STC ST04491AT

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST04491AT ZIM Aircraft Cabin Solutions, LLC 8010 Piedmont Triad Parkway Greensboro, NC 27409 25 Federal Aviation Regulations A16WE Boeing 737-800 Series Cabin Interior Reconfiguration (Demod) in a Boeing 737-800 Series aircraft in accordance with HAECO Cabin Solutions Master Data List 22T028L001, Revision B, dated 21 Jul 2023, or later FAA approved revision. HAECO Cabin Solutions Instructions for Continued Airworthiness 22T028R009, Revision 01, dated 9 Jun 2023, or later FAA accepted revision is a required part of this STC.

(Limitations and Conditions continued on page 3) March 8, 2023 February 29, 2024 May 26, 2023 David Pikett ODA Administrator ODA-100214-CE 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

ST04491AT 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

ST04491AT Date Reissued: February 29, 2024 (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 Series aircraft is as follows:

a. The type certification basis for Boeing 737-800 Series 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, 08 Mar 2023 is based upon Part 25 as amended by Amendment 25-148. 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 25-148:

25.1, 25.23(b)(2), 25.27, 25.301, 25.303, 25.601, 25.603, 25.609, 25.789(a), 25.981(d),

25.1351(a)(1), 25.1360(a), 25.1529, 25.1541(a)(1)(b).

(Certification Basis continued on next page) 3 4

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

ST04491AT Date Reissued: February 29, 2024 (Certification Basis continued)

Regulations at an intermediate amendment:

None.

Regulations at the amendment level in TCDS A16WE:

25.561(a)(b)(3)(c), 25.869(a)(1), 25.1301(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).

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