# STC SA00321BO - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Pro Star Aviation, LLC, United States - Description: Installation of a Thrane &Thrane AVIATOR 200 SwiftBroadband System - Applied: May 5, 2011 - Status date: October 15, 2018 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A78EU](https://openairdocs.org/tcds/A78EU) - Certificate PDF: https://openairdocs.org/files/sha256/4d/a2/4da2af48f378506b80eed16d78fb794d0b7e6d85212275f0b1c5bb03e3af3a58 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B85BBAB641C0A3B2862583580063AF87.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00321BO ## ADs that name it (0) None. ## Approved models (3) - Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) - Pilatus Aircraft Limited PC-12/47E ([TCDS A78EU](https://openairdocs.org/tcds/A78EU)) ## What the certificate says Some pages are OCR from the scanned FAA certificate. OCR can misread letters and numbers. •FEDERAL AVIATION United States of America Department of Transportation CAVISTRATO Federal Aviation Administration Supplemental Type Certificate Number: SA00321BO This certificate issued to: Pro Star Aviation, LLC 8 Kelly Avenue Londonderry, NH 03053 Part 23 of the Federal Aviation Regulations. Original Product - Type Certificate Number: A78EU Make: Pilatus Model: PC-12/45, PC-12/47, and PC-12/47E Description of Type Design Change: Installation of a Thrane & Thrane AVIATOR 200 SwiftBroadband System in accordance with Pro Star Aviation Installation Data List 21037-IDL-01, revision D, dated November 14, 2012, or later FAA approved revision. 1. Operation must be in accordance with Pro Star Aviation Airplane Flight Manual Supplement 21037-FMS-01, revision A, dated November 19, 2012, or later FAA approved revision. The AFMS must be carried in the aircraft during all flights. 2. Maintenance is to be performed in accordance with Pro Star Aviation Instructions for Continued Airworthiness 21037- ICA-01, revision B, dated November 6, 2012, or later FAA accepted revision. The ICA must be made available to the operator at the time of installation. 3. Compatibility of this design change with other previously approved modifications must be determined by the installer. (See continuation on page 3 of 3) Date of Application: May 5, 2011 Date Reissued: October 15, 2018 Date of Issuance: March 19, 2012 Date Amended: November 26, 2012 By Direction of the Administrator Signature Title Douglas M. England Lead ODA Administrator - Pro Star Aviation, LLC ODA-833063-NE The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder. FAA Form 8110-2 (5/14) Page 1 of 3 The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. . FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number : SA00321BO To (Name and address of transferee) From (Name and address of grantor) The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is th e property of the STC holder. . FAA Form 8110-2 (5/14) Page 3 of 3 (Continuation Sheet) Number: SA00321BO Limitations and Conditions: (continued): 4. The data services provided by the installed system are intended for internet connection and email services using portable electronic devices. Any other intended function using the system's data service will require a re-examination of the certification basis. Certification Basis: Based on 14 CFR §§ 21.115 and 21.101, and FAA Order 8110.48 policy for non-significant changes, the certification basis for the installation of the Thrane & Thrane AVIATOR 200 SwiftBroadband System in Pilatus PC-12/45, PC-12/47, and PC-12/47E aircraft is as follows: a. The type certification basis for Pilatus PC-12/45, PC-12/47, and PC-12/47E aircraft is shown in TCDS A78EU for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change is as follows: Regulations at the amendment level in TCDS A78EU For all models: 14 CFR §§ 23.1, 23.3, 23.29, 23.251, 23.303, 23.307, 23.321, 23.341, 23.561(a)(b(l))(c(1)(2))(d)(e), 23.601, 23.603, 23.605, 23.609, 23.611, 23.619, 23.623, 23.625, 23.627, 23.771, 23.853, 23.867, 23.1301, 23.1309, 23.1322(d), 23.1351, 23.1357(c), 23.1367, 23.1381, 23.1419, 23.1501, 23.1529, 23.1541, 23.1581, G23.1-G23.4. For PC-12/47E model: 14 CFR §§ 23.301, 23.305, 23.561(b(2)(3))(c(3)), 23.613, 23.629, 23.773, 23.1 322(e), 23.1357(a), 23.1365(b)(d)(e), 23.1431. Regulations at an amendment level 23-49 For all models: 14 CFR §§ 23.1359 For PC-12/45 and PC-12/47 models: 14 CFR §§ 23.301, 23.305, 23.561(b(2)(3))(c(3)), 23.571, 23.613, 23.629, 23.773, 23.1 322(e), 23.1357(a), 23.1359, 23.1365(b)(d)(e), 23.1431. --------------------------------------------------------------------- END ----------------------------------------------------------------------- ## Every issue (3) - October 15, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4d/a2/4da2af48f378506b80eed16d78fb794d0b7e6d85212275f0b1c5bb03e3af3a58) - November 26, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/48/36/48364a2c7b274b5ec824153d5823dbbdc941aff739d7663955cf426bd81bcde5) - March 19, 2012: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/45/d7/45d7d2bae2ee5ffc7e956fede31ee2edd9aeaad18b60ee597031d5a2aece7d92) --- 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.