N625JS

HISTORY OF FLIGHTOn April 15, 2018, about 1030 central daylight time, an amateur-built Wittman Tailwind W-10 airplane, N625JS, impacted terrain near San Antonio, Texas. The commercial pilot was fatally injured, and the airplane was destroyed by impact forces and fire. The airplane was registered to and operated by the pilot as a Title 14 Code of Federal Regulations Part 91 personal flight. Visual meteorological conditions prevailed for the flight, which departed Castroville Municipal Airport (CVB), Castroville, Texas, about 1025 and was destined for Freedom Springs Ranch Airport (TA66), Pipe Creek, Texas.

A friend of the pilot reported that the purpose of the flight was to accumulate additional flight time with the overhauled engine that had been installed on the airplane during its last condition inspection about 6.5 months before the accident. The pilot's friend reported the pilot had planned to fly from TA66 to CVB to purchase fuel. The pilot's friend also reported that the airplane departed TA66 about 0900. Fueling records showed that the pilot purchased 6.87 gallons of 100 low-lead aviation fuel about 1018 from a self-service fuel pump located at CVB. There were no witnesses to the airplane landing, refueling, or departing CVB.

A witness located about 1 mile from the accident site reported that he initially saw the airplane flying about 1,500 ft above the ground with no noticeable engine issues but that, as the airplane flew past his position, the engine was "struggling" for about 10 seconds, and a total loss of power followed. The witness stated that the airplane was on fire as it descended nose down into terrain. The witness did not observe any black smoke but observed a "fireball" as the airplane descended.

Another witness located near the accident site reported that the airplane was flying west at a very low altitude with fire coming from the bottom of the airplane. The witness stated that, after the airplane passed over, it briefly pitched up before it suddenly banked and descended nose down into the ground west of his position. The witness reported that the airplane "exploded into a fireball" when the airplane impacted the ground.

A review of available Federal Aviation Administration (FAA) air traffic control radar data revealed no transponder data associated with the flight. PERSONNEL INFORMATIONAccording to FAA records, the 68-year-old pilot held a commercial pilot certificate with airplane single-engine land, airplane multiengine land, and instrument airplane ratings. The pilot also held an expired flight instructor certificate for single-engine airplanes. His most recent FAA third-class medical certificate was issued on February 2, 2016, with a limitation that required him to possess glasses for near vision and that he must use hearing amplification. On his medical certificate application, the pilot reported 1,149 hours of total flight experience, 35 hours of which occurred within the previous 6 months. The pilot's third-class medical certificate expired on February 28, 2018, but he had completed the BasicMed medical education course and received a comprehensive medical examination from his physician on March 8, 2018.

A review of the pilot's logbook revealed that he stopped recording individual flights after December 31, 2006. As of that date, the pilot had accumulated 845.1 hours of flight experience, of which 828.1 hours and 17 hours were logged in single-engine and multiengine airplanes, respectively. At that time, he had accumulated 296.1 hours in the accident airplane make and model. The remainder of the flight log included multiple flight reviews and two entries for combined flight time in Cessna 172 airplanes (One entry totaling 175.2 hours for flights flown between September 12, 2012, and January 25, 2016, and another entry totaling 43.8 hours for flights flown between January 16, 2016, and April 1, 2017). The final logbook entry, dated January 25, 2018, was for a flight review in a Cessna 172. The pilot's flight history between the final logbook entry and the date of the accident could not be determined nor could his recency of experience in the accident airplane. AIRCRAFT INFORMATIONThe amateur-built airplane, serial number JS466, was constructed with a steel tube fuselage, wood wings, and fabric covering. The two-seat, high-wing monoplane was equipped with fixed conventional landing gear and flaps. The airplane was powered by a 125-horsepower, 4-cylinder, Lycoming O-290-D reciprocating engine, serial number 1355-20-16. The engine provided thrust through a fixed-pitch, two-blade Aymar-DeMuth 70X62 wood propeller. On November 7, 1986, the airplane received its original special airworthiness certificate from the FAA. On April 11, 1993, the builder applied for an updated special airworthiness certificate and associated operating limitations. The pilot purchased the airplane on January 10, 2004, and its registration certificate was issued on February 26, 2004.

