STC ST11167SC

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST11167SC This certificate issued to: VT DRB Aviation Consultants 9800 John Saunders Road San Antonio, TX 78216

Part _25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Boeing Model: 737-700 A16WE

Installation of an executive style interior in accordance with “Data List, Installation Data, Aeria, P8052.BBJ.0713S-P1” document no. DL1900M09, revision E, dated 12/15/15 or later FAA approved revision; “Instructions for Continued Airworthiness for the Installation of a VIP Interior in Boeing 737-700IGW (BBJ) Series Aircraft,” document no.

8052CT25-03, revision A, dated 11/19/15 or later FAA accepted revision; and, “Airplane Flight Manual Supplement,” document no. 8052CT25-01, revision IR, dated 12/10/15 or later FAA approved revision.

1. The installer must determine whether this design change is compatible with previously approved modifications.

Date of Application: August 29, 2014 Date Reissued: 12/17/15; March 19, 2018

Date of Issuance: December 16, 2015 Date Amended:

Signature

Title VT DRB Aviation Lead ODA Administrator ODA-831473-SW

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

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

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST11167SC

To (Name and address of transferee)

From (Name and address of grantor)

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11167SC

Date Reissued: March 19, 2018

2. 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.

3. 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.

4. STCs ST11121SC, “Structural Modification for the installation of EMS AMT-3800 SATCOM antenna,” ST01635LA, “Installation of Cabin Interior Noise Reduction Kit,”, ST01568LA, “Installation of Aft Wing Fairing Acoustic Treatment Kit,” and ST01716NY-D, “Installation of an Auxiliary Fuel System,” must be installed prior to installation.

5. Modification does not support Part 121 operations as compliance to 14CFR 25.562(c) has not been fully evaluated.

Certification Basis:

Based on 14 CFR §§21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Boeing 737-700 aircraft modified by installing an executive style VIP interior is as follows:

a. The type certification basis for Boeing 737-700 series airplanes is shown on TCDS A16WE 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, August 29, 2014, include:

Regulations at the latest amendment 25-0 through 25-138 14 CFR §25.305(a)(b), 25.561(a)(b)(c), 25.856(a), 25.857(c), 25.899(a)(b), 25.1439(a)(b) and 25.1585(a).

Regulations at an intermediate amendment 14 CFR §25.571(a) amd 25-72 & (b) amd 25-86, 25.807(d) amd 25-72, 25.855(a)(b)(c)(d)(h)(3) amd 25-93, and

25.981(a)(3)(d) amd 25-125.

Exemptions from 14CFR part 25 - None

Equivalent safety findings exist with respect to the following regulations - None

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