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Modification to the flap control system to provide a maximum...

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

Overview

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Introduction

Modification to the flap control system to provide a maximum landing flap of 40 degrees in the norma
McDonnell Douglas DC9
€ RFQ

Product Description

Modification to the flap control system to provide a maximum landing flap of 40 degrees in the norma

Please contact modification supplier for further details.

STC Status: Surrendered
STC Date: 02/12/14
Responsible Office: