STC ST11127SC

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: ST11127SC 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 to be operated as part of an Air Canada Leisure Carrier Fleet in accordance with “Data List – Installation, ACN, 767-300, LCF Modification,” document no. DL1880M04, revision IR, dated 3/14/14 or later FAA approved revision; “Airplane Flight Manual Supplement for interior reconfiguration of Boeing 767-300 series,” document no. 1880CT25-03, revision IR, dated March 14, 2014 or later FAA approved revision; and, “Instructions for Continued Airworthiness for the Interior Reconfiguration in Boeing 767-300 Series Aircraft,” document no. 1880CT25-05, revision A, dated 3/7/14, or later FAA accepted revision.

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

Date of Application: June 21, 2013 Date Reissued: 3/18/14; March 19, 2018

Date of Issuance: March 14, 2014 Date Amended: 11/17/14; January 23, 2015

Signature

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

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: ST11127SC

To (Name and address of transferee)

From (Name and address of grantor)

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: ST11127SC

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. This airplane may not be used for FAA Part 121 operations, unless modified to meet Special Condition 25- 369-SC.

5. When “Data List, Design Data, ACN, Rouge, 767-300 Series “D” Group,” document no. DL1913M01, revision N, dated January 22, 2015, or later FAA approved revision is installed, STC ST02392LA is 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 to be operated as part of an Air Canada Leisure Carrier Fleet 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, June 21, 2013, include:

Regulations at the latest amendment 25-0 through 25-138 14 CFR §25.305(a)(b), 25.307(a), 25.603, 25.605(a), 25.625(a)(c)(d), 25.787(a)(b), 25.789, 25.791(a)(b), 25.793,

25.851(a)(1), (a)(5)-(a)(8), (b)(2), 25.853(a)(c)(d)(h), 25.854(a)(b), 25.1307(c), 25.1431(a)(b)(c)(d), 25.1529, and

25.1581.

Regulations at an intermediate amendment 14 CFR §25.365 (g) (amd. 25-54), 25.613(a)(b) (amd. 25.46), 25.812(a)(e) (amd. 25.58), 25.869(a)(4) (amd 25-72), and 25.981(a)(3), (b) (amd. 25-102).

Exemptions from 14CFR part 25 - None

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

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