# STC SA00223WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: ONE ONLY STC, SN BB-41:  Installation of the Bendix/King CAS 67A TCAS II System
- Applied: May 2, 1994
- Status date: April 9, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 21, Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/8b/b5/8bb59ad2b1661a975cd8bd3794f867403f3dbc38a7fa6d972a562df5281906f9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/64EB29F39D941670862586290069942F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00223WI-D

## ADs that name it (0)

None.

## Approved models (1)

- Textron Aviation Inc. 200 ([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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA00223WI-D This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 23of the Federal Aviation Regulations.

Original Product – Type Certificate Number: Make: Beech Model:

A24CE 200

Installation of the Bendix/King CAS67A TCASII System.

REQUIRED DATA: 1. Master Drawing List 155-09584-0000, Rev. 2, dated 9-12-94, and 2. Airplane Flight Manual Supplement 006-00828-0000, dated 10-25-94. Later FAA approved revisionsto the above listed data are incorporated without further revision to this Supplemental Type Certificate.

1. This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof that airplane.

Date of Application: 5-2-94 Date Reissued: 2-28-00; 4-9-20

Date of Issuance: 10-25-94 Date Amended:

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

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

(Continuation Sheet) Number: SA00223WI-D

Limitationsand Conditions: (continued)

2. This Approval islimited to aircraft Serial Number BB-41.

3. The CAS67A TCASII System hasbeen shown to be compatible with, and isapproved for use with, the Collins Model TDR-94D Mode STransponder.

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.

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## Every issue (2)

- April 9, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8b/b5/8bb59ad2b1661a975cd8bd3794f867403f3dbc38a7fa6d972a562df5281906f9)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/e6/2c/e62c8ca52998953205df26631d2d07477a8d118fada918688fdd8d54523b30b5)

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