# STC SA1780CE-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Install King KFC flight control system two or three axis,with or without flight director
- Applied: October 18, 1983
- Status date: April 8, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A23CE](https://openairdocs.org/tcds/A23CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a6/a5/a6a5385d4bde84e2ebf2c0006c4c87d2e23147686834f9a3422d3cbd69a611c3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/409EC44E377729018625860D005495AD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1780CE-D

## ADs that name it (0)

None.

## Approved models (4)

- Textron Aviation Inc. 58P ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Textron Aviation Inc. 58PA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Textron Aviation Inc. 58TC ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))
- Textron Aviation Inc. 58TCA ([TCDS A23CE](https://openairdocs.org/tcds/A23CE))

## 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: SA1780CE-D This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 23of the Federal Aviation Regulations.

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

A23CE

58TC, 58TCA, s/n TK-147, TK-151 and after 58P, 58PA, s/n TJ-436, TJ-444 and after

Install King KFC200 Flight Control System, two or three axis, with or without Flight Director.

REQUIRED DATA: 1. King Master Drawing List 155-9286-00dated 7-20-83, and 2. Airplane Flight Manual Supplement (a) 006-0409-00, approved 11-18-83or (b) 006-0409-01approved 11-18-83, or later FAA approved revisionsto 1, 2a or 2b.

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: 10-18-83 Date Reissued: 2-28-95; 2-28-00; 4-8-20

Date of Issuance: 11-18-83 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 8, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/a6/a5/a6a5385d4bde84e2ebf2c0006c4c87d2e23147686834f9a3422d3cbd69a611c3)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/81/85/8185ca37d7d7d93aa8cdc553ae055c1d5d4c8bb36e0810e0864a91f1362366fa)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.