# STC SA1134CE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Honeywell International Inc, United States - Description: Installation of King Model KFC-200 2-axis (3 optional), flight control system or optional KC-291 yaw damper controller - Applied: January 20, 1975 - Status date: April 6, 2020 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21 - Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16) - Certificate PDF: https://openairdocs.org/files/sha256/ce/f1/cef1b099930962cf60820a8d8312733b487af0321bc23eff6431b3afd5e08a0b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/366B4218F9447CB286258615005C4CDD.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1134CE ## ADs that name it (0) None. ## Approved models (10) - Textron Aviation Inc. 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Textron Aviation Inc. E55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) ## 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 3 Number: SA1134CE This certificate issued to: Honeywell International Inc. 21111 N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations. Make: Beech 3A16 Model: 95-55, 95-A55, 95-B55, 95-B55A, 95-C55, D55, E55, E55A, 58, 58A Description of Type Design Change: Installation of King Model KFC 200, 2 axis (3 optional) Flight Control System or optional KC 291 Yaw Damper Controller. Data Required: 1. Master Drawing List 155-9032-00, Revision 19, dated December 1, 1979, or Master Drawing List 155-9032- 01, Revision 1, dated April 14, 1980. 2. Installation Manual 006-0200-00, Revision 4, dated December 1, 1979, or Installation Manual 005-0200-02, Revision 1, dated April 14, 1980. 3. Appropriate FAA Approved Airplane Flight Manual Supplement as listed on Continuation Sheet, or later FAA 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 inter-relationship 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: 1-20-75 Date Reissued: 1-31-95; 2-28-00; 4-6-20 Date of Issuance: 4-18-75 Date Amended: 6-19-75; 6-25-75; 8-26-75; 4-29-76; 6-7-76; 6-18-76; 3-10-77; 6-7-77; 2-12-80; 6-3-80; 10-5-82; 11-3-82 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM FAA Form 8110-2 (5/14) Page 2 of 3 To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1134CE FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued) FAA Approved Airplane Flight Manual Supplements: Airplane Model King Part No./Date Original AFMS King Part No./Date AFMS for use with KI 256 King Part No./Date AFMS for use with KG 258 and KC 292 E55/E55A 006-0300-00/4-18-75 006-0300-00/3-10-77 006-0300-01/6-7-77 95-B55 006-0303-00/6-19-75 006-0303-00/3-10-77 006-0303-01/6-7-77 58 006-0304-00/6-25-75 006-0304-00/3-10-77 006-0304-01/6-7-77 95-A55 006-0321-00/4-29-76 006-0321-00/11-1-79 006-0321-01/11-1-79 D55 006-0320-00/6-7-76 006-0320-00/3-10-77 006-0320-01/6-7-77 95-C55 006-0331-00/6-18-76 006-0331-00/3-10-77 006-0331-01/6-7-77 95-55 006-0321-00/4-29-76 006-0321-00/11-1-79 006-0321-01/11-1-79 E55/E55A 006-0385-00/5-1-80 006-0385-01/5-1-80 95-B55/95-B55A 006-0385-10/5-1-80 006-0385-11/5-1-80 58/58A 006-0385-20/5-1-80 006-0385-21/5-1-80 95-A55 006-0385-40/5-1-80 006-0385-41/5-1-80 D55 006-0385-30/5-1-80 006-0385-31/5-1-80 95-C55 006-0385-50/5-1-80 006-0385-51/5-1-80 95-55 006-0385-40/5-1-80 006-0385-41/5-1-80 ---------------------------------------------------------------------------END-------------------------------------------------------------------------- ## Every issue (2) - April 6, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/ce/f1/cef1b099930962cf60820a8d8312733b487af0321bc23eff6431b3afd5e08a0b) - February 28, 2000: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/ab/84/ab8414fa7c6009afe36fa8b647d974be27214efc493e943e469da7b035ccfedf) --- 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.