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Modification in the leading edge slat and flap configurations

Structure (ATA 51-57)
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Overview

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Introduction

Modification in the leading edge slat and flap configurations
Boeing 727
€ RFQ

Product Description

Modification in the leading edge slat and flap configurations

Please contact modification supplier for further details.

STC Status: Amended
STC Date: 23/03/99
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400

Boeing Company, The

  • 727-200 Series