# STC ST11055SC - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Omni Air International, United States - Description: Installation of an IMS RAVE seat-centric IFE system - Applied: May 14, 2012 - Status date: January 7, 2016 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE) - Certificate PDF: https://openairdocs.org/files/sha256/92/5e/925eb6460f6000b5b92a4e546d062ea13765118c09a59456a36fa05038fd1be6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/59F8080E69459C2E8625803C006BEE8D.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST11055SC ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 777-200 Series ([TCDS T00001SE](https://openairdocs.org/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. FAA Form 8110-2 (5/14) Page 1 of 3 Number: ST11055SC Part 25 of the Federal Aviation Regulations Original Product – Type Certificate Number: T00001SE Make: Boeing Model: 777-200 Series Description of Type Design Change: Installation of an IMS RAVE seat-centric IFE system in accordance with “Compliance Data List,” document no. DL1864M00, revision A, dated March 28, 2013 or later FAA approved revision. “Airplane Flight Manual Supplement,” document no. 439-00-0006, revision IR, dated March 27, 2013 or later FAA approved revision, and, “Instrucitons for Continued Airworthiness,” document no. 1864R44M07, revision A, dated March 26, 2013 or later FAA accepted revision must be made available to the operator at the time of installation. 1. The installer must determine whether this change is compatible with previously approved modificaitons. 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: Date of Application: May 14, 2012 Date Reissued: January 7, 2016 Date of Issuance: March 28, 2013 Date Amended: October 21, 2014 Signature Title John Hardie Acting Manager, Fort Worth Aircraft Certification Office, Southwest Region Omni Air International 3303 N. Sheridan Road, Hangar 19 Tulsa, OK 74115 FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: ST11055SC To (Name and address of transferee) From (Name and address of grantor) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11055SC FAA Form 8110-2 (5/14) Page 3 of 3 Date of Issuance: March 28, 2013 Date Amended: October 21, 2014 Date of Reissuance: January 7, 2016 Certification Basis (Continued): 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 Series modified by installing IMS RAVE IFE system 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, May 14, 2012, is based upon part 25 as amended by Amendment 25-82: 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 this modification was determined to be: Regulations at the latest amendment 25-0 through 25-136 14CFR 25.1, 25.29(a)(b), 25.301(a)(b), 25.303, 25.305(a)(b), 25.307(a), 25.562(a)(b)(2)(c)(5), 25.601, 25.603, 25.605(a), 25.609, 25.613(a)(b), 25.789(a), 23.1307(c), 25.1351(a)(1)(d), 25.1431(a)(b)(c)(d), 25.1501, 25.1529, 25.1541, 25.1581 and 26.11. Regulations at an intermediate amendment 14CFR 25.981(a)(3)(b), (amd 25-102); 25.1353(a)(b)(d), (amd. 25-113). Regulations at the amendment level in TCDS T00001SE 14CFR 25.2, 25.341(a), 25.561, 25.785(b)(d), 25.853(a)(c), 25.869(a)(4), 25.1301, 25.1309(a)(b)(d)(f)(g), 25.1357(a)(c). -END- United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11055SC FAA Form 8110-2 (5/14) Page 4 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11055SC FAA Form 8110-2 (5/14) Page 5 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11055SC FAA Form 8110-2 (5/14) Page 6 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11055SC FAA Form 8110-2 (5/14) Page 7 of 3 ## Every issue (2) - January 7, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/92/5e/925eb6460f6000b5b92a4e546d062ea13765118c09a59456a36fa05038fd1be6) - March 28, 2013: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/53/e9/53e999a2ca38c6ec6adeedd0e3be7cb7afa218ad39cbf59ac7e52cc6bc2e883d) --- 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.