STC SA5135NM

This Certificate issued to Rockwell Collins, Inc.

1733 Alton Parkway Irvine, California 92606 Part 25* of the Federal Aviation Regulations. *Certification basis set forth on continuation sheet 3.

Original Product Type Certificate Number : A16WE Make Boeing Model 737-400, 700, 800 Series Airplanes Description of Type Design Change: Installation of Video Entertainment System in accordance with FAA approved Rockwell Collins (Sony Trans Com) Index List 062-0138-000, Rev. “NEW” dated October 4, 1993, or later FAA approved revision.

Limitations and Conditions: This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. A copy of this STC must be included in the permanent record of the modified aircraft.

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. (Continued On Page 3)

Date of application : November 26, 1990

Date of issuance : March 21, 1991

Date reissued : April 1, 1993; October 28, 1993;

August 30, 2000; May 30, 2006, June 7, 2016

Date amended : January 30, 1992; April 15, 1998;

July 10, 1998; December 10, 2010; May 10, 2013

(Signature) Manager, Technical & Administrative Support Staff, Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-289

Number SA5135NM

Limitations and Conditions (Continued)

See referenced Rockwell Collins (Sony Trans Com) Index List 062-0138-000 for further applicable “Limitations”.

Certification Basis

Based on 14 CFR §§ 21 .115 and 21.101, and FAA Order 8110.48, the type certification basis for the Boeing 737-400, 700, 800 is as shown on TCDS A 16WE for parts changed or affected by the change. Based on 14 CFR § 21.101(g), applicable provision of 14 CFR part 26 and included in the certification basis. For any future Part 26 amendments, the holder of this STC must demonstrate compli ance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations 14 CFR § 26.11, (Amdt. No. 26-0 ). The above certification basis is only applicable to Roc kwell Collins Index List 062-0138-000, Revision “AC”, dated November 16, 2010 or later FAA approved revisions.

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