STC SA5639NM-D

Supplemental type certificate · United Airlines Inc

Holder
United Airlines Inc · United States
Status
Current · Reissued
Status date
November 30, 2011
Applied
December 10, 1991
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA22WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Install a new G-3 Galley in place of the divider/partition unit and a new F/C closet in zone A. Installation of new centerline overhead stowbins and new aisle lighting structure. All zones have interior décor upgrade. The seating configuration of the aircraft will become 38 F/C + 260 Y/C for total seating capacity of 298 passengers.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

This Certificate issued to United Air Lines, Inc.

600 Jefferson Street Houston, Texas 77002

Part 25 of the Federal Aviation Regulations. See Type Certificate Data Sheet A22WE for Special Conditions.

A22WE

Boeing

DC-10-10 series Description of Type Design Change: Install a new G-3 Galley in place of the divider/partition unit and a new F/C closet in zone A. Installation of new centerline overhead stowbins and new aisle lighting structure. All zones have interior d écor upgrade. The seating configuration of the aircraft will become 38 F/C + 260 Y/C for tota l seating capacity of 298 passengers. This modification was accomplished in accordance with United Air Lines, DAS-1-WE, Approved Master Drawing List No. 5639 dated September 2, 1992, or later FAA approved revisions.

Limitations and Conditions: This approval should not extended to other aircraft of this model on which other previously approved modifications ar e incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse e ffect upon the airworthiness of that aircraft.

This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight in the fuselage. If the holder agrees to permit another person to use this certificate to alter th e product, the holder shall give the other person written evidence of that permission.

This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: December 10, 1991

Date of issuance: September 2, 1992

Date reissued: November 30, 2011

( Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office ( Title)

NOTE:

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ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 1

MakeModelData sheet
The Boeing CompanyDC-10-10A22WE