Supplemental type certificate · United Airlines Inc

Holder
United Airlines Inc · United States
Status
Current · Reissued
Status date
November 30, 2011
Applied
November 15, 1996
Product
Aircraft · Large Multi-Engine
Certification basis
Part 21, Part 25
Data sheet
TCDSA16WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Reconfiguration of interior arrangement per U. S. Technical Consultants Master Control List 2403-25-000, Revision NC, dated March 4, 1997. Master Control List 2403-25-000, Revision A, dated April 15, 1997. Master Control List 2403-25-000, Revision B, dated August 8, 1997, or later FAA approved revisions; and as revised by United Air Lines Master Document List No. 00283, Revision Original, dated August 23, 2003, or later FAA approved revisions.

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. TC Data Sheet A16WE for Special Conditions.

A16WE

Boeing

737-322, 737-522 Description of Type Design Change:

Reconfiguration of interior arrangement per U. S. Technical Consultants Master Control List 2403-25-000, Revision NC, dated March 4, 1997.

Master Control List 2403-25-000, Revision A, dated April 15, 1997.

Master Control List 2403-25-000, Revision B, dated August 8, 1997, or later FAA approved revisions;

and as revised by United Air Lines Master Document List No. 00283, Revision Original, dated August 23, 2003, or later FAA approved revisions.

Limitations and Conditions: This approval should not be incor porated on any certificated product on which approved modifications are incorporated, unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the certified product. A copy of this STC must be included in the permanent records of the modified aircraft. All of the above interior furnishings meet the flammability requirements of 14 CFR

25.853(a) Amendment 32), the heat release requirement s (65/65) and optical smoke density (200) for 14 CFR 25.853(a-1) (Amendment 66) for 737-522 aircraft. If the holder agrees to permit another person to use this certificate to alter the 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: November 15, 1996

Date of issuance: March 5, 1997

Date reissued: June 4, 2002; November 22, 2002; September 19, 2003; November 30, 2011

Date amended: April 15, 1997; August 8, 1997

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

Number ST00283LA-D

Date of Issuance: March 5, 1997 Date Amended: April 15, 1997; August 8, 1997

The following 737-322 series number aircraft are eligible for this STC:

23642-23644, 23665-23675, 23947-23957, 24147-24149, 24191-24193, 24228-24230, 24240-24253, 24301, 24319-24321, 24360-24362, 24378, 24379, 24452-24455, 24532-24540, 24637-24642, 24653-24673, 24653-24674, 24717-24718

The following 737-522 serial number aircraft are eligible for this STC:

25254, 25255, 25290, 25291, 25381-25388, 26642, 26643, 26645, 26646, 26648, 26649, 26651, 26652, 26655, 26656, 26658, 26659, 26662

- END -

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 · 2

MakeModelData sheet
The Boeing Company737-300 SeriesA16WE
The Boeing Company737-500 SeriesA16WE