STC SA3474NM

United States Of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number ST02550LA

FAA Form 8110-2 (3/21) SUPERSEDES PREVIOUS EDITION Page 1 of 2

This Certificate issued to Safran Cabin Inc.

5701 Bolsa Ave Huntington Beach, CA 92647 Part 25* of the Federal Aviation Regulations.

*Certification basis is set forth in Type Certificate Data Sheet A16WE and continuation page 3.

Original Product - Type Certificate Number : A16WE Make :

The Boeing Company 737-800 Series

Description of Type Design Change: Installation of Galley G4B in accordance with Driessen Master Data List MDL-501530-1 Revision F dated January 7, 2016 or later FAA approved revisions.

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. 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.

(Limitations and conditions continued on page 3)

Date of application : January 16, 2015 Date of issuance : January 28, 2016

Date Amended: : March 15, 2023

(Signature) For Gregory S. DiLibero Manager, West Certification Branch, AIR-770 Compliance and Airworthiness Division Aircraft Certification Service

United States Of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number ST02550LA

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 2 of 2

United States Of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number ST02550LA

FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 2 of 2

Limitations and Conditions: Instructions for continued Airworthiness (ICA), Driesen Components Maintenance Manual (CMM) 25-30-501530-1 Revision 1, dated December 11, 2015, or later FAA accepted revision must be made available to the operator at the time of installation.

Certification Basis:

Based on 14CFR 21.115 and 21.101, and the FAA policy for changes in FAA order 8110.48, the certification basis for this modification was determined to be:

a. The type certification basis for Boeing Model 737-800 airplanes is shown in TCDS A16WE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by this change as of the reference date of application, January 16, 2015is based on part 25 as amended by Amdt 25-140 and CFR part 26.

Based on 14 CFR 21.115 and 21.101, the certification basis for this modification was determined to be:

Regulations at the latest amendment 25-0 through 25-140

25.853(a), (d), (h) Amdt 25-116; 25.561 (b)-(d) Amdt 25-91

Regulations at the latest amendment 25-0 through 25-140

25.1583(c) Amdt 25-105

Regulations at the amendment level in TCDS A16WE

25.23(a), (b); 25.301(a)-(c); 25.303; 25.305 (a)-(c), 25.37(a), (d); 25.365 (e)(g); 25.561 (a);

25.601;25.603 (a) –(c); 25.605(a); 25.609 (a), (b); 25.611;25.625(a)-(c); 25.787(a) (b); 25.789 (a);

25.791(c); 25.803 (a); 25.813 (a) (b); 25.851(a4), (a7); 25.869(a) (4); 25.1301 (a)-(d); 25.1307 (c);

25.1309(a)(b)(d); 25.1351 (a); 25.1353(a), (c) (f); 25.1431 (c); 25.1519; 25.1529; 25.1541 (a)(b);

25.1557(a).

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 changes to the STC, 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 21.11 ©, (d) (Amdt 26-0)

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