STC ST11083SC

Number: ST11083SC

This certificate issued to: American Airlines, Inc.

3900 N. Mingo Road Engineering Dept., MD 208 Tulsa, OK 74116

Part 25 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: T00001SE Make: Boeing Model: 777-200 Series

IFE Power and Control Panel Modification in accordance with Master Data List, B1330-MDL, Revision A, dated December 19, 2016 or later ODA-700094-SW approved revision.

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.

This STC is contingent on prior or concurrent incorporation of STC ST10498SC.

This STC is contingent on concurrent incorporation of Boeing Service Bulletin 777-24-0075, Revision 4, date January 08, 2014 or later approved revision.

(Limitations and Conditions continued on page 3 of 3)

Date of Application: August 25, 2016 Date Reissued:

Date of Issuance: December 19, 2016 Date Amended:

Signature Richard T. Burk

Title: ODA-700094-SW Administrator

FAA Form 8110-2 (8/13) Page 1 of 3

SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)

Transfer the ownership of Supplemental Type Certificate Number: ST11083SC

To (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and ZIP Code)

From (Name of grantor)

(Address of grantor)

(Number and street)

(City, State, and ZIP Code)

FAA Form 8110-2 (8/13) Page 2 of 3

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11083SC Date of Issuance: December 19, 2016

The Instructions for Continued Airworthiness, Document Number B1330-ICA, Revision A dated November 16, 2016 or later FAA AEG accepted shall be made available to the operator at the time of installation. The aircraft shall be maintained in accordance with the applicable Instructions for Continued Airworthiness. A revised EWIS ICA is not required for this STC.

Certification Basis:

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 the Boeing Model 777-200 Series aircraft for the change is as follows:

a. The Type Certification basis for Boeing Model 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, August 25, 2016, is based upon Part 25 as amended by Amendment 25-143 and Part 26 as amended by Amendment 26-6. 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 25-143

25.899, 25.981(a.3)(d)

Regulations at an intermediate amendment

25.853(a) Amendment 25-83

Regulations at the amendment level in TCDS T00001SE

25.21(a.1), 25.29, 25.301, 25.303, 25.305(a-b), 25.307, 25.561, 25.601, 25.603, 25.605, 25.607, 25.609, 25.611,

25.613(a-b)(d-e), 25.619, 25.623, 25.625, 25.869(a.4), 25.1301, 25.1307(c), 25.1309(a-b)(d)(g), 25.1351(a.1),

25.1353(a-b), 25.1357(a)(c), 25.1529, 25.1541, 25.1583(c.2)

14 CFR Part 26 Regulations Based on 14 CFR §21.101(g), applicable provisions 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 of this STC, compliance has been found for the following regulations 14 CFR § 26.11(c) (Amendment No. 26-0 through 26-6).

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FAA Form 8110-2(8/13) Page 3 of 3