STC ST10823SC

Part 25 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of an Executive Interior in accordance with Gore Design Completions (GDC), Ltd., Certification Drawing List, GDC-359-03, Revision W, released March 7, 2008, or later FAA approved revision. The aircraft is to be maintained per the “Instructions for Continued Airworthiness, Boeing 737-700 Interior Modifications”, GDC Document Number GDC-359-05, Revision G, released March 13, 2008, or later FAA accepted revision. Airplane Flight Manual Supplements

Limitations and Conditions: : You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Boeing Model 737-7EG Serial No. 35990. This STC does not permit manufacturing of parts for multiple installations.

Samsung OPTO-Electronics America Inc.

100 Challenger Road Suite 700 Ridgefield Park, NJ 07660 A16WE Make : The Boeing Company Model : 737-7EG, Serial Number 35990

Date of application : September 27, 2006

Date of issuance : March 20, 2008

Date reissued : March 21, 2008; November 12, 2008

( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region

( Title)

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

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

Number ST10823SC Date of Issuance: March 21, 2008 Date of Reissuance: November 12, 2008

Description of Type Design Change (Continued):

(AFMS) titled “Airplane Flight Manual Supplement for Boeing 737-7EG with an Executive Interior”, Document Number GFA-359-16, Revision IR, dated March 20, 2008, or later FAA approved revision and “Airplane Flight Manual Supplement for a Boeing 737-700 IGW with a Universal Avionics Systems Corporation UNS-1Espw”, Document Number GFA-359-21, dated March 20, 2008, or later FAA approved revision are required.

Maximum seating for this aircraft (other than the pilot and co-pilot) is 5 crew (2 in the cockpit jump seats, 2 in the flight attendant seats and 1 in the crew rest area) and 15 passengers. Other than the pilot and co-pilot, one flight attendant is required on board the aircraft for compliance with this STC. This aircraft is not to be operated for hire or offered for common carriage.

This modification may not be installed after June 7, 2010 unless (1) previously approved electrical wiring interconnection system (EWIS) instructions for continued airworthiness (ICA) have been evaluated and determined to be adequate for this installation by the FAA, or (2) revised EWIS ICA have been approved by the FAA Oversight Office. (Refer to § 26.11).

Certification Basis: All regulation at the amendment levels identified in Type Certificate Data Sheet (TCDS) A16WE except for the following regulations that have been complied with at a high amendment level:

14 CFR 25.820 amendment 114

14 CFR 25.853 amendment 116

14 CFR 25.856 amendment 111

14 CFR 25.981 amendment 102

14 CFR 25.1431 amendment 113

This STC incorporates compliance to the following regulations by FAA Exemption 6820 and 6820A:

14 CFR 25.785(h)(2)

14 CFR 25.807(d)(7)

14 CFR 25.813(e)

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