# STC SA00560DE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of a L3/ACSS TCAS-2000 (Traffic Alert and Collision Avoidance System).
- Applied: March 22, 2004
- Status date: December 14, 2016
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/56/e0/56e0a029aa2444e97266ec2f747d480e16094d03f74b237d4f22f875d12ddcc8
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BA3BA6DC16BE136B8625814D006EDEC7.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00560DE

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Hawker Beechcraft Corporation 1900D ([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

Part of the

Signature

Title Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 SA00560DE Federal Aviation Regulations. * 23* A24CE 1900C, 1900D * Certification basis is set forth in Type Certificate Data Sheet A24CE.

Installation of a L3/ACSS TCAS-2000 (Traffic Alert and Collision Avoidance System) in accordance with Genesis 3 Engineering Master Drawing List, Document No. GEN-040311-002, Revision A, dated September 2, 2004, FAA approved September 23, 2004, or later FAA approved revision.

Raytheon

1. This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of these other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that airplane.

(see continuation sheet 3 of 3) October 25, 2005; May 29, 2007;

December 14, 2016 January 5, 2005; May 13, 2005 March 22, 2004 September 23, 2004 Mark Fuller STC ODA administrator ODA-100129-CE

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

To (Name and address of transferee)

From (Name and address of grantor)

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

Date of Issuance: September 23, 2004 Date Amended: May 13, 2005 Date Reissued: December 14, 2016

2. Instructions for Continued Airworthiness, Document No. GEN-040311-016, Revision IR, dated May 5, 2004, FAA accepted dated June 22, 2004, or later FAA approved revision is required for this installation.

3. A copy of this certificate and FAA approved Flight Manual Supplement, Document No. GEN-040311-020, Revision IR, dated September 23, 2004, or later FAA approved revision must be maintained as part of the permanent records of the modified aircraft.

4. 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 -- SA00560DE 3

## Every issue (3)

- December 14, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/56/e0/56e0a029aa2444e97266ec2f747d480e16094d03f74b237d4f22f875d12ddcc8)
- May 29, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6f/f2/6ff2b596c85810f99a060ea9add77c9ad100a8dd85e23c6c4726c26fa802af58)
- October 25, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f2/b5/f2b58e5ba11d88e538fd6a7022e7ffcd99a6852fbe04fe7187e8acf86e4cc48d)

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