# STC SA01352CH

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Elliott Aviation Technical Products, United States
- Description: Installation of a Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II) in accordance with Elliott Aviation Master Data List, No. 2026-576DL, Revision 8, dated January 6, 2011, or later FAA approved revision.
- Applied: March 30, 2000
- Status date: January 6, 2011
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/35/a7/35a7c49ddb29863d31cbc158b2f04494cedf6ce2ff4bf7294731deb8e20019fd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/86589291B1551D5686257840007AFE6F.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01352CH

## ADs that name it (0)

None.

## Approved models (18)

- Hawker Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (C-12R) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12F) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200C (UC-12M) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200CGT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200CT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200GT ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B200T ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation B300C (C-12W) ([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.

Part 23 of the Federal Aviation Regulations.

Installation of a Rockwell Collins TCAS 4000 Traffic Alert and Collision Avoidance System (TCAS II) in accordance with Elliott Aviation Master Data List, No. 2026-576DL, Revision 8, dated January 6, 2011, or later FAA approved revision.

1) Compatibility of this design change with previously appr oved modifications must be determined by the installer.

2) FAA Approved Airplane Flight Manual Supplement, Elliott Aviation Doc. No. TCAS4000FMS, Revision 0, approved December 4, 2000, or TCAS4000MFD-85CFMS, Revision 0, approved December 4, 2000, as appropriate for the installed configuration, or later FAA approved revision, is required on board the aircraft modified per Configuration 1.

3) FAA Approved Airplane Flight Manual Supplement, Elliott Aviation Doc. No. FS2026-576, Revision 2, approved December 6, 2010, or later FAA approved revision, is required on board the aircraft modified per Configuration 2.

Elliott Aviation Technical Products, Inc.

PO Box 100 Quad City Airport Moline, IL 61266-0100 A24CE Make : Raytheon Aircraft Company (Beech) Model : 200; 200C; 200CT; 200T; B200; B200C; B200CT;

B200T; 300; B300; 300LW; B300C, B200GT, B200CGT

Date of application : March 30, 2000

Date of issuance : December 4, 2000

Date amended : October 27, 2004; January 6, 2011

( Signature) Steven L. Lardinois Manager, Systems and Flight Test Branch Chicago Aircraft Certification Office

( Title)

FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES

Number SA01352CH

Date Amended: January 6, 2011

Limitations and Conditions : (Continued from Page 1 of 3)

4) FAA approved Airplane Flight Manual Supplement, Elliott Aviation Doc. No. FS2026-344, Revision 0, approved October 26, 2004, or later FAA approved revision, is required on the aircraft modified per Configuration 3.

5) FAA Approved Instructions for Continued Airworthiness, Chapter 10 – Airworthiness Limitations, Elliott Aviation Report No.

CA2026-576, Revision 5, FAA approved January 6, 2011, or later FAA approved revision, is required for this modification.

6) If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

- END -

## Every issue (1)

- January 6, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/35/a7/35a7c49ddb29863d31cbc158b2f04494cedf6ce2ff4bf7294731deb8e20019fd)

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