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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

STC Number
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STC Date
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Contact Details
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Introduction

Modification to the flap control system to provide a maximum landing flap of 40 degrees in the normal case and an optional stop in the flap position quadrant to restrict the full landing position to 40 degrees.
DC9
€ RFQ

Product Description

Please contact modification supplier for further details.

STC Status: Reissued
STC Date: 10-11-1991
Responsible Office: Chicago Aircraft Certification Office (ACE-115C), Tel: (847) 294-7358

McDonnell Douglas Corporation

  • DC-9-30 Series