# STC SA1145CE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Installation of King Model KFC-200 - Applied: June 16, 1975 - Status date: April 6, 2020 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15) - Certificate PDF: https://openairdocs.org/files/sha256/e9/69/e969409ea511c3a62ffbd84e4c52f9ba74c62b566d03ffa3ec7167de315657c0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2909177FE598D80E86258615005DB3FC.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1145CE ## ADs that name it (0) None. ## Approved models (2) - Textron Aviation Inc. 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) - Textron Aviation Inc. A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15)) ## 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: SA1145CE 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: Beech 3A15 Model: 36 and A36 Description of Type Design Change: Installation of King Model KFC 200, 2 axis (3 optional or stand alone yaw damper) for Beech Model A36 S/N E572 and later) Autopilot System with a King KI 255 (KI 256 optional) Flight Command Indicator or a KG 258 Attitude Horizon Indicator with the KC 292 Model Controller. REQUIRED DATA: 1. King Master Drawing List 155-9037-00 Rev. 16 dated 5-20-77, 2. Installation Manual 006-0203-00 Rev. 3 dated 4-29-77, 3. FAA Approved Airplane Flight Manual Supplement for a. Model 36, 006-0323-00 Rev. 1 dated 5-27-76, 006- 0323-00 Rev. 2 dated 3-31-77 for KI 256, 006-0323-01 no Rev. dated 5-20-77 for KG 258; b. Model A36, 006-0305-00 no Rev. dated 7-11-75, 006-0305-00 Rev. 3 dated 3-31-77 for KI 256, 006-0305-01 no Rev. for KG 258, or 006-0345-00 no Rev. dated 5- 20-77 for stand alone yaw damper or later FAA approved rev to 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. Date of Application: 6-16-75 Date Reissued: 1-31-95; 2-28-00; 4-6-20 Date of Issuance: 7-11-75 Date Amended: 10-3-75; 12-30-75; 7-19-76; 4-19-77; 7-25-77 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 6, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/e9/69/e969409ea511c3a62ffbd84e4c52f9ba74c62b566d03ffa3ec7167de315657c0) - February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/b7/4d/b74d31f6c7a8011e5474cf053242435d35c8a320ebb391b35b0c449071fd037e) --- 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.