STC SA1776CE-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA1776CE-D This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations.

Original Product – Type Certificate Number: Make: Beech Model:

3A16 E55

Installation of a King KNS660 Multi-Sensor Flight Management System with or without the optional KLN 670 Global Positioning System Sensor.

This approval includesairplanesequipped with the King KFC200 or KFC325 Automatic Flight Control Systemsinstalled in accordance with Supplemental Type Certificates SA1134CEor SA2055CE-D respectively.

Date of Application: 7-21-83 Date Reissued: 2-28-95; 2-28-00; 4-9-20

Date of Issuance: 8-23-83 Date Amended:

4-12-85; 1-14-86; 12-7-87

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SA1776CE-D

Description of Type Design Change: (continued) REQUIRED DATA:

KNS600 Multi-Sensor System without KLN 670 Global Positioning System Sensor:

1. Master Drawing List 155-9293-00, Rev. 3, dated 4-12-85.

2. Airplane Flight Manual Supplement 006-0427-00, Rev. 1, dated 4-12-85.

3. Pilot's Guide 006-08394-00issued 11-15-84for systemscontaining ORS1 software or 006-08407-00issued 12-2-85for systems containing ORS2 software.

KNS600 Multi-Sensor System with KLN 670 Global Positioning System Sensor:

1. Master Drawing List 155-9293-00, Rev. 5, dated 10-16-87.

2. Airplane Flight Manual Supplement 006-0427-00, Rev. 2, dated 12-7-87.

3. Pilot's Guide 006-8407-00, Rev. 1, dated 11-11-87.

Later FAA approved revisionsto items 1 or 2 or later revisionsto items 3 above are incorporated without further revision to the Supplemental Type Certificate.

Limitationsand Conditions: (continued)

This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof 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.

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