Installation of vortex generators to affect reductions in stall speed and minimum control speed and to increase the take off weight to 7579 pounds and the ramp weight to 7629 pounds
Installation of vortex generators to affect reductions in stall speed and minimum control speed and to increase the take off weight to 7579 pounds and the ramp weight to 7629 pounds
Please contact modification supplier for further details.
STC Status: Amended
STC Date: 06/07/94
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Cessna Aircraft Company