# STC SA1487CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of King KFC200 Automatic Flight Control System, two axis, with or without flight director.
- Applied: February 27, 1979
- Status date: April 3, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A21](https://openairdocs.org/tcds/3A21)
- Certificate PDF: https://openairdocs.org/files/sha256/14/03/14039118034dc6a1d359ba2afb0bf7b4e9a97b445c7f668081a45192be5b132c
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5F4FA8C762FDB8E1862585CA00675950.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1487CE

## ADs that name it (1)

- [AD 80-21-03](https://openairdocs.org/ad/80-21-03): Roll Axis Flight Control · King Model KFC-200 two axis flight control system (Honeywell International STC SA1202CE or SA1487CE). Effective Oct 23, 1980. Named in the applicability

## Approved models (1)

- Textron Aviation Inc. P210N ([TCDS 3A21](https://openairdocs.org/tcds/3A21))

## 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.

FAA Form 8110-2 (5/14) Page 1 of 2 Number: SA1487CE This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations.

Original Product – Type Certificate Number: Make: Cessna 3A21 Model: P210N Description of Type Design Change:

Installation of King KFC 200 Automatic Flight Control System, two axis, with or without Flight Director.

REQUIRED DATA: 1. King Master Drawing List 155-9131-00, Rev. 1, dated 4-12-79, 2a. Airplane Flight Manual Supplement 006-0373-00, approved 5-1-79 or 2b. Airplane Flight Manual 006-0373-01, approved 5-1-79 or later FAA Approved revisions to 1, 2a or 2b.

This approval should not be extended to other specific airplanes of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those previously approved modifications will introduce no adverse effect upon the airworthiness of 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: 2-27-79 Date Reissued: 1-31-95; 2-28-00; 4-3-20 Date of Issuance: 5-1-79 Date Amended:

By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

FAA Form 8110-2 (5/14) Page 2 of 2

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

## Every issue (2)

- April 3, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/14/03/14039118034dc6a1d359ba2afb0bf7b4e9a97b445c7f668081a45192be5b132c)
- February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/d3/92/d392f893c4d00a8c3d7ab2cca6022cd021c959cf723367c6036517d7f26b2ff1)

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