STC SA1150CE

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA1150CE This certificate issued to: Honeywell International Inc.

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

Make: Beech A23CE Model: 58P, 58TC, 58PA, 58TCA Description of Type Design Change:

Installation of King Model KFC 200, 2 axis (optional 3 axis and KC 291 Yaw Damper) Flight Control System with a Kl 255 (KI 256 optional) Flight Command Indicator or a KG 258 Attitude Horizon Indicator with a KC 292 Mode Controller.

REQUIRED DATA: 1. King Master Drawing List 155-9039-00, Rev. 11, dated 5-4-77, and Master Drawing List 155-9039-01, Rev. 1, dated 4-29-80. 2. Installation Manual 006-0200-00, Rev. 3, dated 4-15-77 and Installation Manual 006-0200-02, Rev.

1, dated 4-29-80. 3. Appropriate FAA Approved Airplane Flight Manual Supplement as listed on the Continuation Sheet, 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.

Date of Application: 7-14-75 Date Reissued: 1-31-95; 2-28-00; 4-6-20 Date of Issuance: 8-8-75 Date Amended: 2-27-76;11-1-76;6-7-77; 6-2-80; 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: SA1150CE

FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued) REQUIRED DATA:

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 58P 006-0306-00/8-8-75 006-0306-00/5-4-77 006-0306-01/6-7-77 58TC 006-0306-00/2-27-76 006-0306-00/5-4-77 006-0306-01/6-7-77 58TCA 006-0306-00/10-15-76 006-0306-00/5-4-77 006-0306-01/6-7-77 58PA 006-0306-00/9-23-76 006-0306-00/5-4-77 006-0306-01/6-7-77 59P 006-0386-00/5-1-80 006-0386-01/5-1-80 58TC 006-0386-00/5-1-80 006-0386-01/5-1-80 58TCA 006-0386-00/5-1-80 006-0386-01/5-1-80 58PA 006-0386-00/5-1-80 006-0385-01/5-1-80 ---------------------------------------------------------------------------END--------------------------------------------------------------------------