# STC ST11058SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: VT DRB Aviation Consultants, United States - Description: Installation of an interior reconfiguration from a 2-class configuration to an all economy class configuration - Applied: May 15, 2013 - Status date: March 19, 2018 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) - Certificate PDF: https://openairdocs.org/files/sha256/60/f8/60f8c4393fdcefb2b9afe451d8d1aa14743157c14310f3b85aa5c9cdf2b2fe20 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/CD6762977A48F1DA8625826000458B2F.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST11058SC ## 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. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the S TC 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: ST11058SC 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 a 2-class configuration to an all economy class configuration in accordance with “Data List, Installation Data for, ANA B767-300 Interior Reconfiguration, ODA STC,” document no. DL1873M02, revision IR, dated 2/28/14 or later FAA approved revision; “Instructions for Continued Airworthiness for Airdo Boeing 767-300 Interior Modification”, document no. P369/AED/004, revision A, dated 12/27/13 or later FAA accepted revision; and “Airplane Flight Manual Supplement for Interior Reconfiguration of Boeing 767-300 series,” document no. P369/TST/008, revision IR, dated 2/28/14 or later FAA approved revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. Date of Application: May 15, 2013 Date Reissued: 11/24/14; March 19, 2018 Date of Issuance: February 28, 2014 Date Amended: March 18, 2014 Signature Title VT DRB Aviation Lead ODA Administrator ODA-831473-SW The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the S TC holder. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST11058SC 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 the property of the S TC 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: ST11058SC 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 airplane must be equipped with an adequate capacity of life rafts and approved survival equipment in accordance with §25.1411(d), Amendment 25-32 and §25.1415(b) and (c), Amendment 25-29 in order to conduct extended overwater operations. 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 Boeing 767-300 series modified by installing an interior reconfiguration from a 2-class configuration to an all economy class 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, May 15, 2013, include: Regulations at the latest amendment 25-0 through 25-138 14 CFR §25.305(a)(b), 25.307 (a), 25.625(a)(c), 25.787 (a)(b), 25.789(a), 25.791 (a)(b), 25.851 (a)(1), (a)(5)-(a)(8), 25.853(a), 25.1301 (a), 25.1307(c), 25.1431(a)(b)(c)(d), 25.1529, and 25.1581. Regulations at an intermediate amendment 14 CFR §25.561(a)(b)(c) (amd. 25-64), 25.812 (a)(c)(d)(e)(i)(k) (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 (3) - March 19, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/60/f8/60f8c4393fdcefb2b9afe451d8d1aa14743157c14310f3b85aa5c9cdf2b2fe20) - March 18, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3a/c1/3ac1b47256a2e1846ac463f9f705d7f7ed0dd42c54eaf4672550c8cac27161b2) - February 28, 2014: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/74/c0/74c0cc85d6c1ccac6ac4af83fc0efeb1271a270162fac85f05e5b4b653cf45f7) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.