STC ST04497AT

FAA 8110-2 (10/24) Page 1 of ___ ST04497AT ZIM Aircraft Cabin Solutions, LLC 8010 Piedmont Triad Parkway Greensboro, NC 27409 25 Federal Aviation Regulations Airbus A330-200 Series A46NM Interior Reconfiguration on an Airbus A330-200 Series aircraft in accordance with ZIM Aircraft Cabin Solutions, LLC MDL 23T059L001, Rev B, dated 09 Jul 2025, or later FAA approved revisions. (Description of Type Design Change continued on page 3) (Limitations and Conditions continued on page 3) 10/23/24 7/9/25 Jose Pevida - ODA Administrator Lead ODA-100214-CE 4

ZIM Aircraft Cabin Solutions, LLC Instructions for Continued Airworthiness 23T059R009 Rev 00, dated 21 Apr 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 Airbus A330-200 series aircraft is as follows:

a. The type certification basis for Airbus A330-200 series aircraft is shown on TCDS A46NM 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, 23 Oct 2024 is based upon Part 25 as amended by Amendment 25-153. 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 25-153

25.1, 25.23, 25.29, 25.301, 25.303, 25.562(a)(b)(c)(2)(3)(4)(5)(6)(7)(8), 25.601, 25.603,

25.605(a), 25.609, 25.619, 25.789(a), 25.793, 25.815, 25.853(a)(c)(d)(e), 25.899, 25.981(d)

25.1353(a)(c), 25.1360, 25.1423(c), 25.1529, 25.1541(a)(1)(b), 25.1561(b)(c)(e).

(Certification Basis continued on next page) 3 4 Add Page 07/09/25

Regulations at an intermediate amendment

25.869(a)(4) Amdt 25-72.

Regulations at amendment level in TCDS A46NM

25.305(a)(b), 25.307(a)(d), 25.365(e)(2)(g), 25.561(a)(b)(1)(3)(c)(d), 25.571(b), 25.611,

25.613(a)(b), 25.625, 25.785(a)(b)(c)(d)(e)(h)(1)(i)(1)(3), 25.787(a)(b), 25.791(a)(b)(e),

25.803(a)(c), 25.811(b)(c)(d), 25.812(a)(1)(e), 25.813(a)(d)(e), 25.851(a)(1),

25.853(a)(b)(2)(3)(c), 25.1301, 25.1309(a)(b)(g), 25.1351(a)(1), 25.1411(a)(b), 25.1431(c),

25.1447, 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 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).

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