STC SA2322CE-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title 3 SA2322CE-D Honeywell International Inc.

21111 N 19th Ave Phoenix Arizona 85027 Civil Air Regulations.4b Installation of dual Bendix/King KFC 400 Automatic Flight Control Systems.

REQUIRED DATA: 1. Master Drawing List 155-9513-01, Rev. 7, dated 5-90 and 2. Airplane Flight Manual Supplement 006-00499-0000, Rev. 1, dated 6-14-90 or later FAA approved revision to 1 or 2.

1. Compliance must be shown with applicable Service Bulletins and airplane modifications as listed on the Required Aircraft Modifications Document 155-09552-0000, Rev. 1, dated 10-89 or later revision.

(Continued on Continuation Sheet) 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

Richard B. Sleigh ODA Administrator, ODA-602216-NM Avionis Marcel Dassault (AMD) Fanjet Falcon Series C, D, E, F Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5 12-20-94; 2-28-00; 3-31-20 6-14-90 11-9-89 4-19-89 A7EU

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

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

3 Limitations and Conditions: (continued)

2. This Approval included an evaluation and finding of acceptance of the interface between the Bendix/King EFS 10 EFIS, KFC 400 AFCS, KNS 660 FMS, KAD 480 Air Data and Series III Communication/Navigation/Identification (CNI) Systems.

3. This modification is approved only with the concurrent installation of modifications as defined by STC SA2317CE-D (Bendix/King KAD 480 Air Data) and STC SA2315CE-D, Configuration “B” (Bendix/King EFS 10 EFIS with Bendix/King KAH 460 AHRS).

4. 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.

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