# STC ST10531SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Associated Air Center, Inc. - c/o CT Corporation System
- Description: Installation of an Executive Interior
- Status date: January 23, 2018
- Data sheets: A16WE
- Certificate PDF: https://openairdocs.org/files/sha256/98/7c/987cfe49bdf42ccb26bff0375e1e622bd2c640be15094e0b8166e8c1140b688b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101150380620230428164326.0001
- Page: https://openairdocs.org/stc/ST10531SC

## ADs that name it

None.

## Approved models (1)

- The Boeing Company 737-700 Series (TCDS A16WE)

## 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 (8/13) Page 1 Number:

Part of the Federal Av iation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

By direction of the Administrator Signature Title ST10531SC Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 25 A16WE Boeing 737-7N6

Installation of an Executive Interior in accordance with the Associated Air Center (AAC) "Master Document List" Document Number, 2335000000, Revision A, dated May 3, 2006, or later FAA approved revision. Airplane Flight Manual Supplement (AFMS) Document Number 2335021090, Revision IR, dated May 2, 2006, or later FAA approved revision is required.

Descriptive data pertaining to this design change are considered inadequate for duplication in other products. This approval is limited to only the installation made in Boeing Model 737-7N6, Serial Number 34260. This STC does not permit manufacturing parts for multiple installations. Airworthiness limitation inspections per 14 CFR Part 25, Appendix H are contained in AAC document number 2335050090, Revision C, dated May 3, 2006, titled "Instructions for Continued Airworthiness, Chapter 3. The cockpit door assembly installed in this aircraft is not certified to the ballistic requirements of 14 CFR Part 25.795 due to the addition of decorative coverings to the door and its surroundings. Ballistic door certification for this STC is not required as this aircraft has a limitation not to be operated for hire or common carriage.

6/20/2005 5/3/2006 1/23/2018 Jose Mora-Vargas ODA Administrator ODA-710437-SW

FAA Form 8110-2 (8/13) Page 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

ST10531SC

FAA Form 8110-2 (8/13) Page 3

ST10531SC Certification Basis:

The certification basis for the Supplemental Type Certificate (STC) is the same as that identified on Type Certificate Data Sheet (TCDS) A16WE with the elected addition of Exemption Number 6820 and 6820A plus compliance with 14 CFR FAR Part

25.981, amendment number 102.

END

## Every issue (2)

- January 23, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/98/7c/987cfe49bdf42ccb26bff0375e1e622bd2c640be15094e0b8166e8c1140b688b)
- May 3, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/55/4b/554bef74226f67084266402c54fec21489c1efcaa00b143c06e7bc0330d97063)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.