# STC SA1164CE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of King KFC-200 two axis autopilot system with King KI-255 (or -256) flight command indicator or King KG-258 altitude horizon indicator with a KC-292mode controller.
- Applied: August 15, 1975
- Status date: February 28, 2000
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/96/f2/96f280c172157f191874990e29ff4f2682903515ee829b3b298b2c6aa10f41d3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/5CCB6B037683D51485256CC10080DF28.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA1164CE

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company F33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA1164CE / This certificate issued to: Honeywell International Inc.

23500 W. 105"h Street Olathe, KS 66061 Part 3 of the CiVil Ait Regulalions Original Product - Type Cerlificate Number: ЗА15 Make: Beech Model: F33A Description of Type Design Change:

Installation of King KFC 200, 2 axis autopilot system with a King KI 255 (or KI 256) Flight Command Indicator or a King KG 258 Attitude Horizon Indicator with a KC 292 Mode Controller.

REQUIRED DATA: 1. King Master Drawing List 155-9044-00 Rev. 8 dated 5-20-77. 2. Installation Manual 006-0203-00 Rev. 3 dated 4-29-77. 3. FAA Approved Airplane Flight Manual Supplement a. 006- 0308-00 no revision dated 9-12-75. b. 006-0308-00 Rev. 3 dated 3-31-77, for KI 256 or c. 006-0308-01 no revision dated 5-20-77, for KG 258 or later FAA Approved Revisions of 1, 2, or 3.

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.

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendereds suspended, revoked or a lermination dale is herwise established by the Administrator of the Federal Aviation Administration Date of Application: 8-15-75 Date Reissued: 1-31-95; 2-28-00 Date of Issuance: 9-17-75 Date Amended: 4-20-77; 7-25-71 FEDERAL AVIATION By Direction of the Administrator (Signature) * Chris Durkin TOMNISTRATO DAS Coordinator, DAS-500863-CE (Title) 47

## Every issue (1)

- February 28, 2000: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/96/f2/96f280c172157f191874990e29ff4f2682903515ee829b3b298b2c6aa10f41d3)

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