The aircraft features a cantilever strut-braced triplane layout, a single-seat, with an optional two-seats-in-tandem open cockpit, fixed conventional landing gear and a single engine in tractor configuration.
The St Croix Sopwith Triplane differs from the original 1916 design in that it employs a welded steel tube fuselage, modern engine installation and other minor details. The Triplane is all covered in doped aircraft fabric. Its 26.51NaN1 span wing uses strut and cable-bracing and has a wing area of 231square feet. The cabin width is 27inches. The acceptable power range is 150to and the standard engine used is the 1900NaN0 Lycoming O-435 powerplant.
The St Croix Sopwith Triplane has a typical empty weight of 1475lb and a gross weight of 2000lb, giving a useful load of 525lb. With full fuel of the payload for the pilot, passengers and baggage is 315lb.
The standard day, sea level, no wind, take off with a 1900NaN0 engine is 2500NaN0 and the landing roll is 7500NaN0.
The manufacturer estimated the construction time from the supplied kit as 4000 hours.
By 1998 the company reported that 25 kits had been sold and 15 aircraft were completed and flying.