# STC SA1771CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of King KFC 200 flight control system (2 axis), with or without flight director
- Applied: January 18, 1983
- Status date: March 21, 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/e6/a1/e6a14f24ad8c001d7e533967dfa4d19c7b9bfe7a3c26486733fd3f55bf1ae4e3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/84229556CA57EA138625861E007A36C9.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1771CE-D

## ADs that name it (1)

- [AD 85-25-02](https://openairdocs.org/ad/85-25-02): Autopilot Systems · King Radio Autopilot Systems, M20J, M20K and 1 more. Effective Jan 27, 1986. Cited in the text

## Approved models (2)

- Mooney Aircraft Corporation M20J ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20K ([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: SA1771CE-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, s/n 24-1368, 24-14-19and up M20K, s/n 25-0740, 25-0791and up

Installation of King KFC200 Flight Control System (2 axis), with or without Flight Director.

REQUIRED DATA: King Master Drawing List 155-9279-00dated 3-1-83 or later FAA approved revision.

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 any 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: 1-18-83 Date Reissued: 2-28-95, 2-28-00, 3-21-20

Date of Issuance: 3-8-83 Date Amended:

3-18-83

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 2 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

## Every issue (2)

- March 21, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e6/a1/e6a14f24ad8c001d7e533967dfa4d19c7b9bfe7a3c26486733fd3f55bf1ae4e3)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/74/34/7434093a7508ff4cf4fce4f870a5b62e2a834749acb693fefc0c150f6c3e2d34)

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