# STC ST10505SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Enflite Inc.
- Description: Installation of an Enflite Model 42100 Pocket Door between the forward galley and the passenger compartment, without the electric door option installed.
- Status date: May 10, 2019
- Data sheets: T00003NY, T00003NY
- Certificate PDF: https://openairdocs.org/files/sha256/5b/f2/5bf24e3fae48305876aa7f3ee299c4dacb9af7820d83a63bf3c7d87decd45679
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2010BC3139989B24862585CB0038421D.0001
- Page: https://openairdocs.org/stc/ST10505SC

## ADs that name it

None.

## Approved models (2)

- Bombardier Inc. BD-700-1A10 (TCDS T00003NY)
- Bombardier Inc. BD-700-1A11 (TCDS T00003NY)

## 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.

FAA Form 8110-2 (5/14) Page 1 of 2

Number: ST10505SC

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: T00003NY Make: Bombardier, Inc.

Model: BD-700-1A10; BD-700-1A11

Installation of an Enflite Model 42100 Pocket Door between forward galley and passenger compartment, between the aft lavatory and passenger compartment, or in a mid-passenger cabin position, with or without the electric option installed, in accordance with Enflite, Inc., Master Document List MDL42100-1, Rev. X, dated December 31, 2008 or later FAA approved revision.

The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. Installation of this FAA STC is only valid on aircraft that have interior configurations listed in Enflite Inc., Drawing NBR42100-1, Rev. F, dated 9/04/2008 or NBR42100-2, Rev. E, dated 9/04/2008 or later FAA approved revisions.

Door finish requirements are determined by the installer and must not interfere with the emergency egressor decompression requirements. Maximum door assembly weight when installed shall not exceed the requirements defined in Enflite, Inc., drawing number N42100, Rev. K, dated 8/30/2007 or later FAA approved revisions.

Certification Basis:

In accordance with Type Certificate Data Sheet T00003NY, with the additional details defined in FAA Exemption Number 9676 and 14 CFR, FAR 25.981, Amendment 102.

Date of Application: August 15, 2005 Date Reissued: May 10, 2019 Date of Issuance: February 27, 2006 Date Amended: November 16, 2006; February 20, 2009

Signature

Title Jim Grigg Manager, Fort Worth ACO Branch, Compliance & Airworthiness Division Aircraft Certification Service Enflite, LLC 105 Cooperative Way Georgetown, TX 78626

FAA Form 8110-2 (5/14) Page 2 of 2

FAA Form 8110-2 (5/14) Page 2 of 2

Transfer the ownership of Supplemental Type Certificate Number: ST10505SC

To (Name and address of transferee)

From (Name and address of grantor)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SE8628SW

FAA Form 8110-2 (5/14) Page 2 of 2

## Every issue (4)

- May 10, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5b/f2/5bf24e3fae48305876aa7f3ee299c4dacb9af7820d83a63bf3c7d87decd45679)
- February 20, 2009: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/b3/4f/b34fc5efe852ac03492eae1505eac4407c703c14aa499179bc5158f21b2cf7c8)
- November 16, 2006: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/55/6b/556bf9d8491fe02da46c74f9ee0d99801e9471a73d1079ccc66c1743ee5e65d4)
- February 27, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/05/55/0555c3a6e85141b0c8d5c5262948daeb4a545dbfffb1f59a8e909bcbe2326a11)

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