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Lake Micro Aero Dynamics Vortex Generators
Lake Micro Aero Dynamics Vortex Generators
Lake Micro Aero Dynamics Vortex Generators
 
The Micro Vortex Generators for the Lake Aircraft LA-4, LA-4A, LA-4P, LA-4-200, and Model 250 are ready for installation. These provide a reduction in stall speed and a reduced landing / takeoff roll. Improved characteristics, complete kit. Stall characteristics greatly improved, get off the water more soon!

The Micro VG Kit consists of 92 Vortex Generators mounted on the FULL SPAN on the wings, just aft the leading edge, and 58 Vortex Generators mounted near the leading edge of the Flaps. The kit includes the detailed drawings, instructions, templates for positioning the VGs, spares, Loctite Depend adhesive. This is an 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.

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.
Please choose from the models and write it in the space provided: Lake Aircraft LA-4, LA-4A, LA-4P, LA-4-200, Model 250

The VGs can be painted to match your plane for an additional cost. Please specify the information below.

Sale Price: $2,145.00


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Product Code: VG-LAKE

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 Registration Number


Existing Aerodynamic Modifications:


Extended wings on aircraft?


Paint Color(s) and Product Code(s)


Pre-painted Micro VG

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

Qty:  
Features Technical Specs Information
 
Features

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 airspeeds with improved control authority.


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