STC ST04496AT

FAA 8110-2 (10/24) Page 1 of ___ ST04496AT ZIM Aircraft Cabin Solutions, LLC 8010 Piedmont Triad Parkway Greensboro, NC 27409 25 Federal Aviation Regulations Boeing 737-800 Series A16WE Interior Reconfiguration of a Boeing 737-800 Series aircraft in accordance with ZIM Aircraft Cabin Solutions, LLC MDL 23T009L001, Rev B, dated 14 Jul 2025, or later FAA approved revisions.

(Description of Type Design Change continued on page 3) (Limitations and Conditions continued on page 3) 7/9/24 7/15/25 Jose Pevida - ODA Administrator Lead ODA-100214-CE 4

ZIM Aircraft Cabin solutions, LLC Instructions for Continued Airworthiness 23T009R009 Rev 03, dated 08 Jul 2025, or later FAA accepted revision is a required part of this STC.

(Limitations and Conditions continued)

1) This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane.

2) 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.

Certification Basis Based on 14 §§ CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Boeing 737-800 aircraft is as follows:

a. The type certification basis for Boeing 737-800 aircraft 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, July 9 2024 is based upon Part 25 as amended by Amendment 25-151. Based on 14 §§ CFR 21.115 and 21.101, and the FAA policy for 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 25-151

25.1, 25.23, 25.27(b), 25.301, 25.303, 25.562(a)(b)(c)(2)(3)(4)(5)(6)(7)(8),

25.562(b)(2)(c)(4)(5)(6)(7)(8)*, 25.601, 25.603, 25.605(a), 25.609, 25.619, 25.625, 25.785(b)*,

25.789(a), 25.803(a)(c), 25.815, 25.853 (a)(c)(d)(e), 25.853(d)**, 25.863***, 25.869(a)(1)****,

25.899, 25.981(d), 25.1351(a)(1), 25.1353(a)****, 25.1360(a), 25.1415, 25.1423(c),

25.1431(c)****, 25.1529, 25.1541(a)(1)(b).

(Certification Basis continued on next page) 3 4 Add Page 07/15/25

Regulations at an intermediate amendment None.

Regulations at amendment level in TCDS A16WE

25.305(a)(b), 25.307(a), 25.561(a)(b)(3)(c), 25.571(b), 25.611, 25.613(a)(b),

25.785(a)(b)(c)(d)(f)(1)(3)(h)(2)(i)(j)(k), 25.787(a)(b), 25.791(a)(b)(c)(e), 25.811(b)(c)(d),

25.812(e), 25.813(a)(b)(c)(d), 25.831, 25.853(a)(c), 25.869(a)(4), 25.1301, 25.1301(a)****,

25.1309(a)(b)(g), 25.1309(b)(d)(e)****, 25.1353(a)(b), 25.1357(a)(c),

25.1411(a)(b)(d)(f), 25.1431(c), 25.1447(a)(c).

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 amendment, 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 regulations (Amdt. 26-0 through 26-7):

26.11(c), 26.47(c).

*Dynamic approval only, Special condition applicable: 25-386-SC **HRSC approval only, Special condition applicable: 25-358-SC ***Airbag System approval only, Special condition applicable: 25-632-SC ***Airbag System approval only, Special condition applicable: 25-386-SC and 25-632-SC -------------------------------------------------------END------------------------------------------------------- 4 4 Add Page 07/15/25