STC ST04574NY

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

IMPORT ST04574NY Elisen & associes Inc.

440 Boul. Armand-Frappier, Suite 200 Laval, Quebec Canada H7V 4B4 Part 25 the Title 14 Code of Federal Regulations A59NM Dassault Aviation Falcon 7X S/N 0113

1. Installation of Interior Reconfiguration must be accomplished in accordance with Elisen & associes Inc.

Modification Data Summary MDS-3039 Revision A, TCCA approved on November 20, 2019.

2. Duncan Aviation Airplane Flight Manual Supplement CERTDOC-010306 Revision A, TCCA approved on November 13, 2019, is required as part of this modification.

(See Description of Type Design Change continued on Page 3 of 3)

1. The installer must determine whether this design change is compatible with previously approved modifications.

(See Limitations and Conditions continued on Page 3 of 3) March 18, 2020 January 8, 2021 Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance & Airworthiness Division Aircraft Certification Service 3

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number:

IMPORT ST04574NY 3

FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number:

IMPORT ST04574NY Date of Issuance: January 8, 2021

Description of Type Design Change (continued):

3. The aircraft is to be maintained in accordance with the Duncan Aviation Instructions for Continued Airworthiness CERTDOC-010142 Revision A, TCCA accepted on November 20, 2019 or later TCCA accepted revisions.

2. You cannot use descriptive data from this design change to duplicate other products.

This approval is limited to only the installation made in Dassault Aviation Falcon 7X S/N 0113. This STC does not permit manufacturing of parts for multiple installations.

3. The "Limitations" section of Duncan Aviation Airplane Flight Manual Supplement CERTDOC-010306 Revision A, TCCA approved on November 20, 2019, is applicable as part of this modification.

4. Mandatory replacement times and/or inspection intervals are defined in the "Airworthiness Limitations" section of the Duncan Aviation Instructions for Continued Airworthiness CERTDOC-010142 Revision A, TCCA approved on November 20, 2019.

5. This STC is only applicable to Dassault Aviation Falcon 7X S/N 0113.

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