Installation of vortex generators on the wings, engine nacelle, horizontal tail surfaces, and leading edge of the rudder of the above model aircraft
Installation of vortex generators on the wings, engine nacelle, horizontal tail surfaces, and leading edge of the rudder of the above model aircraft
Please contact modification supplier for further details.
STC Status: Issued
STC Date: 16/10/08
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Hawker Beechcraft Corporation