Installation of vortex generators on the wings, tail surfaces, and...
Overview
Introduction
Installation of vortex generators on the wings, tail surfaces, and vertical fin, in accordance with Micro AeroDynamics Drawing Package MA2146, Revision A, dated March 11, 2004, and installed in accordance with Installation Manual MA2147, Revision IR, dated January 25, 2001 (for the 206 series) or MA2196, Revision IR, dated March 11, 2004 (for the 207 series), or later FAA approved revisions.
Product Description
Installation of vortex generators on the wings, tail surfaces, and vertical fin, in accordance with Micro AeroDynamics Drawing Package MA2146, Revision A, dated March 11, 2004, and installed in accordance with Installation Manual MA2147, Revision IR, dated January 25, 2001 (for the 206 series) or MA2196, Revision IR, dated March 11, 2004 (for the 207 series), or later FAA approved revisions.
Please contact modification supplier for further details.
STC Status: Amended
STC Date: 27/04/04
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Cessna Aircraft Company
- 206
- 206H
- 207
- 207A
- P206
- P206A
- P206B
- P206C
- P206D
- P206E
- T206H
- T207
- T207A
- TP206A
- TP206B
- TP206C
- TP206D
- TP206E
- TU206A
- TU206B
- TU206C
- TU206D
- TU206E
- TU206F
- TU206G
- U206
- U206A
- U206B
- U206C
- U206D
- U206E
- U206F
- U206G