# STC ST10891SC-D - Type: Supplemental type certificate - Status: Current, Issued - Holder: Dassault Falcon Jet Corp., United States - Description: Avionics and Interior Installations in accordance with Data List Report No. F2EX-01039 Revision B dated April 13, 2011, or later FAA approved revision. FAA Approved AFM Supplement, Report 37159-F2EX-D514 dated April 14, 2011 or later FAA approved revision is required. Supplemental Maintenance Manual, Report SMM F2000EX - SN 216, revision Original, dated January 21, 2011 or later FAA approved revision is required. Supplemental Illustrated Part Catalog, Report SIPC F2000EX- SN 216, revision C, dated April 13, 2011 or later FAA approved revision is required. Supplemental Wiring Diagram Manual, Report F2MB-001-D514, revision E, dated April 5, 2011 or later FAA approved revision is required. - Applied: December 8, 2011 - Status date: April 14, 2011 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A50NM](https://openairdocs.org/tcds/A50NM) - Certificate PDF: https://openairdocs.org/files/sha256/58/01/5801649aadfd2f23faa2fcd47303d0560419154bb49f84bd20e79a55ba8a9f2f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8A813BCE8D570092862578B10061DA96.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST10891SC-D ## ADs that name it (0) None. ## Approved models (1) - Dassault Aviation FALCON 2000EX ([TCDS A50NM](https://openairdocs.org/tcds/A50NM)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number ST10891SC-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-01039 Revision B dated April 13, 2011, or later FAA approved revision. FAA Approved AFM Supplement, Report 37159-F2EX-D514 dated April 14, 2011 or later FAA approved revision is required. Supplemental Maintenance Manual, Report SMM F2000EX - SN 216, revision Original, dated January 21, 2011 or later FAA approved revision is required. Supplemental Illustrated Part Catalog, Report SIPC F2000EX- SN 216, revision C, dated April 13, 2011 or later FAA approved revision is required. Supplemental Wiring Diagram Manual, Report F2MB-001-D514, revision E, dated April 5, 2011 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. 216. This STC does not permit manufacturing of parts for multiple installations. Date of application: December 8, 2010 Date of issuance: April 14, 2011 (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 ST10891SC-D Issue Date: April 14, 2011 FAA Form 8110-2-1 (10-68) PAGE 3 of 3 PAGES Description of Type Design Change (Continued): (None) (None) Certification Basis: Based on 14 CFR ยงยง 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 7, data January 3, 2011, 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 25.341 (a),(b),(c) 25-86 25.365 (a),(b),(c), (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),(e),(j) 25-54 25.785 (a),(c),(d), (k),(l) 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), (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)(1),(2), (3),(4),(c) 25-72 25.981 (a)(3),(b) **25-102 SECT. PARA. AMDT.** 25.1301 (a),(b), 25.1307 (c) 25-72 25.1309 (a),(b),(d), (e),(f),(g) 25-41 25.1351 (a)(1) 25-72 25.1353 (a),(b) 25-42 25.1355 (a) 25-38 25.1357 (a),(c) O 25.1411 (a),(b),(d) (e),(f),(g) 25-79 25.1415 (a),(b),(c), (d) 25-82 25.1431 (c) O 25.1438 (a),(b),(c) 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 (g) 25-54 END ## Every issue (1) - April 14, 2011: Issued, Current. [certificate](https://openairdocs.org/files/sha256/58/01/5801649aadfd2f23faa2fcd47303d0560419154bb49f84bd20e79a55ba8a9f2f) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.