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Cessna 120, 140 Micro Aero Dynamics Aircraft Vortex Generators
Cessna 120, 140 Micro Aero Dynamics Aircraft Vortex Generators
Cessna 120, 140 Micro Aero Dynamics Aircraft Vortex Generators

The Micro Vortex Generators for the Cessna 120 and 140 are FAA, STC approved. It provides a 9% reduction in stall speed, improved aileron response, reduced landing and takeoff roll.
The Micro VG Kit consists of 68 Vortex Generators mounted on the wings, just aft of the leading edge and 28 Vortex Generators mounted on the underside o the horizontal stabilizer. The kit includes the STC detailed drawings, instructions, templates for positioning the VGs, spares, Loctite Depend adhesive and all the materials needed for the easy one day installation except a bottle of isopropyl alcohol, a ladder and a roll of paper towels.
The Micro Vortex Generators are manufactured under FAA PMA from aircraft grade 6063-T6 Aluminum, alodined to a Boeing mil-spec, ready for painting. Each VG is curved on the bottom to fit the contour of the wing. Easy one day professional installation. If installed by Blue Skies Aviation
, there is a 10% discount off of the Micro Vortex Generators. The discount is given at the time of the installation, off of the installation cost.

Please choose from the models below and write it in the space provided:
Cessna 120 or Cessna 140


The VGs can be painted to match your plane for an additional $200 per color, please specify the information below.
Sale Price: $695.00

Product Code: CESSNA-120-AND-140

Add 8130 for Micro VGs

Specify location for the 8130 Certificate in special instructions (International Orders Require One) [$110.00]
Model Number

Special Instructions

Aircraft make and model

Existing aerodynamic modifications:

Extended wings on aircraft?

Paint color/s and product code

Pre-painted Micro VG

Without paint
One additional color [$265.00]
Two additional colors [$530.00]
Three additional colors [$795.00]

Features Technical Specs Information

A Micro Vortex Generator

Creates a tiny vortex in the airstream over an airfoil. This vortex energizes the normally stagnant boundary layer of air on the wing's surface. An energized boundary layer is more resistant to flow separation than a stagnant boundary layer. The result is that airflow "sticks" to the wing better, permitting flight at lower air speeds with improved control authority.

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