STC ST11163SC

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: ST11163SC 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: Airbus Model: 320-232 (S/N 4388 only) A28NM

Installation of G1 and G5 galleys in accordance with “Data List, Compliance Data, Volant, A320 Galley,” document no. DL1899M00, revision F, dated 12/16/14 or later FAA approved revision; “Instructions for Continued Airworthiness,” document no. 1899CT25M02, revision F, dated 12/11/14; and, “Instructions for Continued Airworthiness,” document no. 1899CT25M03, revision F, dated 12/11/14 or later FAA accepted revision.

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

2. STC ST03394NY must be installed prior to installation.

3. 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.

Date of Application: August 29, 2014 Date Reissued: 2/3/15; 3/30/15; March 19, 2018

Date of Issuance: December 23, 2014 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: ST11163SC

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: ST11163SC

Date Reissued: March 19, 2018

4. 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, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Airbus 320-232 aircraft modified by installing G1 and G5 galleys is as follows:

a. The type certification basis for Airbus 320-232 series airplanes is shown on TCDS A28NM 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 §25.29(a)(b), 25.305(a)(b), 25.307(a), 25.561(a)(b)(c), 25.613(a)(b), 25.625, 25.853(a)(d3)(e)(h), 25.856(a),

25.1307(c), 25.1309(a)(b)(d), 25.1351(a1), 25.1353(a), 25.1431(c)(d), and 25.1529.

Regulations at an intermediate amendment 14 CFR § 25.981 (amd. 25-102).

Exemptions from 14CFR part 25 - None

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

-------------- END -------------