# STC ST11211SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: VT DRB Aviation Consultants - Description: Reconfiguration of cabin interior - Status date: March 19, 2018 - Data sheets: A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM, A46NM - Certificate PDF: https://openairdocs.org/files/sha256/ac/7d/ac7dff531c34ffb7ffe6e01c83418e23d1834994b043da402f31d4df6d1dd241 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/653277D3650001C886258260004886F1.0001 - Page: https://openairdocs.org/stc/ST11211SC ## ADs that name it None. ## Approved models (9) - Airbus SAS A330-301 (TCDS A46NM) - Airbus SAS A330-302 (TCDS A46NM) - Airbus SAS A330-303 (TCDS A46NM) - Airbus SAS A330-321 (TCDS A46NM) - Airbus SAS A330-322 (TCDS A46NM) - Airbus SAS A330-323 (TCDS A46NM) - Airbus SAS A330-341 (TCDS A46NM) - Airbus SAS A330-342 (TCDS A46NM) - Airbus SAS A330-343 (TCDS A46NM) ## 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 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: ST11211SC 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: Airbus Model: A330-300 series aircraft A46NM Reconfiguration of cabin interior in accordance with “Data List, Installation Data, Air Canada, A330 Lite Cabin Reconfiguration” document no. DL1955M09, revision IR, dated 11/10/16 or later FAA approved revision; “Airplane Flight Manual Supplement,” document no. 1955CT25-03, revision IR, dated 11/8/16 or later FAA approved revision; and “Instructions for Continued Airworthiness for the Interior Reconfiguration of an Airbus A330-300 Series Aircraft,” document no. 1955CT25-05, revision IR, dated 11/8/16 or later FAA accepted revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. Date of Application: December 21, 2015 Date Reissued: March 19, 2018 Date of Issuance: November 11, 2016 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: ST11211SC 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: ST11211SC 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. 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 Airbus A330-300 aircraft modified by reconfiguring the cabin interior is as follows: a. The type certification basis for Airbus A330-300 series airplanes is shown on TCDS A46NM 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, December 21, 2015, include: Regulations at the latest amendment 25-0 through 25-142 14 CFR §25.29(a)(b), 25.853(a)(d), 25.1307(c), 25.1431(c), 25.1557(a)(c) and 25.1581(a)(b)(d). Regulations at an intermediate amendment 14 CFR §25.869(a)(4) amd 25-72. Exemptions from 14CFR part 25 - None Equivalent safety findings exist with respect to the following regulations - None -------------- END ------------- ## Every issue (1) - March 19, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ac/7d/ac7dff531c34ffb7ffe6e01c83418e23d1834994b043da402f31d4df6d1dd241) --- 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.