STC SA1468SW

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate SA1468SWNumber:

This certificate issued to: Fly-A-Charter, LLC d/b/a Avcon 2 843 Willow Run Airport Ypsilanti, MI 48198 BB__.

Make: Dassault AviationOriginal Product A7EU 7\SH&HUWLILFDWH1XPEHU Fan Jet Falcon Basic, Series C, D, E, F, GModel: Mystere-Falcon 20, Series C5, D5, E5, F5Description of Type Design Change:

Installation of openable window in co-pilot's side and qualifying both existing pilot and new co-pilot windows as emergency exits. Data required:

1. Basic Falcon series C/D/E/F/G only: FAA Approved Drawing List No. 2722, dated March 28, 1972, or later FAA Approved revision.

Continued on page 3.

1. Basic Falcon series C/D/E/F/G only: FAA Approved Airplane Flight Manual Supplement (AFMS) dated May 14, 1972, or later FAA Approved revision is required.

Continued on Page 3.

1/24/75, 7/6/87, 6/10/21August 10, 1971Date of Application: Date Reissued:

4/22/83, 3/23/88, 5/18/89, 12/7/04May 24, 1972Date of Issuance: Date Amended:

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I United States of America Department of Transportation Federal AviationAdministration Supplemental Type Certificate SA1468SWNumber:

Date oI transfer:

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United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA1468SW Date Reissued: June 10, 2021 Airworthiness requirements (*continued from page 1):

Effective December 31, 1953, Amendments 4b-1 through 4b-12, Special Regulations SR-422B plus applicable FAR 25 paragraphs listed on TCDS A7EU.

Type Design Change (continued from page 1):

2. Mystere-Falcon 20 series C5/D5/E5/F5 only: FAA Approved Drawing List, No. 2722, Revision A, dated August 20, 2004, or later FAA Approved revision.

Limitations and Conditions (continued from page 1):

2. Mystere-Falcon 20 series C5/D5/E5/F5 only: FAA Approved Airplane Flight Manual Supplement (AFMS) No. AI204030, Rev (-), dated May 14, 1972, or later FAA Approved revision is required.

3. 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 these other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

4. Compatibility of this design change with previously approved modifications must be determined by the installer.

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