Overview

STC Number
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Contact Details
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Introduction

Installation of vortex generators on the wing and vertical stabilizer and 'split flaps', mounted on the lower trailing edge of the flaps


Piper PA-34 Seneca
€ RFQ

Product Description

Installation of vortex generators on the wing and vertical stabilizer and 'split flaps', mounted on the lower trailing edge of the flaps

Please contact modification supplier for further details.

STC Status: Amended
STC Date: 12/08/94
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400

Piper Aircraft, Inc.

  • PA-34-200T
  • PA-34-220T