# STC ST11212SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: VT DRB Aviation Consultants - Description: One-time installation of an executive interior - Status date: March 19, 2018 - Data sheets: T00001SE - Certificate PDF: https://openairdocs.org/files/sha256/dd/1c/dd1c0e5e6994faa953ff71779245464b4ea9b3206eca453472472da6d1b593ae - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9A6B1F04CFA05A678625826000458BA6.0001 - Page: https://openairdocs.org/stc/ST11212SC ## ADs that name it None. ## Approved models (1) - The Boeing Company 777-200 Series (TCDS T00001SE) ## 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. 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, ai rcraft engine, or propeller. FAA Form 8110-2 (5/14) Page 1 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST11212SC 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: 777-200, S/N 30867 only T0001SE One-time installation of an executive interior in accordance with “Data List, Compliance Data, Aeria, P8050, Polaris 777, ODA STC,” document no. DL1935M00, revision AH, dated 5/9/17 or later FAA approved revision; “Instructions for Continued Airworthiness for the Installation of a VIP Interior in Boeing 777-200 Series Aircraft,” document no. 8050CT25-03, revision A, dated 5/4/17 or later FAA accepted revision; and “Airplane Flight Manual Supplement,” document no. 8050CT25-01, revision A, dated 5/2/17 or later FAA approved revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. Date of Application: July 10, 2015 Date Reissued: March 19, 2018 Date of Issuance: May 13, 2017 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, ai rcraft engine, or propeller. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST11212SC 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, ai rcraft engine, or propeller. 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: ST11212SC 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. Operations involving the carriage of persons or property for compensation or hire are prohibited with this STC installed. 5. In order for this airplane, certified under SFAR 109, to be placed in part 135 or part 121 operations, the airplane must be brought back into full compliance with the applicable operation part. 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 777-200, S/N 30867, modified by installing an executive interior is as follows: a. The type certification basis for Boeing 777-200 series airplanes is shown on TCDS T00001SE 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, July 10, 2015, include: Regulations at the latest amendment 25-0 through 25-141 14 CFR §25.305(a)(b), 25.613(a)(b)(f), 25.787(a)(b), and 25.853(a)(c)(h). Regulations at an intermediate amendment 14 CFR § 25.981(a)(3)(b) amd 25-102. Exemptions from 14CFR part 25 - a. Exemption 17058 from 25.817, dated 8/8/16. Equivalent safety findings exist with respect to the following regulations - None Special conditions - a. Special condition 25-654-SC for “Installation of an Airbag System in Shoulder Belts,” dated 3/31/17. Special Federal Aviation Regulations - a. SFAR 109 “Special Requirements for Private Use Transport Category Airplanes,” dated 6/8/09. -------------- END ------------- ## Every issue (2) - March 19, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/dd/1c/dd1c0e5e6994faa953ff71779245464b4ea9b3206eca453472472da6d1b593ae) - May 13, 2017: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/39/a4/39a47857ba7d9d155f1516e6b57d924adf23f13e238441e6d555695b4bee5e8f) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.