NTSB Narrative Summary Released at Completion of Accident
On April 14, 2013, about 0815 eastern daylight time, an experimental amateur-built Kit Fox IV 1200, N117S, was substantially damaged when it impacted terrain while attempting a landing at Treasure Coast Airpark (FL37), Port St. Lucie, Florida. The private pilot was fatally injured. Visual meteorological conditions prevailed, and no flight plan was filed for the local personal flight, which was conducted under the provisions of 14 Code of Federal Regulations Part 91.
A number of witnesses saw portions of the flight, but no one saw all of it. According to some of the witnesses, the airplane took off from runway 27, turned to the north, then circled back to a left downwind for a landing on the same runway. One witness, also a pilot, noted that during the downwind leg, the airplane was “very close in” to the runway. He also noted that although the airplane had taken off in conditions that were a “little hazy,” he subsequently saw it “popping through clouds” on the downwind leg until his view was blocked by a house.
Another witness stated that, as the airplane turned toward the final approach to the runway, she saw the nose drop, and that the airplane then headed “straight down” before she lost sight of it behind a tree line.
Multiple witnesses also reported hearing the engine operating at a high power level without any anomalies.
The airplane impacted the ground next to a busy road, and with storms and darkness anticipated, local authorities requested that it be moved prior to NTSB arrival, which was granted under the condition that extensive photographs be taken.
A site visit the next morning revealed ground scars that were consistent with the airplane initially impacting the ground nose-down. The initial impact point was characterized by a shallow crater in which a portion of a propeller blade was found the previous day. The crater was located in the vicinity of 27 degrees, 14.28 minutes north latitude, 080 degrees, 28.52 minutes west longitude, about 090 degrees, 470 feet from the runway 27 threshold.
A linear ground scar, about the length of the airplane’s wing, emanated from the crater toward a heading of about 220 degrees magnetic. Another ground scar, also about the length of the airplane’s wing, emanated from the crater toward a heading of about 060 degrees magnetic. There was then a lack of ground scarring, which was consistent with the airplane having bounced once before it came to rest on its nose, about 25 feet, 330 degrees magnetic from the crater, heading about 110 degrees magnetic.
An examination of the wreckage at a storage facility revealed that all flight control surfaces were present. Control continuity could not be confirmed to the cockpit due to cockpit crushing.
An approximately 45-degree upward bend of the fuselage was noted just aft of the landing gear. There was also leading edge damage along the entire left wing, and fabric tears on both the upper and lower inboard sections of the right wing. Wing crush angles could not be determined due to the fabric-covered, wooden rib construction.
One of the three composite propeller blades was sheared near the hub while the next blade in rotation exhibited a chordwise fracture and leading edge scuffing and the third blade was relatively unscathed. The spinner exhibited aft and rotational deformation.
A hand-held GPS unit was recovered from the wreckage and forwarded to the NTSB Recorders Laboratory to attempt a data download.