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Approval of maximum zero fuel weight increase (155,000 lbs.) and...

Aircraft General (ATA 5-18) Airframe Systems (ATA 20-50)
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Overview

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Introduction

Approval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data pertaining to this modification are considered inadequate for duplication in other aircraft.This approval is limited to the installation in the Boeing 727-200, (Serial Number 20938 only).
Boeing 727
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Product Description

Approval of maximum zero fuel weight increase (155,000 lbs.) and maximum landing weight increase(164,000 lbs.). Data pertaining to this modification are considered inadequate for duplication in other aircraft.This approval is limited to the installation in the Boeing 727-200, (Serial Number 20938 only).

Please contact modification supplier for further details.

STC Status: Reissued
STC Date: 20/01/05
Responsible Office: Los Angeles Aircraft Certification Office (ANM-100L), Tel: (562) 627-5200

Boeing Company, The

  • 727-200 Series