# STC SA1573CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of KAP 100 single axis flight control system
- Applied: October 20, 1982
- Status date: March 25, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A24](https://openairdocs.org/tcds/3A24)
- Certificate PDF: https://openairdocs.org/files/sha256/5f/14/5f1481f255b6f386a2bd2f2bee1ac302fc8e3b1e7f760bd53a405ca0c95bc369
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D8BE991B716395A6862585CE006FE137.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1573CE-D

## ADs that name it (0)

None.

## Approved models (1)

- Textron Aviation Inc. A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

## 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: SA1573CE-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations.

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

3A24 A 185F Serial Number 18503154 and above

Installation of KAP 100 single axis Flight Control System.

REQUIRED DATA: King Master Drawing List 155-9264-00 Rev. 1, dated 12-15-82 or later FAA approved revisions.

In addition to the land plane, this approval includes airplanes equipped with amphibious or seaplane floats installed in accordance with Type Certificate 3A24 , Supplemental Type Certificates SA7GL, SA328CE, SA445CE, SA558NW and SA877EA. 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 those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

Date of Application: 10-20-82 Date Reissued: 2-28-95, 2-28-00, 3-25-20

Date of Issuance: 11-3-83 Date Amended:

1-19-83

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: SA1573CE-D

Limitations and Conditions: (continued) 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)

- March 25, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5f/14/5f1481f255b6f386a2bd2f2bee1ac302fc8e3b1e7f760bd53a405ca0c95bc369)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/0d/26/0d2697d99a267bbdd40e7f10c7d56da8255183cda2d5f043254cae65bb4621e7)

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