# STC ST04508CH - Type: Supplemental type certificate - Status: Current, Issued - Holder: StandardAero Business Aviation Services LLC, United States - Description: Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM System and a KuKa Radome in accordance with Master Data List (MDL), 1039410, Revision (F), dated November 05, 2021, or later FAA Approved Revision. - Applied: November 6, 2021 - Status date: November 6, 2021 - Product: Aircraft - Certification basis: Part 21 - Data sheets: [TCDS T00005NY](https://openairdocs.org/tcds/T00005NY) - Certificate PDF: https://openairdocs.org/files/sha256/19/6a/196acb2e4184b82201e7c2e8dba05bd7e45430f5efd7684334b7f332544b2bdd - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E0C85A68D22D4A7D8625878F00591E05.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST04508CH ## ADs that name it (0) None. ## Approved models (1) - Bombardier Inc. BD-100-1A10 (Challenger 300) ([TCDS T00005NY](https://openairdocs.org/tcds/T00005NY)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. VIAT United States of America Department of Transportation Federal Aviation Administration TOAMISTRATO Supplemental Type Certificate Number: ST04508CH This certificate issued to: StandardAero Business Aviation Services, LLC 1200 North Airport Drive Springfield, IL 62707 Part 25 of the Federal Aviation Regulations. Original Product Make: Bombardier Inc. Type Certificate Number: T00005NY Model: BD-100-1A10 Description of Type Design Change: Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM System and a KuKa Radome in accordance with Master Data List (MDL), 1039410, Revision (F), dated November 05, 2021, or later FAA Approved Revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. Equivalent Level of Safety Findings have been made for the following regulations(s): 14 CFR 25.251(b) Vibration and Buffeting (documented in ELOS Memorandum ST10384CH-T-F-1) 3. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. An STC holder who allows a person to alter an aircraft, aircraft engine, or propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: _ ST04508CH (Continuation Sheet) Description of Type Design Change: (continued) FAA Approved Airplane Flight Manual Supplement, 1040118, Revision (A), dated August 30, 2021, or later FAA Approved Revision is a required part of Configuration 01 installation. FAA Approved Airplane Flight Manual Supplement, 1039574, Revision (A), dated August 30, 2021, or later FAA Approved Revision is a required part of Configuration 02 installation. FAA Approved Airplane Flight Manual Supplement, 1040319, Revision (C), dated September 28, 2021, or later FAA Approved Revision is a required part of Configuration 03 installation. FAA Approved Airplane Flight Manual Supplement, 1040322, Revision (B), dated September 09, 2021, or later FAA Approved Revision is a required part of Configuration 03 installation. The aircraft must be maintained in accordance with FAA approved Instructions for Continued Airworthiness, 1040134, Revision (A), dated October 01, 2021, or later FAA approved revision in addition to the basic airplane maintenance manuals. Certification Basis (continued) Based on 14 CFR §§ 21.101, 21.115 and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for the Bombardier Inc. BD-100-1A10, Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM System and a KuKa Radome is as follows: a. The type certification basis for Bombardier Inc. BD-100-1A10 is shown on TCDS T00005NY 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, January 21, 2021, is based upon TCDS T00005NY. Based on 14 CFR § 21.101 and 21.115, and the FAA policy for significant changes in FAA Order 8110.48A, the certification basis for this modification was determined to be: Regulations at the amendment level in TCDS T00005NY 25.1(a, b)(Original), 25.143(a)(25-84), 25.161(c(3))(25-38), 25.251(a-d)(25-77), 25.301(a, b)(25-23) 25.303(25-23), 25.305(a, b)(25-86), 25.307(a) (25-72), 25.331(a-c)(25-86), 25.333(a, b)(25-86) 25.335(a-d)(25-91), 25.337(a-d)(25-23), 25.341(a, b)(25-86), 25.349(a, b)(25-94) 25.351(a-d)(25-91), 25.365(a, b, d)(25-87), 25.561 (a-c)(25-91), 25.571(a-c)(25-96) 25.581(a, c)(25-23), 25.601(Original), 25.603(a-c)(25-46), 25.605(a)(25-46), 25.607(a-c)(25-23) 25.609(a, b) (Original), 25.611(25-23), 25.613(a-d)(25-72), 25.619(a-c)(25-23), 25.625(a-d)(25-72) 25.629(a, b(1, 2))(25-77), 25.773(a(2))(25-72), 25.777(a)(25-46), 25.853(a(1)) (25-83) 25.869(a(4)) (25-72), 25.1301(a-d)(Original), 25.1307(c)(25-72), 25.1309(a, b, d, g)(25-41) 25.1322(d)(25-38), 25.1351(a)(25-72), 25.1353(a, b)(25-42), 25.1357(a, c)(Original) 25.1381(a, b)(Original), 25.1401(a, b)(25-41), 25.1419(a)(25-72), 25.1431(a, c) (Original) 25.1501(a, b)(25-42), 25.1519(Original), 25.1529(25-54), 25.1581(a(2), d)(25-72) 25.1583(c)(25-105), 25.1585(a, b)(25-105), 25.1587(b)(25-105) Possession on this Supplemental Type Certificate (STC) document by persons other than instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. An STC holder who allows a person to alter an aircraft, aircraft engine, or the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine, or propeller. The STC's supporting documentation (drawings. propeller must provide that person with written permission acceptable to the FAA. (Ref. 14 CFR 21.120). FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 3 of 3 ## Every issue (1) - November 6, 2021: Issued, Current. [certificate](https://openairdocs.org/files/sha256/19/6a/196acb2e4184b82201e7c2e8dba05bd7e45430f5efd7684334b7f332544b2bdd) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.