# STC SA11224DS

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc., United States
- Description: Rockwell Collins Pro Line Fusion phase 2 or 3 as installed in a Textron Aviation B200GT/B200CGT aircraft satisfies the airworthiness requirements necessary to support operational approval of Category II approach procedures
- Applied: November 20, 2017
- Status date: April 19, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/0a/03/0a034dff422b76ae1c266b9ec663baec804893e8514a84d279eaafec354411d2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID178174158020230511131459.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA11224DS

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA11224DS This certificate issued to: Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215

Part 23* of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Textron Aviation Model: B200GT, B200CGT A24CE

Description of Type Design Change: Rockwell Collins Pro Line Fusion phase 2 or 3 as installed in a Textron Aviation B200GT/B200CGT aircraft satisfies the airworthiness requirements necessary to support operational approval of Category II approach procedures. Required data: 1. Master Data List (MDL) No. 605-00-0001, Rev. A, dated 10/12/2018, or later FAA approved revision; 2. Airplane Flight Manual Supplement (AFMS) No. 605-00-0027, Rev. C, dated 9/21/2018, or later FAA approved revision; 3. Instructions for Continued Airworthiness (ICA) No. 605-00-0028, Rev. IR, dated 10/1/2018, or later FAA accepted revision.

1. The installer must determine whether this design chan ge is compatible with previously approved modifications.

2. 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.

3. The STC assumes Rockwell Collins Pro Line Fusion Phase 2 or 3 is already installed on each airplane eligible for the proposed modification.

4. The STC assumes Litef LCR-100 AHRS is already installed on each airplane eligible for the proposed modification.

Date of Application: November 20, 2017 Date Reissued: 4/19/2023

Date of Issuance: October 15, 2018 Date Amended:

Signature Title for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service

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

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SA11224DS

To (Name and address of transferee)

From (Name and address of grantor)

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

Number: SA11224DS

Date reissued: 4/19/2023

*New 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 the Textron Aviation B200GT/B200CGT aircraft with Rockwell Collins Pro Line Fusion phase 2 or 3 as installed in a Textron Aviation B200GT/B200CGT aircraft satisfies the airworthiness requirements necessary to support operational approval of Category II approach procedures is as follows:

a. The type certification basis for Textron Aviation Model B200GT/B200CGT airplanes is as shown on TCDS A24CE 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, November 20, 2017, include:

Regulations at the latest amendment 23-0 through 23-64:

14 CFR § 23.771(a), 23.777(a)(b), 23.1431(b), 23.1525, 23.1555(a).

Regulations at an intermediate amendment:

14 CFR § 23.1303(c) amendment 23-49.

Exemptions from 14CFR part 23: None.

Equivalent safety findings exist with respect to the following regulations: None.

Special conditions: None.

Special Federal Aviation Regulations: None.

-------------- END -------------

## Every issue (2)

- April 19, 2023: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0a/03/0a034dff422b76ae1c266b9ec663baec804893e8514a84d279eaafec354411d2)
- October 15, 2018: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/3c/25/3c25ef851ad295149ce7a9940bebbd02176f228b486bda844da81b89d27e4667)

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