STC ST10161SC

FAA Form 8110-2-1(10-69) Page 1 of 4 Number ST10161SC This Certificate issued to

Part 25 of the Federal Aviation Regulations.

Description of Type Design Change: Reconfigure the interior cabin and install updated IFE products in accordance with Master Data List C2551-MDL, Rev H, dated November 14, 2011, and Airplane Flight Manual Supplement dated Feb 27, 2009 or later AA ODA 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 4)

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, OK 74116 A1NM Make: Boeing Model: 767-323 Date of application : November 8, 2005

Date of issuance : June 7, 2006

Date amended : 27 February 2009, 13 June 2011, 15 November 2011

( Signature)

Cheryl Hurst ODA-700094-SW Administrator

( Title)

FAA Form 8110-2-1(10-69) Page 3 of 4 (Continuation Sheet)

Number ST10161SC

Instructions for Continued Airworthiness, Document Number C2551-ICA, Revision J, dated November 7, 2011 or later FAA AEG accepted revision shall be made available to the operator at the time of installation. A revised Electrical Wiring Interconnection System (EWIS) ICA is required for this STC.

EWIS ICA Source Document, C2551-EWIS ICA, Revision NEW, dated September 7, 2011 or later FAA approved revision shall be made available to the operator at the time of installation. The aircraft shall be maintained in accordance with the above ICA.

Requires the installation of STC SA3992SW-D, dated 15 September 1997 or later ODA approved revision.

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 767-323 series aircraft for the change is as follows:

a. The Type Certification basis for Boeing Model 767-323 series airplanes is shown on TCDS A1NM 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, November 8, 2005 is based upon Part 25, as amended by Amendment 25-117. 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 25-117

25.301, 25.303, 25.601, 25.603, 25.605, 25.607, 25.609, 25.611, 25.619, 25.787.a.b, 25.789 (a), 25.791,

25.793, 25.815, 25.851.a.1, a.4, a5, a.6, 25.856.a, 25.981.a.3, b, 25.1301, 25.1307.c, 25.1309, 25.1351.a.

25.1357.a,c, 25.1519, 25.1529, 25.1541, 25.1557.a,c, 25.1561.b,c, 25.1581.a.2

Regulations at an intermediate amendment

25.561.d AMDT 64

25.613.a.b.c.d AMDT 46

25.785.a,b,c,d,f.1,f.3,h,i,j,k, AMDT 72

25.807.d AMDT 72

25.811.a,b,c,d,g AMDT 79

25.812.a.1,c,d,e,i, l.1,2,3 AMDT 88

25.813.a,b,d,e AMDT 76

25.831.a,b AMDT 87

25.853.a,d,e AMDT 83

25.869.a.1,a.4 AMDT 72

25.1411.a,b,d,e,f AMDT 79

25.1415.b.1 AMDT 72

25.1583.c.1,c.2 AMDT 72

FAA Form 8110-2-1(10-69) Page 4 of 4 (Continuation Sheet)

Number ST10161SC

Certification Basis (continued):

Regulations at the amendment level in TCDS A1NM

25.21.a.1, 25.29, 25.305, 25.307.a,b,c, 25.365.e,f,g, 25.561.a,b,c, 25.571.a.b, 25.605, 25.613, 25.615,

25.625.a,b,c, 25.789, 25.803.c, 25.1165.b, 25.1351.a, 25.1353.a,b, 25.1431.a,c, 25.1447.a,c.1,c.4

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),(d.5), (Amendment No. 26-0, through 26-3) and 14 CFR § 26.47(c), (Amendment No. 01).

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