# STC ST10902SC-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Associated Air Center, Inc. - c/o CT Corporation System, United States
- Description: Installation of an Executive Interior
- Applied: February 11, 2008
- Status date: December 11, 2017
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE)
- Certificate PDF: https://openairdocs.org/files/sha256/fd/c4/fdc4318a425e33e7fba57bef5deff85b4e0bb178dd4776aa9b604c41b67e015c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182184042420230417143025.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST10902SC-D

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 737-700 Series ([TCDS A16WE](https://openairdocs.org/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

ST10902SC-D 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 2546000000, Revision B, dated November 30, 2017, or later FAA/ODA approved revision.

Airplane Flight Manual Supplement (AFMS), Document Number 2546021090, Revision IR, dated September 21, 2010, 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 36090. This STC does not permit manufacturing of parts for multiple installations.

2/11/2008 9/21/2010 12/11/2017 5/10/2011 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):

ST10902SC-D

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

ST10902SC-D Limitations and Conditions (Continued):

Airworthiness limitation inspections per 14 CFR Part 25, Appendix H, are contained in Chapter 3 of AAC Document Number 2546050090, Revision D, dated January 12, 2011 titled “Instructions for Continued Airworthiness” or later FAA/ODA approved revision.

The FAA has reviewed the applicant's assessment showing that this modification does not impact the existing Electrical Wiring Interconnection System Instructions for Continued Airworthiness (EWIS ICA) and found that no additional EWIS ICA tasks are required. Refer to Report No. 2878052091 "EWIS ICA Evaluation", Revision A, dated January 21, 2011, 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: 14 CFR 25.321(c)(d) Amdt. 25-86; 25.811(a)(b)(c)(d)(1)(2)(3) (e)(1)(2)(4)(f)(1)(2)(3)

(g) Amdt 25-88; 25.842(c) Amdt 25-116; 25.853(h) Amdt 25-83; 25.853(a) Amdt 25-116; 25.981(a)(3)(b) Amdt 25-102; and 25.1423(c) Amdt 25-115.

END

## Every issue (3)

- December 11, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fd/c4/fdc4318a425e33e7fba57bef5deff85b4e0bb178dd4776aa9b604c41b67e015c)
- May 10, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/9b/3e/9b3e0a20eea140ce74f2a16d204cd935bc29e4d4f73d1054be5b97077258955f)
- September 21, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/9f/27/9f273bc5b548b899122870119ab400197700e37659a21c8a61610935a7c63be2)

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