STC SA2315CE-D

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA2315CE-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 Bendix/King 5 tube EFS 10 Electronic Flight Instrument System.

REQUIRED DATA (Configuration A):

1. Master Drawing List 155-9492 -00, Rev. 2, dated 3-27-89 and 2. Airplane Flight Manual Supplement 006-00491-0000, Rev. 1, dated 4-19-90 or later approved revision to 1 or 2.

(Continued on Continuation Sheet) Limitations and Conditions:

1. Compliance must be shown with applicable Service Bulletins and airplane modifications as listed on the Required 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: 6-13-88 Date Reissued: 2-28-95; 2-28-00; 4-2-20 Date of Issuance: 4-10-89 Date Amended: 4-19-90; 1-9-91 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: SA2315CE-D

FAA Form 8110-2 (5/14) Page 3 of 3 Description of Type Design Change: (continued) REQUIRED DATA (Configuration B) (with Bendix/King KAH 460 AHRS):

1. Master Drawing List 155-9492 -01 Rev. 5, dated 1-91 and 2. Airplane Flight Manual Supplement 006-00491-0000, Rev. 1, dated 4-19-90 (EFS 10) and 3. Airplane Flight Manual Supplement 006-00802-0000, Rev. 0, dated 1-9-91 or later FAA approved revisions to 1, 2 or 3.

Limitations and Conditions: (continued)

2. A third attitude indicator m eeting the requirements specified in FAR 25-1303 (b)(4) must be installed.

3. Installation of the EFS 10 Syst em was evaluated in accordance with CAR 4b (amendment 4b-1 and additional items noted on T.C. Data Sheet A7EU).

4. Compliance has been shown with the following sections of FAR Part 25; 25.1301 (amend. 25-38); 25.1303(b) (amend 25-38);

25.1309 (amend. 25-41); 25.1321(a)(b)(d)(e) (amend. 25-41); 25.1322 (amend. 25-38); 25.1331 (amend. 25-41); 25.1333 (amend. 25-41); 25.1335 (amend. 25-41); 25.1523 (amend. 25-3).

5. This approval included an eval uation and finding of acceptance of the interface between the Bendix/King KFC 400 AFCS, KAD 480 Air data, Serial III Communication/Navigation/Identification (CNI) and KNS 660 FMS Systems.

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.

---------------------------------------------------------------------------END--------------------------------------------------------------------------