STC SA1145CE

Supplemental type certificate · Honeywell International Inc

Holder
Honeywell International Inc · United States
Status
Current · Reissued
Status date
April 6, 2020
Applied
June 16, 1975
Product
Aircraft · Small Airplane
Certification basis
Part 3, Part 21
Data sheet
TCDS3A15

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of King Model KFC-200

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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):

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 2

MakeModelData sheet
Textron Aviation Inc.363A15
Textron Aviation Inc.A363A15

Every issue · 2

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
April 6, 2020Reissued, currentCertificate
February 28, 2000Reissued, earlier issueCertificate