STC ST10899SC-D

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

Part of the Federal A viation Regulations.

Original Product – Type Certificate Number: MDNH:

MRGHO:

Signature

Title

ST10899SC-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 2603000000, Revision B, dated April 26, 2013, or later FAA/ODA approved revision. Airplane Flight Manual Supplement (AFMS), Document Number 2603021090, Revision A, dated April 26, 2013, 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 37111. This STC does not permit manufacturing of parts for multiple installations.

9/30/2008 2/10/2010 12/11/2017 4/26/2013 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):

ST10899SC-D

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

ST10899SC-D Limitations and Conditions (Continued):

This aircraft is not to be operated for hire or offered for common carriage. Airworthiness limitation inspections per 14 CFR Part 25, Appendix H, are contained in Chapter 3 of AAC Document Number 2603050090, Revision C, dated July 24, 2010 titled “Instructions for Continued Airworthiness” or later FAA approved revision.

This STC incorporates the use of Exemption Numbers 6820 and 6820A.

Note: For STC ST10911SC amendment approved January 28, 2013, 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.

Reference AAC Report No. 2828052091 "EWIS ICA Evaluation", Revision IR dated March 7, 2013, 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:

Initial STC dated February 10, 2010:

Flight Loads, General - 25.321(c),(d) Amdt. 25-86 Damage Tolerance and Fatigue Evaluation of Structure - 25.571(a),(b) Amdt. 25-96 Compartment Interiors - 25.853(a),(c) Amdt. 25-116 Cargo or Baggage Compartment Smoke or Fire Detection Systems - 25.858 Amdt. 25-93 Fuel Tank Ignition Prevention - 25.981(a)(3),(b) Amdt. 25-102 System Lightning Protection - 25.1316(b),(c)(6) Amdt. 25-80

STC Amendment dated April 26, 2013:

Flight Loads, General - 25.321(c),(d) Amdt. 25-86 Gust and Turbulence Load - 25.341 (b) Amdt. 25-86 Ditching - 25.801 (a) Amdt. 25-88 Emergency Exit Marking - 25.811 (d)(1) Amdt. 25-88 Electrical Equipment and Installations - 25.1353 (a),(b) Amdt. 25-113 Safety Equipment, General - 25.1411 - (f) Amdt. 25-79 Ditching Equipment - 25.1415 - (a),(b),(e) Amdt. 25-82 Operating Limitations - 25.1583 (h) Amdt. 25-105

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