What it approves
Installation of Starlink Aviation 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.
SA02812SE AeroMech Incorporated 3977 Harbour Pointe Blvd SW Mukilteo, WA 98275 Part 23 Title 14, Code of Federal Regulations A37CE Textron Aviation Inc.
208, 208B
1. The installer must determine whether this design change is compatible with previously approved modifications.
2. If the holder agrees to permit another person to use this certificate, the holder shall give the other person written evidence of that permission.
See continuation sheet 3 September 6, 2024 June 30, 2025 ODA Administrator 4 Installation of Starlink Aviation System in accordance with the Required Data:
1. Master Drawing List (MDL) AM0395-DL01-00, Revision -, dated 19 June 2025 or later FAA-approved revision.
2. Instructions for Continued Airworthiness AM0395-IC01-00, Revision -, dated 16 June 2025 or later FAA accepted revision.
SA02812SE June 30, 2025 4
SA02812SE June 30, 2025 Description of Type Design Change (Continued):
3. Airplane Flight Manual Supplement (AFMS) AM0395-FM01-00, Revision -, dated 12 June 2025, or later FAA approved revision.
Limitation and Conditions (Continued):
3. A copy of this certificate must be maintained as part of the permanent records of the modified aircraft.
4. The system installed by this STC is intended to provide a non-essential, non-required internet connection to portable electronic devices (PED). Use of this system for any other purpose or connection of this system to other onboard equipment may require additional regulatory approval.
5. Operational approval to permit use of Portable Electronic Devices (PED) is not part of this STC. Further approvals may be required to allow the operation of PED.
6. This STC is applicable to all serial numbers of Textron Aviation Inc. Model 208 and 208B Series Aircraft.
(Continuation Sheet) Number
FAA 8110-2 (
10/24 )
Page ___ of ___ Certification Basis:
Based on 14 CFR §21.101 and 21.115, and the FAA policy for changed aeronautical products in FAA Order 8110.48, the type certification basis for this modification is as follows:
1. For parts not changed or not affected by this modification see the original certification basis for the Textron Aviation Inc. Model 208 and 208B Series Aircraft, shown on TCDS A37CE.
2. For parts changed or affected by this modification since the date of application, September 6 2024, the certification basis is as follows:
14 CFR Part 23 regulations at the amendment level in TCDS A37CE:
14 CFR 23.251, 23.572, 23.629, 23.1301, 23.1309(a)(c), 23.1419(b).
14 CFR Part 23 regulations at amendment levels through 23-63:
14 CFR 23.1, 23.21, 23.23, 23.25, 23.31, 23.45. 23.61, 23.65(b), 23.301(a)(b), 23.303,
23.305(a)(b), 23.307(a), 23.321, 23.333(a)(b)(c), 23.337(a)(b)(c), 23.341(a), 23.561(a)(b)(3),
23.601, 23.603, 23.605(a), 23.607(a)(b), 23.609, 23.611, 23.613, 23.623(a), 23.625(a)(b)(c),
23.627, 23.771(a), 23.777(a)(b), 23.787(a)(b), 23.853(a)(d)(3)(ii)(iv), 23.867, 23.1351(a)(1)(2),
23.1357(a)(c), 23.1359(c), 23.1365(a)(b)(d)(e), 23.1367, 23.1431(a)(b), 23.1501, 23.1529,
23.1541(a)(b), 23.1555(a), 23.1581(a)(b)(1)(f), 23.1583(m), 23.1585(a)(j).
END
SA02812SE June 30, 2025 4 4 Add Page
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