Installation of vortex generators on wings and tail surfaces in...
Overview
Introduction
Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156, Revision IR, dated April 18, 2001, and Installation Manual MA2157, Revision IR, dated July 3, 2001, or later FAA approved revision to either of these documents. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.
Product Description
Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156, Revision IR, dated April 18, 2001, and Installation Manual MA2157, Revision IR, dated July 3, 2001, or later FAA approved revision to either of these documents. 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: 17/07/01
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Cessna Aircraft Company
- 210G
- 210H
- 210J
- 210K
- 210L
- 210M
- 210N
- P210N
- T210G
- T210H
- T210J
- T210K
- T210L
- T210M
- T210N