# STC ST00005LB-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: United Airlines Inc, United States
- Description: Install curtains around three passenger seats directly forward of door 3 right hand side.  Also, install placards for the curtains.  The curtains consist of a forward transverse curtain, the longitudinal curtain and the aft transverse curtain.  The curtains are attached to PSU panel, sidewalls and curtain tracks.  This modification was accomplished in accordance with United Air Lines, DAS-1-WE, Approved Master Drawing List No. 00005 dated May 19, 1995, or later FAA approved revisions.
- Applied: April 3, 1995
- Status date: November 30, 2011
- Product: Aircraft, Large Multi-Engine
- Certification basis: Part 21, Part 25
- Data sheets: [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE)
- Certificate PDF: https://openairdocs.org/files/sha256/56/6e/566e7b8612884b4305e89c45154e88734cee24c4820028476eb51395c9082dd1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DA3B62DE84D003558625799500660DC1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00005LB-D

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 777-200 Series ([TCDS T00001SE](https://openairdocs.org/tcds/T00001SE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can 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 T00001SE for Special Conditions Original Product Type Certificate Number :

T00001SE

Boeing

777-200 Series Description of Type Design Change: Install curtains around three passenger seats directly forward of door 3 right hand side. Also, install placards for th e curtains. The curtains consist of a forward transverse curtain, the longitudinal curtain and the aft transverse curtain. The cu rtains are attached to PSU panel, sidewalls and curtain tracks. This modification was accomplished in accordance with United Air Lines, DAS-1-WE, Approved Master Drawing List No. 00005 dated May 19, 1995, or later FAA approved revisions.

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 a ffect upon the airworthiness of that aircraft.

This determination should include consideration of significant change 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: April 3, 1995

Date of issuance: May 19, 1995

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.**

## Every issue (1)

- November 30, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/56/6e/566e7b8612884b4305e89c45154e88734cee24c4820028476eb51395c9082dd1)

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