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Installation of vortex generators on the wing leading edge, underside...

Airframe Systems (ATA 20-50) Structure (ATA 51-57)
Overview Product description

Overview

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Introduction

Installation of vortex generators on the wing leading edge, underside of the horizontal stabilizer, and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117, Revision IR, dated July 14, 1999, and Installation Instructions MA2118, Revision IR, dated September 21, 1999, or later FAA approved revisions to either of these documents.NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy
Piper PA-23
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Piper PA-28
€ RFQ

Product Description

Installation of vortex generators on the wing leading edge, underside of the horizontal stabilizer, and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117, Revision IR, dated July 14, 1999, and Installation Instructions MA2118, Revision IR, dated September 21, 1999, or later FAA approved revisions 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: Amended
STC Date: 27/04/04
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400

Piper Aircraft, Inc., The New

  • PA-23
  • PA-23-160