# STC SA1570CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis flight control system.
- Applied: July 1, 1982
- Status date: March 18, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12)
- Certificate PDF: https://openairdocs.org/files/sha256/3e/96/3e968500230b960e8e663e6fc6fc06c15c6609ab1d7067e10949ddd26042d734
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EB5D3B34C0CF9FC1862586160067B16B.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1570CE-D

## ADs that name it (1)

- [AD 85-23-07](https://openairdocs.org/ad/85-23-07): Autopilot Systems · Aerostar PA-60-700P (Aerostar 700P), 172L, 172P and 37 more. Effective Jan 27, 1986. Cited in the text

## Approved models (3)

- Textron Aviation Inc. 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Textron Aviation Inc. 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Textron Aviation Inc. 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12))

## 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 3 Number: SA1570CE-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 3A12 Model: 172N, 172P and 172Q Description of Type Design Change:

Installation of KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis Flight Control System.

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.

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: 7-1-82 Date Reissued: 2-28-95; 2-28-00; 3-18-20 Date of Issuance: 9-17-82 Date Amended: 11-19-90 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1570CE-D

FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued) REQUIRED DATA:

KAP 100 Single Axis Flight Control System I. Master Drawing List 155-9255-00, Rev. 3, dated 10-22-90.

2. Airplane Flight Manual Supplement 006-0412-00, Rev. 1, dated 11-19-90.

KAP 150 and KFC 150 Two Axis Flight Control System I. Master Drawing List 155-9255-00, Rev. 3, dated 10-22-90.

2. Airplane Flight Manual Supplement 006-0412-01, Rev. 1, dated 11-19-90.

Later FAA approved revisions to above listed data are incorporated without further revision to the Supplemental Type Certificate.

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## Every issue (2)

- March 18, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3e/96/3e968500230b960e8e663e6fc6fc06c15c6609ab1d7067e10949ddd26042d734)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a7/62/a7622efe30f95b517a703f8ac48633817ec335f0055990b225c84770e725752e)

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