STC ST11365DS

Part 25 of the Federal Aviation Regulations. (See Page 3 for complete certification basis)

Modification of a Cabin Interior in accordance with GDC Technics Master Data List AT1060-MDL, Revision ( M), dated June 23, 2021 or later FAA approved revision.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. Descriptive data pertaining to this design change are considered inadequate for duplication in other aircraft.

This approval is limited to only the installation made in The Boeing Company 737- 700 Series S/N 38028 and S/N 36720. This STC does not permit manufacturing of parts for multiple installations.

GDC Technics, LLC 2060 Eagle Parkway Fort Worth, Texas 76177 A16WE Make: The Boeing Company Model: 737-700 Series

Date of application: March 05, 2021

Date of issuance: June 24, 2021 Date reissued:

(Signature) Robert Miller, ODA Administrator GDC Technics, LLC. Fort Worth, TX ODA-834545-SW

(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):

Supplemental Type Certificate Number: ST11365DS Date of issuance: June 24, 2021 Date of amendment:

Date of reissue:

Certification Basis (continued)

Based on 14 CFR §§ 21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for The Boeing Company 737-700 Series aircraft Modification of a Cabin Interior is as follows:

a. The type certification basis for The Boeing Company 737-700 Series is shown on TCDS A16WE 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, March 05, 2021, is based upon TCDS A16WE. Based on 14 CFR § 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for this modification was determined to be:

Regulations at the amendment level in TCDS A16WE

25.1(a, b)(25-0), 25.29(a, b)(25-72), 25.301(a, b)(25-23), 25.303(25-23), 25.305(a, b)(25-77), 25.305(d)(25-86),

25.307(a)(25-72), 25.365(a-d, e, g)(25-72), 25.561(a-c)(25-0), 25.562(a-c)(25-64), 25.571(a)(25-72), 25.571(b)(25-86),

25.601(25-0), 25.603(a-c)(25-46), 25.605(a)(25-46), 25.607(25-0), 25.609(a, b)(25-0), 25.611(25-23),

25.619(a-c)(25-23), 25.625(a-d)(25-72), 25.783(j)(25-72), 25.785(b-d, f1, f3, h, i, k)(25-72), 25.787(a, b)(25-51),

25.789(a, b)(25-46), 25.791(a-e)(25-72), 25.811(a-d, g)(25-46), 25.812(b1, e, f)(25-58), 25.813(a-e)(25-76),

25.815(25-38), 25.851(a, b)(25-74), 25.853(a, c, d-f)(25-72), 25.854(a, b)(25-74), 25.869(c)(25-72),

25.1301(a-d)(25-0), 25.1309(a, b, d, e1,e2,e3i, g)(25-41), 25.1351(a)(25-72), 25.1353(a, b)(25-42), 25.1355(a)(25-38),

25.1357(a, c)(25-0), 25.1411(a, b, f)(25-70), 25.1421(25-41), 25.1431(a, c)(25-0), 25.1438(b, c)(25-41),

25.1439(a, b)(25-38), 25.1441(a, b)(25-0), 25.1447(a, b, c1, c3, c4)(25- 41), 25.1455(25-23), 25.1529(25-54),

25.1541(a, b)(25-0), 25.1557(a, c)(25-72), 25.1561(b, c)(25-46).

Regulations at a later amendment level

25.613(a, b, c, f)(25-112), 25.869(a4)(25-113),

14 CFR Part 26 Regulations

Based on 14 CFR §§ 21.101(g), applicable provisions of 14 CFR Part 26 are included in the cert ification 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), (Amdt. No, 26-0), 26.47 (c), (Amdt. No, 26-1).

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