# STC ST04437CH - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Stellar Blu Solutions LLC - Description: Installation of a Dual Modem K/Ka-Band SATCOM Terminal and Wireless Cabin System - Status date: June 28, 2021 - Data sheets: A16WE, A16WE - Certificate PDF: https://openairdocs.org/files/sha256/fd/f3/fdf3483ca67389da264d960c6c308146489626a6625fa768fc9c4514724e01b6 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100382860420250804182133.0001 - Page: https://openairdocs.org/stc/ST04437CH ## ADs that name it None. ## Approved models (2) - The Boeing Company 737-700 Series (TCDS A16WE) - The Boeing Company 737-700C Series (TCDS A16WE) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. ST04437CH Stellar Blu Solutions, LLC 2060 Eagle Pkwy. Fort Worth, TX 76177 Part 25 the Federal Aviation Regulations A16WE BOEING 737-700 Series, 737-700C Series Installation of a Dual Modem K/Ka-Band SATCOM Terminal and Wireless Cabin System in accordance with GDC Technics Master Data List B1015-MDL, Revision (L), dated June 14, 2021 or later FAA approved revision. (See Continuation Sheet 3 of 5) October 11, 2019 January 9, 2023 June 30, 2020 June 28, 2021 S. Frances Cox Manager, DSCO Branch, Compliance & Airworthiness Division Aircraft Certification Service 5 ST04437CH 5 ST04437CH Date of Issuance: June 30, 2020 Date Amended: June 28, 2021 Date of Reissuance: January 9, 2023 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. FAA Approved Airplane Flight Manual Supplement document number S010-TP-49, Rev (A) dated June 10, 2020, or later FAA approved revision is a required part of this modification for configuration -01 thru -04 as listed on the MDL. 3. FAA Approved Airplane Flight Manual Supplement document number B1065-TP-49, Rev (A) dated May 17, 2021, or later FAA approved revision is a required part of this modification for configuration -05 as listed on the MDL. 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. Equivalent Level of Safety Findings have been made for the following regulation(s): 14 CFR 25.251(b) Vibration and Buffeting (documented in TSB ELOS Memorandum (ST10078CH-T-F-1). 6. In addition to the basic aircraft maintenance manuals, the aircraft must be maintained in accordance with FAA approved Instruction for Airworthiness ICA Document S010-TP-05, revision (008) Airworthiness Limitations dated June 11, 2021 or later FAA approved revision. 7. In accordance with FAA Seattle Aircraft Certification Office letter dated June 28, 2021 [Refer to 782-21-8795a], this modification is FAA approved as an Alternative Method of Compliance (AMOC) to the requirements of paragraph (g) and (h) of Airworthiness Directive (AD) 2013-19-23 for the area of PSE 53-60-01-2 covered by this STC. ST04437CH Date of Issuance: June 30, 2020 Date Amended: June 28, 2021 Date of Reissuance: January 9, 2023 Certification Basis: Based on 14 CFR §§21.115, 21.101 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for The Boeing Company 737-700 Series, 737-700C Series aircraft Installation of a Dual Modem K/Ka-Band SATCOM Terminal and Wireless Cabin System is as follows: a. The type certification basis for The Boeing Company 737-700 Series, 737-700C Series 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, October 11, 2019, is based upon TCDS A16WE. Based on 14 CFR §§21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for this modification was determined to be: ST04437CH Date of Issuance: June 30, 2020 Date Amended: June 28, 2021 Date of Reissuance: January 9, 2023 Certification Basis (continued): Regulations at the amendment level in TCDS A16WE 25.1(a,b)(25-0), 25.23(a,b)(25-0), 25.29(a,b)(25-72), 25.143(a)(25-84), 25.251(a-d) (25-77), 25.301(a,b)(25-23), 25.303(25-23), 25.305(a-c,e)(25-86), 25.307(a)(25-72), 25.321(a,b)(25-86), 25.331(a-c)(25-91), 25.333(a,b)(25-86), 25.335(a-f)(25-91), 25.337(a-d)(25-23), 25.341(a,b)(25-86), 25.351(a-d)(25-91), 25.365(a-f)(25-87), 25.473(a,b)(25-91), 25.561(a-c)(25-91), 25.571(e1)(25-96), 25.581(a,c)(25-23), 25.601(25-0), 25.603(a-c)(25-46), 25.605(a,b)(25-46), 25.607(a-c)(25-23), 25.609(a,b)(25-0), 25.611(25-23), 25.613(a-d)(25-72), 25.619(a-c)(25-23), 25.625(a-c)(25-72), 25.629(a,d,e)(25-77), 25.841(a)(25-87), 25.855(h2)(25-72), 25.857(c3)(25-60), 25.869(a4)(25-72), 25.1301(a-d)(25-0), 25.1307(c)(25-72), 25.1309(a,b,d,e1,e2,e3i,g)(25-41), 25.1316(a-c)(25-80), 25.1351(a)(25-72), 25.1353(a,b)(25-42), 25.1355(a)(25-38), 25.1357(a,c,d)(25-0), 25.1381(a,b)(25-72), 25.1419(a)(25-72), 25.1431(a,c)(25-0), 25.1501(a,b)(25-42), 25.1519(25-0), 25.1529(25-54), 25.1581(a-d)(25-72), 25.1583(c)(25-72), 25.1585(a,b)(25-46). Regulations at a later amendment level 25.571(a,b1)(25-96), 25.853(a)(25-116), 25.855(c)(25-93). 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 amendments, 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 following regulations 14 CFR §§26.11(c)., (Amdt. No. 26-47(c(1)), (Amdt. No. 26-1). -END- 5 5 ## Every issue (2) - June 28, 2021: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/fd/f3/fdf3483ca67389da264d960c6c308146489626a6625fa768fc9c4514724e01b6) - June 28, 2021: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/5b/2d/5b2d594f8eafa3114bb5e613caae29921da1b30925b5a280efd7a0ab447f643f) --- From OpenAirDocs.org, an independent open copy of FAA data. 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