STC ST11161SC

Possession of this Su pplemental Type Certificate (STC) document by persons other than the STC holder does not constitute rights to th e 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: ST11161SC 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: 767-300 A1NM

Installation of an interior reconfiguration from JAL “international” to “domestic” configuration in accordance with “Data List, Installation Data, JAL 767-300 Interior Modification,” document no. DLP368M04, revision IR, dated 11/18/14 or later FAA approved revision; “Airplane Flight Manual Supplement,” document no. P368CT25-03, revision IR, dated 10/29/14 or later FAA approved revision; and “Instructions for Continued Airworthiness for the Interior Reconfiguration in 767-300 Series Aircraft,” document no. P368CT25-05, revision IR, dated 8/28/14, or later FAA accepted revision.

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

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.

Date of Application: August 29, 2014 Date Reissued: March 19, 2018

Date of Issuance: November 18, 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 th e 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: ST11161SC

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 th e 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: ST11161SC

Date Reissued: March 19, 2018

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.

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 767-300 series modified by installing an interior reconfiguration from JAL “international” to “domestic” configuration is as follows:

a. The type certification basis for Boeing 767-300 series airplanes is shown on TCDS A1NM 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), 25.307(a)(d), 25.562, 25.603, 25.605, 25.625(a)(c)(d), 25.787(a)(b), 25.789(a), 25.791(a)(b),

25.793, 25.851(a)(1), (a)(5)-(a)(8), 25.853(a)(c)(d)(e)(h), 25.856(a), 25.1307(c), 25.1431(a)(b)(c)(d), 25.1529,

25.1581(a)(b)(d), 25.1583(h) and 25.1585(a).

Regulations at an intermediate amendment 14 CFR §25.365(g) (amd. 25-54), 25.812(a)(c)(d)(e)(i)(1) (amd. 25-58), 25.869(a)(4) (amd 25-72), and

25.981(a)(3)(b) (amd. 25-102).

The following Tenryu Aero Component seats have been tested to show compliance to 25.561(a)(b)(c)(d) (amd. 25-

64):

401001F0001, Double LH Outboard Seat 401001F0012, Double RH Outboard Seat 401002F0001, Single Center Seat Exemptions from 14CFR part 25 - None

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

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