STC ST00183IB

IMPORT ST00183IB

JET AVIATION AG AESCHENGRABEN 6 4051 BASEL

SWITZERLAND Part 25 Title 14 Code of Federal Regulations A16WE The Boeing Company 737-8

1. Structural installation of a Dual Iridium/LTE Antenna on the forward fuselage upper lobe, between STA 480 and STA 500, stringer S-1 to stringer S-2R must be in accordance with Jet Aviation AG Master Data List Document No. JBSL-M-03862MDL-001, Issue B, dated October 6, 2023, or later EASA approved revisions.

(See Description of Type Design Change Continued on Page 3 of 3)

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

(See Limitations and Conditions Continued on Page 3 of 3) February 2, 2024 March 12, 2024 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT ST00183IB 3

IMPORT ST00183IB Date of Issuance: March 12, 2024 Description of Type Design Change (continued):

2. Maintenance must be in accordance with Jet Aviation AG Instructions for Continued Airworthiness (ICA) Document No. JBSL-M-03862ICA-001, Issue A, dated October 6, 2023, or later EASA accepted revisions.

3. Operation must be in accordance with 365 Aerospace DDS Ltd. Flight Manual Supplement Document No. FMS-1002-001, Revision B, dated October 2, 2020, or later EASA approved revisions.

2. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission.

3. This STC is applicable to all serial numbers for this Make-Model.

4. Aircraft is to be maintained in accordance with "Airworthiness Limitations" section of Jet Aviation AG ICA referenced under item 2 in the description of type design change section of this STC.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48A, the certification basis for this modification are as follows:

a. The type certification basis is as shown on TCDS A16WE for parts not changed or not affected by the change.

b. The type certification basis for is shown on TCDS A16WE for parts changed or affected by the change plus:

FAR 25.23, 25.27, 25.601, 25.609 at initial Amendment, 25.301, 25.303, 25.337,

25.581 (b)(1), 25.607, 25.631 at Amendment 25-23, 25.1401 (b) at Amendment 25-41,

25.603, 25.605, 25.789 (a) at Amendment 25-46, 25.1529 at Amendment 25-54, 25.25 at Amendment 25-63, 25.29, 25.625, 25.1581 at Amendment 25-72, 25.251 (b) at Amendment 25-77, 25.305, 25.321 at Amendment 25-86, 25.561 at Amendment 25-91,

25.613 at Amendment 25-112, 25.611 (a), 25.899, 25.1301 (a), 25.1703 at Amendment 25-123, 25.1419 at Amendment 25-129, 25.1583 at Amendment 25-130, 25.307 at Amendment 25-139, 25.571 at Amendment 25-148, 25.365 at Amendment 25-149,

25.841 at Amendment 25-151 ----------END---------- 3 3