Installation of vortex generators on the wings and tail surfaces...
Overview
Introduction
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2178, Revision IR, dated January 17 2003, and Installation Manual MA2179, Revision IR, dated February 24, 2003, or later FAA approved revision to either of these documents.NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.
Product Description
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2178, Revision IR, dated January 17 2003, and Installation Manual MA2179, Revision IR, dated February 24, 2003, or later FAA approved revision to either of these documents.NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.
Please contact modification supplier for further details.
STC Status: Issued
STC Date: 21/03/03
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Cessna Aircraft Company, The
- 210
- 210-5 (205)
- 210-5A (205A)
- 210A
- 210B
- 210C
- 210D
- 210E
- 210F
- T210F