# STC ST10916SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Associated Air Center, Inc. - c/o CT Corporation System, USA
- Description: Installation of an Executive Interior
- Applied: April 4, 2012
- Status date: December 11, 2017
- Product: Aircraft, Large Airplane
- Certification basis: Part 25
- Data sheets: [TCDS A46NM](https://openairdocs.org/tcds/A46NM)
- Certificate PDF: https://openairdocs.org/files/sha256/7a/df/7adfe2b36668ed4b1844cf956ed6a45cba7258c1528a7bc6da8c6d048e5bb13a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID129461840020230417145822.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST10916SC

## ADs that name it (0)

None.

## Approved models (1)

- Airbus SAS A330-243 ([TCDS A46NM](https://openairdocs.org/tcds/A46NM))

## 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

ST10916SC Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 25 A46NM Airbus A330-243 Installation of an Executive Interior in accordance with Associated Air Center (AAC) "Master Document List" Document Number 3007000000, Revision B, dated August 13, 2015, or later FAA/ODA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 3007021090, Revision A, dated June 30, 2015, or later FAA/ODA approved revision is required.

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.

4/4/2012 6/5/2014 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):

ST10916SC

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

ST10916SC Limitations and Conditions (Continued):

Airworthiness limitation inspections per 14 CFR Part 25, Appendix H are contained in Chapter 3 of AAC Document Number 3007050090, Revision B, dated April 28, 2014, titled "Instructions for Continued Airworthiness" or later FAA/ODA approved revision.

The Cabin Wireless Local Area Network (WLAN) system is intended to provide internet connection and e-mail services using portable electronic devices (PEDs.) Any other intended function of this equipment will require a re-examination of the certification basis.

Certification Basis: The same as that identified on Type Certificate Data Sheet A46NM, except for the election of later amendments as listed.

Strength and deformation: 25.305 (a)(b)(c) Amdt. 25-86 (galleys) Emergency Landing Conditions, General: 25.561 Amdt. 25-91 (galleys) Mat strength properties and design values: 25.613 Amdt. 25-112 (galleys) Compartment interiors: 25-853 (a)(c) 25-116 (seat material fire blocking) Thermal/acoustic insulation materials: 25-856 (a) 25-111 Fuel ignition prevention: 25-981 Amdt. 25-102 System lightning protection: 25-1316 (b)(c) Amdt. 25-80

END

## Every issue (1)

- December 11, 2017: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/7a/df/7adfe2b36668ed4b1844cf956ed6a45cba7258c1528a7bc6da8c6d048e5bb13a)

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