Community hub
Recent from talks
Knowledge base stats:
Talk channels stats:
Members stats:
Symphony SA-160
The Symphony SA-160 is a CAR 523 certified, two-seat, single-engine, high-wing airplane that was manufactured by Symphony Aircraft Industries in Trois-Rivières, Quebec, Canada in the mid-2000s.
The SA-160 is a development of the Stoddard-Hamilton Glastar amateur-built kit aircraft and is externally similar to that design.
The SA-160 was developed from the Glastar by incorporating many significant changes to the basic design with the aim of simplifying construction and complying with certification requirements. The redesign work was completed by the engineering staff of Ostmecklenburgische Flugzeugbau (OMF Aircraft), (East Mecklenburg Aircraft Works Limited) of Neubrandenburg, Mecklenburg-Vorpommern, Germany between 1998 and 2000. The aircraft produced by OMF were sold under the designation OMF-100-160 Symphony. Later aircraft produced by Symphony Aircraft are designated Symphony SA-160.
The SA-160 has an aluminum wing design, utilizing a NASA GAW-2 Whitcomb airfoil. To simplify construction the wing has no washout and instead has two composite vortex generators of a unique design, outboard on each wing, to ensure that the inboard portion of the wing stalls first, thus retaining aileron control through the stall.
The wing is equipped with slotted Fowler flaps, which occupy 2/3 of the span. These deploy to 40 degrees and lower the stall speed by 9 knots to 51 knots (60 mph). The flaps are always set to 20 degrees for takeoff. The ailerons are operated by control sticks and feature end-fences inboard and outboard for better slow speed and stall handling.
The fuselage is a 4130 welded steel tube cage covered in a non-structural fibreglass skin. The tail group is a mix of fibreglass fairings and aluminum surfaces.
The SA-160 is powered by a Lycoming O-320-D2A powerplant of 160 hp, driving a two-bladed wood fixed pitch MT propeller.
Symphony Aircraft continued the development started by OMF on a Thielert Centurion 1.7 diesel powered version, which OMF had designated as the OMF-100-135. The performance with the 135 hp engine was disappointing and the project was shelved in 2005.
Hub AI
Symphony SA-160 AI simulator
(@Symphony SA-160_simulator)
Symphony SA-160
The Symphony SA-160 is a CAR 523 certified, two-seat, single-engine, high-wing airplane that was manufactured by Symphony Aircraft Industries in Trois-Rivières, Quebec, Canada in the mid-2000s.
The SA-160 is a development of the Stoddard-Hamilton Glastar amateur-built kit aircraft and is externally similar to that design.
The SA-160 was developed from the Glastar by incorporating many significant changes to the basic design with the aim of simplifying construction and complying with certification requirements. The redesign work was completed by the engineering staff of Ostmecklenburgische Flugzeugbau (OMF Aircraft), (East Mecklenburg Aircraft Works Limited) of Neubrandenburg, Mecklenburg-Vorpommern, Germany between 1998 and 2000. The aircraft produced by OMF were sold under the designation OMF-100-160 Symphony. Later aircraft produced by Symphony Aircraft are designated Symphony SA-160.
The SA-160 has an aluminum wing design, utilizing a NASA GAW-2 Whitcomb airfoil. To simplify construction the wing has no washout and instead has two composite vortex generators of a unique design, outboard on each wing, to ensure that the inboard portion of the wing stalls first, thus retaining aileron control through the stall.
The wing is equipped with slotted Fowler flaps, which occupy 2/3 of the span. These deploy to 40 degrees and lower the stall speed by 9 knots to 51 knots (60 mph). The flaps are always set to 20 degrees for takeoff. The ailerons are operated by control sticks and feature end-fences inboard and outboard for better slow speed and stall handling.
The fuselage is a 4130 welded steel tube cage covered in a non-structural fibreglass skin. The tail group is a mix of fibreglass fairings and aluminum surfaces.
The SA-160 is powered by a Lycoming O-320-D2A powerplant of 160 hp, driving a two-bladed wood fixed pitch MT propeller.
Symphony Aircraft continued the development started by OMF on a Thielert Centurion 1.7 diesel powered version, which OMF had designated as the OMF-100-135. The performance with the 135 hp engine was disappointing and the project was shelved in 2005.