The Patented Modification

The modification enhances the aerodynamic efficiency of the wing. In general, this modification to the Boeing 737 realizes reduced fuel consumption by increasing the aircraft's lift-to-drag ratio.

The aft segments of the trailing edge flaps are relocated aft and below their standard locations when the flaps are retracted. These changes result in increased wing area, increased airfoil camber, and a lengthened wing cord.

Specifically, this creates a more highly cambered trailing edge of the airfoil. The aft flap segments resume their normal positions in regards to the other flap segments during flap deployment. Trailing edge flaps are not limited in travel or operation. Induced drag is directly related to the angle of attack, and thus a greater angle generates more induced drag. The increased aft wing camber enables the airfoil to achieve the same lift at a lower angle of attack.

"Each kilogram of fuel saved reduces CO2 emissions by 3.16 kilograms" -IATA

Approved and Verified by: U.S Federal Aviation Agency European Aviation Safety Agency Transport Canada General Administration of Civil Aviation of China

AeroTech Wing Modification System: Reduces Fuel Burn by up to 4% Rapid ROI average of 12-15 months Parts Warranty for Three Years Approximately 300 man hour installation Reduces Carbon Footprint and Greenhouse gasses