STC ST10159SC-D

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).

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