# STC SA947CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of King Radio KFC-300 automatic flight control system (integrated flight director and autopilot).
- Applied: May 8, 1973
- Status date: March 26, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A2PC](https://openairdocs.org/tcds/A2PC)
- Certificate PDF: https://openairdocs.org/files/sha256/31/a6/31a6d3910b6fa5681f744778f719a74743c81cda4af9ea9a78ed1ee16395fb5b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C5B7A9489D1E75978625862900735DCE.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA947CE

## ADs that name it (0)

None.

## Approved models (1)

- Mitsubishi Heavy Industries Ltd. MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))

## 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: SA947CE This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 10of the Civil Air Regulations.

Original Product – Type Certificate Number: Make: Mitsubishi Heavy Industries, Ltd.

A2PC MU-2B-35

Installation of King Radio KFC300 Automatic Flight Control System (integrated flight director and autopilot). Data Required: King top drawing #155-9008-00, dated May 8, 1973, Rev. 2 or Rev. 4, dated July 27, 1974, or later FAA approved revision and data referenced therein and including FAA Approved Flight Manual Supplement dated September 11, 1973 or later FAA approved revision.

Limited to Model MU-2B-35 airplaneshaving shelving, gyros, pitch trim & five-volt lighting installed in accordance with STC’s SA1470SW, SA1545SW, SA1641SW & SA1703SW. This approval should not be extended to other specific airplanes of 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 the airplane.

Date of Application: 5-8-73 Date Reissued: 1-31-95; 2-28-00; 3-26-20

Date of Issuance: 9-11-73 Date Amended:

8-30-75; 1-14-76

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: SA947CE

Limitationsand Conditions: (continued) 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.

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## Every issue (2)

- March 26, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/31/a6/31a6d3910b6fa5681f744778f719a74743c81cda4af9ea9a78ed1ee16395fb5b)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d5/6e/d56e921dee2fde6a10d9d1d8b478a54758a131561f4212d768cf4b1fb84d31df)

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