STC SA2317CE-D

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA2317CE-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 4b of the Civil Air Regulations.

Original Product – Type Certificate Number: Make: Avions Marcel Dassault (AMD) A7EU Model: Fanjet Falcon Series C, D, E, F Mystere-Falcon 20-C5, 20-D5, 20-E5, 20-F5 Description of Type Design Change:

Installation of dual Bendix/King KAD 480 Air Data Systems.

REQUIRED DATA for Fanjet Falcon Series C, D, E and Mystere-Falcon 20-C5, 20-D5, 20-E5: 1. Master Drawing List 155-09546-0000, Rev. 8, dated 5-90 and 2. Airplane Flight Manual Supplement 006-00493-0000, Rev. 1, dated 4-19-90 or later FAA approved revision to 1 or 2.

REQUIRED DATA for Fanjet Falcon Series F and Mystere-Falcon 20-F5: 1. Master Drawing List 155-09546-0000, Rev. 8, dated 5-90 and 2. Airplane Flight Manual Supplement 006-00494-0000, Rev. 0, 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.

(See 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.

Date of Application: 3-9-89 Date Reissued: 2-28-95; 2-28-00; 4-2-20 Date of Issuance: 4-10-89 Date Amended: 4-19-90; 6-14-90 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: SA2317CE-D

FAA Form 8110-2 (5/14) Page 3 of 3 Limitations and Conditions: (continued)

2. A third altimeter meeting t he requirement of FAR 25.1303(b)(2) must be installed.

3. A third airspeed indicator m eeting the requirements of FAR 25.1303(b)(1) (unless an airspeed indicator and a placard of Vmo/Mmo limits is provided and installed in lieu of the requirements of 25.1303(b)(1) must be installed.

4. This approval inclu ded evaluation of the interface between the Bendix/King EFS 10 EFIS, KFC 400 AFCS, KAD 480 Air Data, KNS 660 FMS and Series III Communication/Navigation/Identification (CNI) Systems.

5. This modification is approve d for installation only when a concurrent modification is made in accordance with STC SA2322CE-D (Bendix/King KFC 400 Automatic Flight Control System).

6. This approval should not be extended to other specific airpl anes 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 other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

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