# STC ST11128SC

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: VT DRB Aviation Consultants, United States
- Description: Installation of an interior reconfiguration to be operated as part of an Air Canada Leisure Carrier Fleet
- Applied: March 18, 2014
- Status date: March 19, 2018
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 25, Part 121
- Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM)
- Certificate PDF: https://openairdocs.org/files/sha256/58/3e/583ece7995316f21afd0acdf6f3bf5350639f5d7d80876222c3edd4f6707c81c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/37E16DE32A2424D38625826000458B7F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/ST11128SC

## ADs that name it (0)

None.

## Approved models (1)

- The Boeing Company 767-300 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST11128SC 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 Data, STASG, ACN, 767-333, S/N 25586,” document no. DL1898M04, revision IR, dated 3/25/14 or later FAA approved revision; “Airplane Flight Manual Supplement for interior reconfiguration of Boeing 767-300 series,” document no. 1880CT25-03, revision A, dated March 26, 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 B, dated 3/14/14, or later FAA accepted revision.

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

Date of Application: March 18, 2014 Date Reissued: March 19, 2018

Date of Issuance: March 26, 2014 Date Amended:

Signature

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

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

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST11128SC

To (Name and address of transferee)

From (Name and address of grantor)

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: ST11128SC

Date Reissued: March 19, 2018

2. You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Boeing Model 767-333 Serial No. MSN 25586. This STC does not permit manufacturing of parts for multiple installations.

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.

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, March 14, 2014, 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)(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

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

## Every issue (2)

- March 19, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/58/3e/583ece7995316f21afd0acdf6f3bf5350639f5d7d80876222c3edd4f6707c81c)
- March 26, 2014: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/23/0b/230bae0223fdac74a82e998f668211928460db24f8732f9f0012cb78e2604ed4)

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