# STC ST10159SC-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: American Airlines Inc, United States - Description: Interior reconfiguration. - Applied: September 15, 2005 - Status date: May 2, 2013 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS T00001SE](https://openairdocs.org/tcds/T00001SE) - Certificate PDF: https://openairdocs.org/files/sha256/68/93/6893fa6090432a989fe054b9c6424ea04ca1869a489ca8f250219337c11ea2f7 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AB7E61F2AB3F549286257B8800542DFC.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST10159SC-D ## 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 8110-2-1(10-69) Page 1 of 3 Number ST 10159 SC-D This Certificate issued to Part 25 of the Federal Aviation Regulations. Description of Type Design Change: Interior reconfiguration in accordance with Master Data List B0836- MDL, Revision E, dated April 30, 2013, or later ODA-700094-SW approved revision. Limitations and Conditions: This approval should not be incorporated in any aircraft of this specific model until compatibility of this modification with previously approved modifications has been determined by the installer. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. (Limitations and Conditions continued on page 3 of 3) This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. American Airlines, Inc. 3900 N. Mingo Road Engineering Dept., MD 208 Tulsa, Oklahoma 74116 T00001SE Make: Boeing Model: 777-222 Date of application : 15 September 2005 Date of issuance : 25 February 2006 Date reissued : 30 March 2006 Date amended : 2 May 2013 (Signature) C.E. Williams ODA-700094-SW Administrator (Title) FAA Form 8110-2-1(10-69) Page 3 of 3 (Continuation Sheet) Number ST 10159 SC-D The Instructions for Continued Airworthiness, Document Number B0836-ICA, Revision B, dated 31 January 2013 or later FAA AEG accepted revision shall be made available to the operator at the time of installation. The aircraft shall be maintained in accordance with the Instructions for Continued Airworthiness. A revised EWIS ICA is not required for this STC. Certification Basis: Based on 14CFR 21.115 and 21.101, and the FAA policy for non-significant changes in FAA Order 8110.48, the certification basis for the Boeing Model 777-222 aircraft for the change is as follows: a. The Type Certification basis for Boeing Model 777-222 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, 15 September 2005 is based upon Part 25, as amended by Amendment 25-115 and Part 26. Based on 14 CFR 21.115 and 21.101, and the FAA policy for non 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 25-115 25.21(a.1), 25.29, 25.301, 25.303, 25.307, 25.562, 25.601, 25.603, 25.605, 25.609(a), 25.787(a)(b), 25.789(a), 25.791(a)(b), 25.803(c), 25.815, 25.851(a.1), 25.869(a.4), 25.981(a.3), 25.1301, 25.1309(a-d)(g), 25.1351(a), 25.1353(a)(b)(d), 25.1357(a-c), 25.1529, 25.1541, 25.1557(c)(d), 25.1561 Regulations at an intermediate amendment None. Regulations at the amendment level in TCDS T00001SE 25.305, 25.365(a), 25.561, 25.785(b-d)(f.1)(f.3)(h)(k), 25.807, 25.811(b-d), 25.812(e), 25.853(a), 25.1411(a)(d.1)(f), 25.1431(a-c), 25.1447(a)(c.1) 14 CFR Part 26 regulations Based on 14 CFR § 21.101(g), applicable provision of 14 CFR Part 26 are included in the certification basis. For any future 14 CFR Part 26 amendments, the holder of this STC must demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations 14 CFR § 26.11(c), (Amendment No. 26-0, through 26-3). -------------------------------------------------------------- END ----------------------------------------------------------------- ## Every issue (2) - May 2, 2013: Amended, Current. [certificate](https://openairdocs.org/files/sha256/68/93/6893fa6090432a989fe054b9c6424ea04ca1869a489ca8f250219337c11ea2f7) - February 25, 2006: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/0f/37/0f378bf70ab97100b6028949139656e77879e0f4c732cc987f0538ac0615836d) --- 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.