# STC SA00063WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King CAS 66A TCAS I System, or provisions for CAS 66A TCAS I System.
- Applied: May 10, 1993
- Status date: April 8, 2020
- Product: Aircraft, Large Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A21EU](https://openairdocs.org/tcds/A21EU)
- Certificate PDF: https://openairdocs.org/files/sha256/36/e2/36e22a7a0e2ce9e935da1801030c3340c00a65c41f08d527a5c0d72d2f5dd732
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/72131226AA721E3C86258625007588BF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00063WI-D

## ADs that name it (0)

None.

## Approved models (1)

- British Aerospace (Scotland) HP Jetstream Model 3101 ([TCDS A21EU](https://openairdocs.org/tcds/A21EU))

## 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 2 FAA Form 8110-2 (5/14)

Number: SA00063WI-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: British Aerospace Model:

A21EA Jetstream Model 3101

Installation of Bendix/King CAS66A TCASI System, or Provisions for the CAS66A TCASI System.

REQUIRED DATA: 1. Master Drawing List 155-09655-0000, Rev. 4, dated 1-4-95 and 2. Airplane Flight Manual Supplement 006-00831-0000, Rev. 0, dated 2-17-95(AFMSnot required where only provisions are installed). Later FAA approved revisionsto the above listed data are incorporated without further revision to this Supplemental Type Certificate.

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.

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.

Date of Application: 5-10-93 Date Reissued: 2-13-95; 2-28-00; 4-8-20

Date of Issuance: 5-14-93 Date Amended:

2-17-95

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 2 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- April 8, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/36/e2/36e22a7a0e2ce9e935da1801030c3340c00a65c41f08d527a5c0d72d2f5dd732)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/fa/ab/faab5c0b7e337abc3c9cf17c41eaaf66e201654f1a97265294d0603339b58546)

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