STC ST04437CH

Supplemental type certificate · Stellar Blu Solutions LLC

Holder
Stellar Blu Solutions LLC · United States
Status
Current · Reissued
Status date
June 28, 2021
Applied
October 11, 2019
Product
Aircraft · Large Airplane
Certification basis
Part 25
Data sheet
TCDSA16WE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of a Dual Modem K/Ka-Band SATCOM Terminal and Wireless Cabin System

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.

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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
The Boeing Company737-700 SeriesA16WE
The Boeing Company737-700C SeriesA16WE

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
June 28, 2021Reissued, currentCertificate
June 28, 2021Amended, earlier issueCertificate