# STC ST10656SC-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Dassault Falcon Jet Corp., United States - Description: Galley Annex Structure Installation in accordance with Data List Report No. F00-01012 Revision P dated 1-Sept-2011 or later FAA approved revision. - Applied: February 8, 2008 - Status date: March 1, 2012 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A46EU](https://openairdocs.org/tcds/A46EU), [TCDS A50NM](https://openairdocs.org/tcds/A50NM) - Certificate PDF: https://openairdocs.org/files/sha256/98/a2/98a2757fb5c75a886b945d838d46dc9bfabaf3b76cc9058e2544f79cefcc486d - Approved model list and other attachments: [ST10656SC-D_AML.pdf](https://openairdocs.org/files/sha256/85/57/8557617377b01b3801ea3ea753617bd41a767eea6d11cfd463f1e40d21923c67) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C4B7230FB1374866862579CD005FDC63.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST10656SC-D ## ADs that name it (0) None. ## Approved models (2) - Dassault Aviation FALCON 2000EX ([TCDS A50NM](https://openairdocs.org/tcds/A50NM)) - Dassault Aviation Falcon 900EX ([TCDS A46EU](https://openairdocs.org/tcds/A46EU)) ## 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 ST10656SC-D 3801 East 10 th Street Little Rock, Arkansas 72202-3366 Part 25 of the Federal Aviation Regulations. See attached FAA Approval Model List (AML), Document No. 40848, revision A, or later FAA approved airplane models, applicable installation data requirements and specific limitations. Make: Model: Galley Annex Structure Installation in accordance with Data List Report No. F00-01012 Revision R dated 21-Feb-2012 or later FAA approved revision. See page 3 Compatibility of this modification with other previously approved modifications must be determined by the installer. 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. See page 3 Date of application: February 8, 2008 Date of issuance: July 18, 2008 Date reissued: 7-Sept-2011 Date amended:4-Jan-2010 Rev 1, 7-Sept-2011 Rev 2, 1-Mar-2012 Rev 3 (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 ST10656SC-D Revision 3 Issue Date: 1-Mar-2012 FAA Form 8110-2-1 (10-68) PAGE 3 of 3 PAGES Description of Type Design Change (Continued): Maintenance Manual Supplement, Report 37419, revision B, dated 18-July-20007 or later FAA accepted revision. Maintenance Manual Supplement, Report 37420, revision B, dated 11-June-2007 or later FAA accepted revision. Maintenance Manual Supplement, Report 37918, revision A, dated 4-Aug-2007 or later FAA accepted revision. Maintenance Manual Supplement, Report 37919, revision A, dated 5-Aug-2007 or later FAA accepted revision. Maintenance Manual Supplement, Report 37928, revision NC, dated Feb 2008 or later FAA accepted revision. The installer is required to consider the following items for regulatory compliance. Galley Annex Installation Requirements use Report 38445, revision NC, dated 13-May-2008, or later FAA approved revision which includes the following: – Final cabin interior arrangement requires FAA authorized interior compliance inspector. – Flammability approval for the honeycomb panel coving material such as wood veneer, laminate, sound and thermal insulation is required. – The Electrical Systems and Mechanical Systems approved are not included. – The STC includes the structural substantiation of the floor beam strength below the galley. – Maximum stowage weight placarding is not to exceed approved limits. – Verification of FAA approved upper support is present between the Galley Annex and fuselage. 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 this STC is stated in Type Certification Data Sheet (TCDS) A50NM, Revision 7, data January 3, 2011, for Falcon 2000EX and as stated in Type Certification Data Sheet (TCDS) A46EU, Revision 16, data October 27, 2011, for Falcon 900EX **SECT. PARA. AMDT.** 25.1 (a),(b) O 25.301 (a),(b),(c) 25-23 25.303 - 25-23 25.305 (a),(b),(c), (d),(e),(f) 25-86 25.307 (a),(d) 25-72 25.321 (a),(b),(c), (d) 25-86 25.333 (a) 25-86 25.337 (a),(b),(c), (d) 25-23 25.341 (a),(b) 25-86 25.365 (e),(f), (g) 25-87 25.561 (a),(b)(3) (ii),(c),(d) 25-64 **25.601 - O SECT. PARA. AMDT.