STC ST11183SC

Number: ST11183SC This certificate issued to: Delta G Design, Inc.

100 Research Pkwy., Suite 3287-B Waco, TX 76704 Part 25 of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: The Boeing Company Model: 747-8 A20WE

Structural and other modifications necessary for the installation of an Otonomy Security System to include a GSM/3G antenna, security camera and associated components and wiring onto a Boeing 747-8 BBJ aircraft in accordance with MDL DGD-SS03-MD-01, Rev. C, dated January 29, 2016, or later FAA-approved revision.

Maintenance procedure to be conducted in accordance with ICA document DGD-SS03-IC-01, Rev. IR, dated July, 2014, or later FAA-approved revision.

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. This certificate is for structural provisions only. EMI and functional testing is required as part of a separate approval when associated component parts are installed.

(see continuation sheet 3 0f 3)

Date of Application: July 13, 2012 Date Reissued:

Date of Issuance: December 19, 2014 Date Amended: March 26, 2019

Signature

Title Jim Grigg Manager, Fort Worth ACO Branch Compliance & Airworthiness Division Aircraft Certification Service

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

FAA Form 8110-2 (5/14) Page 1 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST011183SC

To (Name and address of transferee)

From (Name and address of grantor)

This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST011183SC FAA Form 8110-2 (5/14) Page 3 of

Note: 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.

Certification Basis: Based on 14 CFR § 21.115 and 21.101(b)(1) and FAA Order 8110.48, the certification basis for the listed models of Boeing 747-8 aircraft modified by the installation of an Otonomy Security System is as follows:

a. The type certification basis for the Boeing 747-8 airplane is shown on TCDS A20WE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, July 13, 2012, is based upon part 25 as amended by Amendment 25-120.

Based on 14 CFR § 21.115 and 21.101(b)(1) and FAA Order 8110.48, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-120 14 CFR § 25.23, 25.301(a)(b), 25.303, 25.305(a)(b), 25.307(a), 25.365(a)(b), 25.371 (a)(b), 25.581, 25.601,

25.603, 25.605(a), 25.609, 25.613(a)(b), 25.625(a), 25.981, 25.1307, 25.1351, 25.1355, 25.1357, 25.1359,

25.1431, 25.1519, 25.1351, 25.1519, 25.1529, 25.1541, 25.1351

Regulations at an intermediate amendment None

Regulations at the amendment level in TCDS A20WE 14 CFR § 25.611. 25.869(a), 25.899, 25.1301, 25.1309, 25.1360, 25.1703, 25.1707, 25.1709, 25.1711,

25.1713, 25.1715. 25.1717. 25.1719, 25.1721, 25.1729 Amendment 25-123

14 CFR Part 26 Regulations Based on 14 CFR § 21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis.

For any future 14 CFR part 26 amendments, the holder of this amended STC must demonstrate complianc e with the applicable sections. As of the issuance date of this amended STC, compliance has been found for the following regulations: 14 CFR § 26.47(c) Amendment No. 26-0 through 26-1

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This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21. 47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST011183SC FAA Form 8110-2 (5/14) Page 4 of

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST011183SC FAA Form 8110-2 (5/14) Page 5 of