STC ST00119IB

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT Number: ST00119IB

This certificate issued to: AMAC Aerospace Switzerland AG Sternengasse 18 4051 Basel, Switzerland Part 25 of Title 14 Code of Federal Regulations .

A16WE Make: The Boeing Company Model: 737-8 Description of Type Design Change:

1. Installation of a VIP cabin interior in accordance with Master Data List, Doc. No. MDL-LB01-2500, Rev.

L, dated November 1, 2023, or later EASA approved revision.

2. Operation must be in accordance with Airplane Flight Manual Supplement, Doc. No. AFMS-LB01-2500 Rev. B, dated June 27, 2023, or later EASA approved revision and is required as part of this installation.

(See Description of Type Design Change Continued on Page 3 of 4)

1. The aircraft must be operated in accordance with the "Certificate Limitations" section of Airplane Flight Manual Supplement Doc. No. AFMS-LB01-2500, Rev. B, dated June 27, 2023, or later EASA approved revision.

(See Limitations and Conditions Continued on Page 3 of 4)

Date of Application: November 29, 2021

Date of Issuance: November 13, 2023 Date Amended:

Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT Number: ST00119IB

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT (Continuation Sheet) Number: ST00119IB Date of Issuance: November 13, 2023

Description of Type Design Change (continued):

3. Maintenance must be in accordance with Instructions for Continued Airworthiness Doc. ICA-LB01-2500, Rev. B, dated June 20, 2023, or later EASA accepted revision and is required as part of this installation.

2. You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Boeing Model 737-8 Serial No. 64084. This STC does not permit manufacturing of parts for multiple installations.

3. The following STCs are prerequisite to this modification:

FAA STC ST04272NY (EASA STC 10060874 Rev 4) - Jet Wave Ka-Band Antenna installation.

FAA STC ST04447NY (EASA STC 10072048) - Fin Top Antenna Ku-Band TIOS Radome installation.

FAA STC ST04664NY (EASA STC 10076636 Rev 1) - WLAN Activation.

FAA STC ST00105IB (EASA STC 10079998) - Certification of Wireless Charging Stations for PEDs.

4. The EASA approved Airworthiness Limitations section of Instructions for Continued Airworthiness, Doc. No. ICA-LB01-2500, Rev. B, dated June 20, 2023, is mandatory.

5. Maximum passenger seating capacity is limited to 19 and only in the seats designated as eligible to be occupied during taxi, takeoff and landing.

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

(See Certification Basis on Page 4 of 4)

United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT (Continuation Sheet) Number: ST00119IB Date of Issuance: November 13, 2023

Certification Basis:

Based on 14 CFR §21.115 and §21.101 and FAA Order 8110.48A the certification basis for this modification to the Boeing 737-8 aircraft is as follows:

a) The type certification basis for the Boeing 737-8 aircraft as shown on TCDS A16WE for parts not changed or not affected by the change.

b) The type certification basis for the Boeing 737-8 aircraft as shown on TCDS A16WE for parts changed or affected by the change with the following exceptions:

- Compliance with Special Federal Aviation Regulation (SFAR) No. 109.

- Exemption No. 21451

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