What it approves
Installation of KA Band Satcom System on rear fuselage crown
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT Number: ST00112IB
This certificate issued to: JET AVIATION AG AESCHENGRABEN 6 4051 BASEL
SWITZERLAND 25 of Title 14 Code of Federal Aviation Regulations .
Original Product Type Certificate Number: A16WE Make: THE BOEING COMPANY
Model: 737-700,737-800,737-900,737-900ER,737-8 Description of Type Design Change:
1. Installation of KA Band Satcom System on rear fuselage crown area in accordance with Master Data List, Doc. JBSL-M-01190MDL-01, Issue 4 dated June 20, 2019 or later approved revisions.
(Description of Type Design Change continued on page 3 of 4)
1. The installer must determine whether this design change is compatible with previously approved modifications.
(Limitations and Conditions continued on page 3 of 4)
Date of Application: March 3, 2021
Date of Issuance: May 18, 2023 Date Amended:
Anthony E. Gallo
Manager, International Validation Branch Compliance & Airworthiness Division Title: Aircraft Certification Service
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT Number: ST00112IB
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT (Continuation Sheet) Number: ST00112IB
Description of Type Design Change: (continued from page 1 of 4)
2. Operation must be in accordance with Airplane Flight Manual Supplement, JBSL-M-01190AFM-01, Issue 1, dated June 2019 or later EASA approved revisions.
3. Maintenance must be accordance with Instructions for Continued Airworthiness,
- Doc. No. JBSL-M-01190ICA-10 issue 4, dated August 10, 2022 or later EASA approved revisions.
-Doc. No. JBSL-M-01190ICA-30, issue 3, dated August 10, 2022 or later EASA approved revisions.
Limitations and Conditions: (continued from page 1 of 4)
2. The EASA approved Airworthiness Limitations section of the Instructions for Continued Airworthiness referenced in the Description of the Type Design Section of this STC is mandatory.
3. The aircraft must be operated in accordance with the operations limitations section of the Airplane Flight Manual Supplement referenced in the Description of Type Design section of this STC.
4. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
5. This STC is applicable to all make and models.
(Certification basis continued on page 4 of 4)
United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate IMPORT (Continuation Sheet) Number: ST00112IB
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 for the 737-700,737-800,737-900,737-900ER,737-8 series is shown on TCDS A16WE for parts not changed or not affected by the change.
b. The Type Certification basis for the 737-700,737-800,737-900,737-900ER,737-8 series is shown on TCDS A16WE for parts changed or affected by the change with the following additions:
Equivalent Level of Safety (ELOS) Finding has been made for the following regulation: §25.251 Vibration/Buffeting Compliance Criteria (documented in ELOS Memorandum ST11177IBNY-T-F-1 dated July 23, 2021.
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ADs that name this STC · 0
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