** 25.603 (a),(b),(c) 25-46 25.605 (a),(b) 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 25.787 (a),(b) 25-51 25.789 (a) 25-46 25.801 (b) 25-72 25.803 (a) 25-46 25.831 (a),(b),(c) 25-41 SECT. PARA. AMDT. 25.1301 (a),(b), 25.1309 (a),(b),(c), (d) 25-41 25.1519 - O 25.1529 - 25-54 25.1541 (a),(b) O H25.1 (a),(b),(c) 25-123 H25.2 (a),(b) 25-54 H25.3 (g) 25-54 END ### ST10656SC-D_AML.pdf Report No: 40848 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 1 of 5 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 **APPROVED MODEL LIST (AML)** ST10656SC-D Galley Annex Structural Installation **REPORT REVISION LEVEL** ISSUE DATE PREPARED BY ODA APPROVED REL NC 16-AUG-11 Kenny Chidester Robert Feazell 11-4258 A 24-Jan-2012 Report No: 40848 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 2 of 5 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 ISSUE PAGE DESCRIPTION OF CHANGE NC Initial Release of report (No Changes) A 3 Added 505 Installation to System Description 4 Updated Limitation and Conditions Revised areas are denoted by change bar. Report No: 40848 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 3 of 5 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 ST10656SC-D Galley Annex Structural Installation Dassault Falcon Jet Corp. 3801 East 10th Street Little Rock, Arkansas 72202-3366 System Description F00-01012-501 This project specifies the structural installation of a monument (Galley Annex) on the left hand side of the aircraft in the aircraft main entry door area. This cabinet typically contains a variety of storage and equipment including general storage, microwave oven, glasses, china, and entertainment equipment. The weights for the various equipment are accounted for in this project but the specific equipment are separately approved. The bottom of the cabinet is designed to duct conditioned air from the basic aircraft system to the aisle. This project evaluates what is intended as a “worst case” design and load distribution. Subsequent installations will be determined to be adequate by comparison to the first article certification. F00-01012-503 The -503 installation is for additional testing to define the interaction curve between shear and tension loading of potted inserts in DFJ honeycomb panels. The previously approved -501 installation is required. F00-01012-505 The -505 installation is for additional testing to define the panel bending in DFJ honeycomb panels. The previously approved -505 installation is required. Report No: 40848 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 4 of 5 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 Certification Basis Item Aircraft Make Aircraft Model Type Certificate Number Certification Basis for Alteration Certification Data List Configuration Installation Instructions Airplane Flight Manual Supplement Maintenance Manual Supplement 1 Dassault Aviation Falcon 2000EX A50NM CFR 25 F00-01012-501 38445 Not Applicable 37928 Rev NC, 37918 Rev A, 37919, Rev A, 37419 Rev B, 37420 Rev B 2 Dassault Aviation Falcon 900EX A46EU CFR 25 F00-01012-501 38445 Not Applicable 37928 Rev NC, 37918 Rev A, 37919, Rev A, 37419 Rev B, 37420 Rev B 3 Dassault Aviation Falcon 2000EX A50NM CFR 25 F00-01012-503 38445 Not Applicable 37928 Rev NC, 37918 Rev A, 37919, Rev A, 37419 Rev B, 37420 Rev B 4 Dassault Aviation Falcon 900EX A46EU CFR 25 F00-01012-503 38445 Not Applicable 37928 Rev NC, 37918 Rev A, 37919, Rev A, 37419 Rev B, 37420 Rev B 5 Dassault Aviation Falcon 2000EX A50NM CFR 25 F00-01012-505 38445 Not Applicable 37928 Rev NC, 37918 Rev A, 37919, Rev A, 37419 Rev B, 37420 Rev B 6 Dassault Aviation Falcon 900EX A46EU CFR 25 F00-01012-505 38445 Not Applicable 37928 Rev NC, 37918 Rev A, 37919, Rev A, 37419 Rev B, 37420 Rev B Limitations and Conditions: The installer is required to consider the following items for regulatory compliance. Galley Annex Installation Requirements use Report 38445, revision NC, dated 13-May-2008, or later FAA approved revision which includes the following: – Final cabin interior arrangement requires FAA authorized interior compliance inspector. – Flammability approval for the honeycomb panel coving material such as wood veneer, laminate, sound and thermal insulation is required. – The Electrical Systems and Mechanical Systems approved are not included. – The STC includes the structural substantiation of the floor beam strength below the galley. – Maximum stowage weight placarding is not to exceed approved limits. – Verification of FAA approved upper support is present between the Galley Annex and fuselage. FAA Approved: Robert J. Feazell STC ODA Administrator Report No: 40848 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 5 of 5 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 Dassault Falcon Jet Corp. ## Every issue (2) - March 1, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/98/a2/98a2757fb5c75a886b945d838d46dc9bfabaf3b76cc9058e2544f79cefcc486d), [ST10656SC-D_AML.pdf](https://openairdocs.org/files/sha256/85/57/8557617377b01b3801ea3ea753617bd41a767eea6d11cfd463f1e40d21923c67) - September 7, 2011: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/8c/0a/8c0ad5b6f79d39613cf82f13b4716dd82a43eedafc9b0fcde05bccd5e58938f8), [ST10656SC-D AML.pdf](https://openairdocs.org/files/sha256/e6/78/e6785ff68d275ae7ee2e3bd4daa3ee869cc6e7e8beb14779262dc0545a74acc3) --- 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.