Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.
Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.
Please contact modification supplier for further details.
STC Status: Issued
STC Date: 13/05/03
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Cessna Aircraft Company