STC ST10913SC

FAA Form 8110-2 (8/13) Page 1

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

ST10913SC Associated Air Center, Inc. - c/o CT Corporation System 1999 Bryan Street, Suite 900 Dallas, TX 75201 25 A28NM Airbus A319-133 Installation of an Executive Interior in accordance with Associated Air Center (AAC) "Master Document List" Document Number 2925000000, Revision G, dated May 3, 2016 or later FAA/ODA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 2925021090, Revision D, dated September 23, 2015 or later FAA/ODA approved revision is required.

Airworthiness limitation inspections per 14 CFR Part 25, Appendix H, are contained in Chapter 3 of AAC Document Number 2925050090, Revision K, dated April 12, 2016, titled “Instructions for Continued Airworthiness” or later FAA/ODA approved revision.

12/29/2011 11/16/2012 12/11/2017 11/17/2014 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):

ST10913SC

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

ST10913SC Limitations and Conditions (Continued):

Compatibility of this design change with previously approved modifications must be determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. The items identified in the AAC Document “Commercial Off The Shelf (COTS) and Nonessential Equipment Summary” Document Number 2925250197, Revision B, dated October 30, 2012, are considered inadequate for duplication and is limited to aircraft Serial Number 4992 only.

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

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. 2925052091, Revision A, dated April 12, 2016 , "EWIS ICA Evaluation", and Report No. 3088052091, Revision A, dated April 12, 2016 "EWIS ICA Evaluation", or later FAA/ODA approved revisions.

This airplane configuration takes advantage of Exemption No. 7489 (reference TCDS A28NM Rev. 11 dated September 7, 2010.)

Certification Basis: The same as that identified on Type Certificate Data Sheet A28NM except for the election of later amendments as listed:

Lavatory Fire Protection: 25.854 (a) Amdt. 25-74 Cargo or Baggage Compartments: 25.855 (c)(d) Amdt. 25-123 Fuel Ignition Prevention: 25.981 (a)(3)(b) Amdt. 25-102 System Lighting Protection: 25.1316 (b)(c)(6) Amdt. 25-80

END