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Increase in aircraft operating weights (Maximum landing weight to 265000...

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

Overview

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Introduction

Increase in aircraft operating weights (Maximum landing weight to 265000 lbs and maximum zero fuel weight to 241500 lbs).

Product Description

Increase in aircraft operating weights (Maximum landing weight to 265000 lbs and maximum zero fuel weight to 241500 lbs).

Please contact modification supplier for further details.

STC Status: Surrendered
STC Date: 01/12/09
Responsible Office: Atlanta Aircraft Certification Office (ACE-115A), Tel: (404) 474-5500

McDonnell Douglas Corporation

  • DC-8-62F