# STC ST10915SC

- 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: December 11, 2017
- Data sheets: A16WE
- Certificate PDF: https://openairdocs.org/files/sha256/5d/e0/5de065a32313f4fdd6c5c696ed0d5cf9caf23cf3ff1db2116f15025f4f9b4124
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174025934720230417145637.0001
- Page: https://openairdocs.org/stc/ST10915SC

## 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

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

ST10915SC Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 25 A16WE Boeing 737-700 Installation of an Executive Interior in accordance with Associated Air Center (AAC) "Master Document List" Document Number 3143000000, Revision IR, dated March 1, 2014, or later FAA/ODA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 3143021090, Revision IR, dated March 1, 2014, or later FAA/ODA approved revision is required.

Descriptive data about this design change can not be used to duplicate other products. This approval is limited to only the installation made in Boeing Model Number 737-700, Serial Number 30496. This STC does not permit manufacturing of parts for multiple installations.

7/31/2013 3/1/2014 12/11/2017 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):

ST10915SC

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

ST10915SC Airworthiness limitation inspections per 14 CFR Part 25, Appendix H, are contained in Chapter 3 of AAC Document Number 3143050090, Revision IR, dated December 18, 2013, titled “Instructions for Continued Airworthiness” or later FAA/ODA approved revision.

Certification Basis: The same as that identified on Type Certificate Data Sheet A16WE except for the election of later amendments as listed:

Fuel ignition prevention: 25.981 (a)(3)(b) Amdt. 25-102

System lighting protection: 25.1316 (b)(c)(6) Amdt. 25-80

## Every issue (2)

- December 11, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5d/e0/5de065a32313f4fdd6c5c696ed0d5cf9caf23cf3ff1db2116f15025f4f9b4124)
- March 1, 2014: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/2a/6f/2a6f09f7421ccb61310dcaf076e44cab8e40f7d4b52317c9a546491ec8e8b563)

---
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.