# STC SA00444WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King KAP 140 Automatic Flight Control System with optional KCS 55A Compass System
- Applied: February 21, 1997
- Status date: April 15, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A13](https://openairdocs.org/tcds/2A13)
- Certificate PDF: https://openairdocs.org/files/sha256/45/c0/45c011e9d69dda624349bf72fd05c8092b6b4ab79c70e501ed683d5e840dfcdd
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1F729EF5164822B5862586140053D723.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00444WI-D

## ADs that name it (0)

None.

## Approved models (1)

- The New Piper Aircraft Inc. PA-28-181 ([TCDS 2A13](https://openairdocs.org/tcds/2A13))

## 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: SA00444WI-D This certificate issued to: Honeywell International Inc.

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

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

2A13

PA-28-181, Serial Numbers 2890206through 2890231and 2843001and after.

Installation of the Bendix/King KAP140 Automatic Flight Control System with optional KSC55A CompassSystem.

REQUIRED DATA:

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: 2-21-97 Date Reissued: 2-28-00; 4-15-20

Date of Issuance: 3-21-97 Date Amended:

1-5-98

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: SA00444WI-D

Description of Type Design Change: (continued) REQUIRED DATA:

KAP140 Two Axis Flight Control System

1. Master Drawing List 159-08158-0001, Rev. 2, dated 3-18-97.

2. Airplane Flight Manual Supplement 006-00850-0000, Rev. 0, dated 3-21-97.

KAP140 Single Axis Flight Control System

1. Master Drawing List 159-08158-0001, Rev. 4, dated 8-28-97.

2. Airplane Flight Manual Supplement 006-00850-0001, rev. 0, dated 1-5-98.

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

------------------------------------------------------------------------------------END--------------------------------------------------------------------------------

## Every issue (2)

- April 15, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/45/c0/45c011e9d69dda624349bf72fd05c8092b6b4ab79c70e501ed683d5e840dfcdd)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f3/28/f32837441012238434fa02d8d74c9bc321c3bae5252b5291552493fec9af6cb3)

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