounce houses, food and more. There is a $5 entrance fee, $3 parking fee and a $15 cooler fee (no glass allowed). Children under 12 are free.

The opening ceremony and live music will kick off at noon. Children's activities are from 10 a.m. until 4 p.m.

Original article can be found here:

Art Sign Company:  

FAA Flight Standards District Office:  FAA Atlanta FSDO-11

NTSB Identification: ERA16FA097

14 CFR Part 91: General Aviation
Accident occurred Saturday, January 30, 2016 in Albany, GA
Aircraft: BROOK AARON D LANCAIR IV P, registration: N401PT
Injuries: 3 Fatal.

This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. NTSB investigators either traveled in support of this investigation or conducted a significant amount of investigative work without any travel, and used data obtained from various sources to prepare this aircraft accident report.

On January 30, 2016, at 1445 eastern standard time, an experimental amateur-built Lancair IV-P, N401PT, operated by a private individual, was destroyed when it impacted terrain shortly after takeoff from the Southwest Georgia Regional Airport (ABY), in Albany, Georgia. The commercial pilot, pilot rated passenger and one additional passenger were fatally injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight, which was conducted under the provisions of Title 14 Code of Federal Regulations Part 91.

Witness reports indicated that the airplane taxied to the beginning of runway 22 at ABY, and lifted off within the first 1,000 feet of the 6,601 foot-long runway. The airplane began to bank sharply immediately after takeoff, and reached a 90-degree bank as it climbed to treetop height. The witness was not certain if the bank was to the right or left; however, the airplane then began to pitch downward and descend, while maintaining the 90 degree bank until it struck the ground.

A witness located about a quarter mile north of the accident site reported that the airplane sounded "normal" until shortly before impact, when the engine noise became louder.

The airplane impacted a grass field about 1,900 feet down the runway, and 280 feet to the right of the runway centerline. The wreckage path extended from the initial impact ground scar along a heading of 270 degrees, and was 170 feet long. A position light with green lens fragments and the right winglet were among the debris found closest to the initial impact scar. Both wings were separated from the fuselage at their root, and were fragmented along the wreckage path. The left wing tip and winglet were found about 130 feet along the wreckage path. The main wreckage area included the empennage, which was largely intact, with severe fire and impact damage forward of the rear seats. The right horizontal stabilizer and elevator were fractured about mid-span with the outboard portion displaced forward. The elevator trim tab was found slightly trailing edge down. The rudder trim tab was found slightly trailing edge right. The engine mounting structural tubes were fractured and the engine was found inverted. The propeller hub separated from the engine flange, and one of the three blades separated from the hub. All three blades exhibited some bending in the aft direction from about mid-span outward, and each had showed some amount of twisting deformation.

The engine power turbine blades were intact and exhibited slight bending at their tips and rub marks at their roots. The engine casing was displaced and twisted, and the engine could not be turned by hand at the starter or the propeller shafts. After removal of the planetary gear system, the propeller shaft turned easily and did not exhibit any evidence of twisting.

Examination of the airframe revealed that the main landing gear were retracted, however the position of the nose landing gear could not be determined. The position of the flaps could not be determined. Pitch control continuity was confirmed from the elevator though push-pull tubes to the aft cabin area. The elevator moved freely. Rudder control continuity was confirmed from the rudder through a push-pull tube to the cable and bell crank assembly in the empennage. The rudder was free to move, however both cables exhibited binding as a result of fire damage. Both ailerons had separated from their respective wings and were found fractured and fire damaged. Both cockpit control sticks remained connected to their control tubes, however continuity from those tubes to the remainder of the control components could not be confirmed due to impact and fire damage.

A portable global positioning system receiver was recovered from the accident site and forwarded to the NTSB Vehicle Recorder laboratory for examination.

A witness reported that as the occupants embarked, the pilot/owner was seated in the left front seat, and the pilot rated passenger was seated in the right front seat. According to Federal Aviation Administration (FAA) records, the pilot reported 1,000 hours of flight experience at the time of his most recent third-class medical examination which was performed on January 20, 2015.The pilot rated passenger held airline transport pilot and flight instructor certificates, and he reported 6,750 flight hours of experience at the time of his most recent FAA second-class medical examination, which was performed on July 8, 2015.

According to FAA records, the airplane was equipped with a Walter 601 series turboprop engine and issued an experimental airworthiness certificate in April 2002. It was purchased by the pilot on December 10, 2015. Initial review of maintenance logbooks revealed that the most recent condition inspections of the airframe and engine occurred on October 29, 2015, and both were found to be in satisfactory condition.

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