FAA Flight Standards District Office: FAA Van Nuys FSDO-01
NTSB Identification: WPR16LA110
14 CFR Part 91: General Aviation
Accident occurred Friday, May 13, 2016 in Mojave, CA
Aircraft: Seguin Quickie, registration: N68TQ
Injuries: 1 Minor.
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 may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.
On May 13, 2016, about 1530 Pacific daylight time, an experimental amateur-built Quickie, N68TQ, was substantially damaged when it impacted a structure and terrain following a loss of engine power at Mojave Air and Space Port (MHV), Mojave, California. The pilot received minor injuries. The test flight was conducted under the provisions of Title 14 Code of Federal Regulations Part 91. Visual meteorological conditions prevailed.
The airplane was originally developed and designed as a kit to be powered by a single piston engine. According to the pilot, he and another individual had modified the airplane to be powered by two turbine engines, and they planned to use it for air-racing purposes. The accident flight was the third flight of the airplane, and the flight was intended to begin exploring the crosswind handling capability and characteristics of the airplane. The pilot intended to conduct several circuits in the airport traffic pattern, each terminating in a low approach and go around, with one landing at the end of the flight.
The pilot departed on runway 12, and conducted his first approach to runway 26. He abandoned that approach, when the airplane was about 200 feet above ground level (agl), and climbed back up to pattern altitude for another approach. This time, based on the winds, he maneuvered for a landing on runway 12. While in the flare at approximately 10 feet agl, a gust from the right side disturbed the airplane, and the pilot applied power to go-around. He heard the left engine "spool down," and confirmed that via the engine instrument indications. The gust disturbance and power loss caused the airplane to track towards the airliners stored at MHV, and the pilot found himself headed for a parked B-747. He maintained approximately 30-40% thrust on the right engine to clear the B-747, but he was unable to correct the directional slew with full aileron/rudder controls. The airplane cleared the parked B-747 but impacted a structure and the ground shortly thereafter.
The pilot held a commercial pilot certificate with multiple ratings. He reported that he had about 1,650 total hours of flight experience, including about 0.8 hours in the accident airplane make and model. His most recent flight review was completed in May 2015, and his most recent Federal Aviation Administration (FAA) second-class medical certificate was issued in September 2015.
FAA information indicated that the airplane was built by the pilot, and registered to him in February 2016. The pilot reported that the airplane was equipped with two Czech-manufactured PBS-TJ40 turbine engines, and that the engines were FADEC (full authority digital engine control) equipped.
The MHV 1520 automated weather observation included winds from 210 degrees at 15 knots, visibility 10 miles, clear skies, temperature 32 degrees C, dew point minus 2 degrees C, and an altimeter setting of 29.95 inches of mercury. The 1540 winds were reported as being from 220 degrees at 18 knots.