STC ST10887SC-D

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number ST10887SC-D

3801 East 10 th Street Little Rock, Arkansas 72202-3366

Part 25 of the Federal Aviation Regulations.

A50NM Dassault Aviation Make:

Model: Falcon 2000EX Avionics and Interior Installations in accordance with Data List Report No. F2EX-01037 Revision C dated November 19, 2010, or later FAA approved revision.

FAA Approved AFM Supplement, Report 37159-F2EX-D246 dated November 22, 2010 or later FAA approved revision is required.

Supplemental Maintenance Manual, Report SMM F2000EX - SN 218, revision Original, dated October 1, 2010 or later FAA approved revision is required.

Supplemental Illustrated Part Catalog, Report SIPC F2000EX- SN 218, revision A, dated November 11, 2010 or later FAA approved revision is required.

Supplemental Wiring Diagram Manual, Report F2MB-001-D246, revision F, dated November 3, 2010 or later FAA approved revision is required.

You cannot use descriptive data about this design change to duplicate other products. This approval is limited to only the installation made in Dassault Aviation Model 2000EX Serial No. 218.

This STC does not permit manufacturing of parts for multiple installations.

Date of application: September 20, 2010

Date of issuance: November 22, 2010

Date reissued: November 22, 2010

(Signature)

Robert J. Feazell ODA-700141-SW STC ODA administrator (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP code)

Signature of grantor (in ink):

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number ST10887SC-D Issue Date: November 22, 2010

FAA Form 8110-2-1 (10-68) PAGE 3 of 4 PAGES Description of Type Design Change (Continued):

(None)

(None)

Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Falcon 2000EX (LX Definition) aircraft fitted with this STC is as follows.

The certification basis for this STC same as stated in Type Certification Data Sheet (TCDS) A50NM, Revision 6, data April 29, 2009, for Falcon 2000EX

SECT. PARA. AMDT.

25.1 (a),(b) O

25.29 25-72

25.301 (a),(b),(c) 25-23

25.303 - 25-23

25.305 (a),(b),(c) 25-86

25.307 (a) 25-72

25.337 (a),(b),(c) 25-23

25.341 (a),(b),(c) 25-86

25.365 (a),(e),(g) 25-87

25.561 (a),(b),

(c),(d) 25-64

25.562 (c)(5) 25-64

25.571 (a),(b) 25-96

25.601 - O

25.603 (a),(b),(c) 25-46

25.605 (a) 25-46

25.609 (a),(b) O

25.611 - 25-23

25.613 (a),(b),(c),

(d),(e) 25-72

25.619 (a),(b),(c) 25-23

25.623 (a),(b) O

25.625 (a),(b),

(c),(d) 25-72

25.777 (a) 25-46

25.783 (b),(j) 25-54

(e) 25-88

25.785 (a),(c),(d),(g) 25-88 SECT. PARA. AMDT.

25.787 (a),(b),(c) 25-51

25.789 (a),(b) 25-46

25.791 (a),(b),(c),

(d),(e) 25-72

25.793 - 25-51

25.803 (e),(1),(2) 25-46

25.807 (b) 25-67

25.809 (b),(d) 25-47

25.811 (a),(b),(c),

(1),(2),(g) 25-46

25.812 (a),(c),(d),

(e),(i) 25-58

25.813 (a),(b),(c)

(2),(e),(f) 25-46

25.815 - 25-38

25.817 - 25-15

25.831 (a),(b) 25-41

25.851 (a)(1),(2),

(3),(5),(7),(8) 25-74

25.853 (a),(c),(f),

(g),(h) 25-83

25.855 (d),(e),(f),(g ) 25-93

25.856 (a) 25-111

25.869 (a)(4),(c) 25-72

25.981 (a)(3) 25-102 SECT. PARA. AMDT.

25.1301 (a),(b),(c),(d) O

25.1307 (c) 25-72

25.1309 (a),(b),(d),

(e),(f),(g) 25-41

25.1351 (a)(1) 25-72

25.1353 (a) 25-42

25.1355 (a) 25-38

25.1357 (a),(c) O

25.1411 (a),(b),(d)

(f),(g) 25-79

25.1415 (a),(b),(c),(d) 25-82

25.1431 (c) O

25.1438 (b) 25-41

25.1439 (a) 25-38

25.1447 (c) (1) 25-41

25.1529 - 25-54

25.1541 (a),(b) O

25.1557 (a),(c),(d) 25-72

25.1561 (a),(b),(c),(d) ,(e) 25-46

25.1581 (a),(b),(d) 25-72 H25.1 (a),(b),(c) 25-54 H25.2 (a),(b) 25-54 H25.3

(e),(f),(g) 25-54 END