# STC SA1212CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc
- Description: Installation of King KFC 200 2 axis (3 optional) flight control system with KCS 55/55A compass and King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller or third axis (yaw damper) only, or manual electric trim only
- Status date: April 2, 2020
- Data sheets: 2A3, 2A3
- Certificate PDF: https://openairdocs.org/files/sha256/4c/d2/4cd24ed15203f1ba36f642ccbfe307d06766113acc31bf97dde5e9c691b6e778
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/7B4F28D9381F358586258629007AB6EF.0001
- Page: https://openairdocs.org/stc/SA1212CE

## ADs that name it

- [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

## Approved models (2)

- Mooney Aircraft Corporation M20F (TCDS 2A3)
- Mooney Aircraft Corporation M20J (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 3 FAA Form 8110-2 (5/14)

Number: SA1212CE 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

M20FS/N 22-1305and on, M20JS/N 24-0001thru S/N 24-1093excluding S/N 24-0773& S/N 24-0939 Installation of King KFC200, 2 axis (3 optional) Flight Control System with a KCS55 (or -55A) compassand a King KI 255 (or -256) Flight Command Indicator or a KG258 Attitude Horizon Gyro with KC292 Mode Controller, or third axis(yaw damper) only or Manual Electric Trim only.

REQUIRED DATA: Master Drawing List 155-9066-00Rev. 10 dated 11-28-77stamped FAA Approved and later approved revision, Installation Manual 006-0214-00Rev. 4 dated 11-28-77and later FAA Approved revisions.

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 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: 3-9-76

Date of Issuance: 4-22-76 Date Reissued: 1-31-95; 2-28-00; 4-2-20

Date Amended: 6-29-76; 9-10-76; 10-22-76; 9-8-77; 1-19-78;

3-12-81

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: SA1212CE

Description o f Type Design Change:(continued)

REQUIRED DATA FAA Approved Airplane Flight Manual Supplement (AFMS) as listed, or later FAA Approved revisions.

King Part Number AFMS Airplane Model Rev. No. Dated 006-0318-00 with KI 225 M20F/J 4 11-28-77 with KI 256 M20F/J 4 11-28-77 006-0318-01 with KG258 (Autopilot Only) M20F/J 1 11-28-77 006-0326-00 Yaw Damper System M20F/J 3 11-28-77 006-0329-00 Manual Electric Trim M20F/J 3 11-28-77 ------------------------------------------------------------------------------------END--------------------------------------------------------------------------------

## Every issue (2)

- April 2, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/4c/d2/4cd24ed15203f1ba36f642ccbfe307d06766113acc31bf97dde5e9c691b6e778)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/c3/f3/c3f307e6dbe505de8e5cb4ac5c57bc83b111d711c15ba6f9326c51752c8330f2)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.