The airplane's recording tachometer was destroyed during the postimpact fire, which precluded a determination of the airplane's total time. According to maintenance documentation, the last condition inspection was completed on September 30, 2017, when the airframe had accumulated a total of 984.9 hours. A field-overhauled engine was installed on the airplane during the last condition inspection. The final logbook entry was for an engine oil change completed on December 10, 2017, when the airframe had accumulated a total of 997.4 hours. At that time, the engine had accumulated 12.5 hours since its overhaul. A postaccident review of the maintenance records found no evidence of unresolved airworthiness issues.

The airplane was equipped with a header fuel tank that supplied fuel directly to the engine carburetor. On April 15, 2011, the fuel tank was removed to repair a leak at the upper aft left corner of the tank. At that time, the airframe had accumulated a total of 965 hours. METEOROLOGICAL INFORMATIONA postaccident review of available meteorological data established that day visual meteorological conditions prevailed at the accident site. The nearest aviation weather reporting station was located at CVB about 5 miles south-southwest of the accident site. At 1035, about 5 minutes after the accident, the CVB automated surface observing system reported a clear sky, calm wind, 10 miles surface visibility, temperature 19°C, dew point -2°C, and an altimeter setting of 30.26 inches of mercury. AIRPORT INFORMATIONThe amateur-built airplane, serial number JS466, was constructed with a steel tube fuselage, wood wings, and fabric covering. The two-seat, high-wing monoplane was equipped with fixed conventional landing gear and flaps. The airplane was powered by a 125-horsepower, 4-cylinder, Lycoming O-290-D reciprocating engine, serial number 1355-20-16. The engine provided thrust through a fixed-pitch, two-blade Aymar-DeMuth 70X62 wood propeller. On November 7, 1986, the airplane received its original special airworthiness certificate from the FAA. On April 11, 1993, the builder applied for an updated special airworthiness certificate and associated operating limitations. The pilot purchased the airplane on January 10, 2004, and its registration certificate was issued on February 26, 2004.

The airplane's recording tachometer was destroyed during the postimpact fire, which precluded a determination of the airplane's total time. According to maintenance documentation, the last condition inspection was completed on September 30, 2017, when the airframe had accumulated a total of 984.9 hours. A field-overhauled engine was installed on the airplane during the last condition inspection. The final logbook entry was for an engine oil change completed on December 10, 2017, when the airframe had accumulated a total of 997.4 hours. At that time, the engine had accumulated 12.5 hours since its overhaul. A postaccident review of the maintenance records found no evidence of unresolved airworthiness issues.

The airplane was equipped with a header fuel tank that supplied fuel directly to the engine carburetor. On April 15, 2011, the fuel tank was removed to repair a leak at the upper aft left corner of the tank. At that time, the airframe had accumulated a total of 965 hours. WRECKAGE AND IMPACT INFORMATIONThe airplane collided with terrain vegetated with tall mesquite bush, yucca, and persimmon trees. The airplane impacted terrain in a 20° nose-down pitch attitude on a 281° magnetic heading. The initial impact point was with a 15-ft tall tree. Fragmented pieces of the left wing and broken branches were found at the base of the tree. The debris located at the base of the tree showed no fire damage. A debris path extended about 50 ft from the initial impact point to the main wreckage. Fuel blight was observed on the tree leaves located along and adjacent to the debris path. Fragmented pieces of the left wing, including the wing spar, left aileron, and left flap, were located about 12 ft from the initial impact point on the left side of the debris path. The left aileron remained attached to the trailing edge of the wing. The left flap remained partially attached to the wing and exhibited bending in multiple locations.

The ground impact area measured about 3.5 ft at its widest point and 8 ft at its longest point . Dirt and vegetation had been ejected from the ground impact area in the direction of the main wreckage. Charred material consistent with the cowling and engine baffles were located at the west end of the ground scar. The debris path consisted of engine components, torn, burned, and fragmented wood and metal components, a seat frame, the left door frame, and the burned remains of the right main landing gear tire. The burnt and fragmented remains of the right wing, including the right aileron and right flap, came to rest on the left side of the debris field. There was burnt vegetation preceding the main wreckage and evidence of ...