# STC ST00198BO

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Pro Star Aviation, LLC, United States
- Description: Installation of Universal Avionics Systems Corporation Flat-Panel Integrated Display System in accordance with Pro Star Aviation Master Document List, Document Number 0304-MDL-10, dated June 1, 2004, or later FAA-approved revision.
- Applied: September 20, 2003
- Status date: September 13, 2018
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE)
- Certificate PDF: https://openairdocs.org/files/sha256/30/e5/30e5374e1226b536202b7e2c5941754c711998192f111242cd6126853f218c82
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F004BA505B1E22FA8625832200556221.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/ST00198BO

## ADs that name it (0)

None.

## Approved models (1)

- The Cessna Aircraft Company S550 ([TCDS A22CE](https://openairdocs.org/tcds/A22CE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00198BO This certificate issued to: Pro Star Aviation, LLC 8 Kelly Avenue Londonderry, NH 03053 Part 25 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: A22CE Make: Cessna Aircraft Company Model: S550 Citation S/II Description of Type Design Change:

Installation of Universal Avionics Systems Corporation Flat-Panel Integrated Display System in accordance with Pro Star Aviation Master Document List, Document Number 0304-MDL-10, dated June 1, 2004, or later FAA-approved revision.

1. Pro Star Aviation Flight Manual Supplement, Document Number 0304-FMSI 10, dated June 18, 2004, or later FAA- approved revision, is required and must be catTied in the aircraft during all flights.

2. The Instructions for Continued Airworthiness, Document Number 0304-ICA-10, Revision IR, dated March 8, 2004 shall be made available to the operator at the time of installation.

3. Compatibility of this design with previously approved modifications must be determined by the installer.

(See continuation on page 3 of 3)

Date of Application: September 20. 2003 Date Reissued: September 13, 2018 Date of Issuance: June 18. 2004 Date Amended:

By Direction of the Administrator Signature Kevin Dickert Title Manager, Boston ACO Branch

FAA Form 8110-2 (5/14) Page 1 of 3

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST00198BO To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

(Ref. 14 CFR 21. 120).

FAA Form 8110-2 (5/14) Page 2 of 3

United States of America Department of Transportation Federal Aviation Administration INISTRATDO Supplemental Type Certificate (Continuation Sheet) Number: ST00198BO Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48. the certification basis for installation of a Universal Avionics Systems Corporation Flat-Panel Integrated Display System in Cessna S500 Citation S/II aircraft is shown on TCDS A22CE.

Special Condition No. 25-ANM-120, High Intensity Radiated Fields (HIRF) Equivalent Level of Safety is applied to § 25.1303. HIRF certification conditions are applied in accordance with FAA Notice 8110.71, dated April 2. 1998.

•-- END ---

FAA Form 8110-2 (5/14) Page 3 of 3

## Every issue (2)

- September 13, 2018: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/30/e5/30e5374e1226b536202b7e2c5941754c711998192f111242cd6126853f218c82)
- September 20, 2003: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/b7/57/b757614ed0bdd6c0bf55cce2d27bec1c026c409d403625a24c16c8bb2eb9d14b)

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