What it approves
Installation of Starlink Aviation In-Flight Connectivity 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.
FAA 8110-2 (10/24) Page 1 of ___ IMPORT ST12354IB PMV Engineering 60 Impasse de Varsovie 82000 Montauban, France Part 25 Title 14, Code of Federal Regulations A57NM Embraer S.A.
ERJ 190-100 ECJ, ERJ 190-100 IGW ERJ 190-100 LR, ERJ 190-100 STD
1. This STC is applicable to all serial numbers for the applicable models.
(See Limitations and Condiions on page 3 of 3 07/04/2025 03/27/2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3
1. Installation of Starlink Aviation In-Flight Connectivity System in accordance with PMV Engineering Master Document List SCA-01900-MDL-S01-R01, dated May 22, 2025, or later EASA approved revision.
(See Description of Type Design Change continued on page 3 of 3)
2. Maintenance in accordance with PMV Engineering Instructions for Continued Airworthiness SCA-01900-ICA-S01-R00, dated March 4, 2026, or later EASA accepted revision.
3. Operated in accordance with Aircraft Flight Manual Supplement SCA-01900-AFMS-R01, dated May 21, 2025, or later EASA approved revision.
2. Maintenance must be in accordance with the Airworthiness Limitations Section of the Instructions for Continued Airworthiness identified in the Description section of this STC.
3. Operation must be in accordance with the Limitations section of the Aircraft Flight Manual Supplement identified in the Description section of this STC.
4. The installer must determine whether this design change is compatible with previously approved modifications.
5. 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.
Certification Basis:
The certification basis for this modification is based upon Part 25 as specified in Type Certificate Data Sheet (TCDS) A57NM, except for the areas changed or affected by the design change, for which the certification basis is the TCDS plus:
An equivalent level of safety finding has been made for the following regulation:
14 CFR 25.251(b) - use of a combination of aerodynamic analysis and flight test in lieu of flight test to the conditions required by 25.251(b), documented in ELOS Memorandum ST20729IB-T-25.251(b)
This modification has been substantiated to be a no acoustic change in accordance with 14 CFR
21.93(b).
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ADs that name this STC · 0
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