# STC SA00442WI-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
- Applied: June 13, 1996
- Status date: April 15, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3)
- Certificate PDF: https://openairdocs.org/files/sha256/d5/3a/d53a3ee4ca53b1532a5fe0ba83e9b66acc023bf4204e51c1790b8b073567e1f9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/85AE6FCD2E975B0E86258614005246EA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00442WI-D

## ADs that name it (0)

None.

## Approved models (1)

- Mooney Aircraft Corporation M20J ([TCDS 2A3](https://openairdocs.org/tcds/2A3))

## 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: SA00442WI-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: Mooney Model:

2A3

M20J Serial Numbers 24-3000and after

Installation of the Bendix/King KAP140 Automatic Flight Control System.

REQUIRED DATA: 1. Master Drawing List 159-08155-0001, Rev. 2, dated 3-7-97; and 2. Airplane Flight Manual Supplement 006-00849-0000, Rev. 0, dated 3-21-97.

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: 6-13-96 Date Reissued: 2-28-00; 4-15-20

Date of Issuance: 3-21-97 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 2 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- April 15, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d5/3a/d53a3ee4ca53b1532a5fe0ba83e9b66acc023bf4204e51c1790b8b073567e1f9)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a7/ee/a7eeefa07475d4ffd7e1011d5d4efb8d3f2de56951b928a8b7cfd7845ca3677b)

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