STC SA2781NM-D

Supplemental type certificate · United Airlines Inc

Holder
United Airlines Inc · United States
Status
Current · Reissued
Status date
November 30, 2011
Applied
October 12, 1990
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA20WE

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

What it approves

Replace first, business, and coach class seats. Change the seat count from 37F-62C-144Y to 18F-62C-164Y. New first class seats utilize electric footrests. New business class seats seat seven across. Relocate the crew bunkhouse from zone B to zone D. Install five new class dividers and a nose closet. Install video monitors, pods and screens at specific locations. This installation is in accordance with United Air Lines DAS-1-WE, Approved Drawing List No. 2781 dated November 6, 1990, or later FAA approved revision.

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. * Ref. Type Certificate Data Sheet A20WE for Special Conditions Original Product Type Certificate Number :

A20WE

Boeing

747SP Series Description of Type Design Change: Replace first, business, and coach class seats. Change the seat count from 37F-62C-144Y to 18F-62C-164Y. New first class seats utilize electric footrests.

New business class seats seat seven across. Relocate the crew bunkhouse from zone B to zone D. Install five new class dividers and a nose cl oset. Install video monitors, pods and screens at specific locations. This installation is in accordance with United Air Lines DAS-1-WE, Approved Drawing List No. 2781 dated November 6, 1990, or later FAA approved revision.

Limitations and Conditions: This approval does not extend 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: October 12, 1990

Date of issuance: November 6, 1990

Date reissued: November 30, 2011

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

NOTE:

DO NOT DELETE THIS PAGE.

DO NOT ADD ANY DATA TO THIS PAGE.

THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.

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 Company747SP SeriesA20WE