# STC ST10652SC-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: Dassault Falcon Jet Corp., United States - Description: Galley Cabinet Structural Installation - Applied: September 7, 2007 - Status date: November 27, 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/ea/f9/eaf91659a8f57bfa45c272483f5edb7445efe89d912aa0cb9c91b0f9297eddf8 - Approved model list and other attachments: [ST10652SC-D AML.pdf](https://openairdocs.org/files/sha256/05/5d/055d5577aa4fb66c7b390d6337d4079566158bc8e5e08706b890da7d762b57c8) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1A702F7BA28F1ED786257B1100644399.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST10652SC-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 ST10652SC-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. 40912, revision B, or later FAA approved airplane models, applicable installation data requirements and specific limitations. Make: Model: Galley Cabinet Structural Installation in accordance with Certification Data List Report No. F00-01010 Revision AD dated 16-Nov-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: September 7, 2007 Date of issuance: May 14, 2008 Date amended:4-Jan-2010 Rev 1, 9-Dec-2011 Rev 2, 27-Nov-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 ST10652SC-D Revision 3 Issue Date: 27-Nov-2012 FAA Form 8110-2-1 (10-68) PAGE 3 of 4 PAGES Description of Type Design Change (Continued): Maintenance Manual Supplement, Report 37419, revision B, dated 18-July-2007 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 37914, revision B, dated 4-Jan-2008 or later FAA accepted revision. Maintenance Manual Supplement, Report 37917, revision A, dated 29-Aug-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 37920, revision A, dated 5-Aug-2007 or later FAA accepted revision. Maintenance Manual Supplement, Report 37950, revision NC, dated 31-Aug-2007 or later FAA accepted revision. Maintenance Manual Supplement, Report 38144, revision A, dated 10-Jan-2008 or later FAA accepted revision. The installer is required to consider the following items for regulatory compliance. Galley Installation Requirements use Report 38290, revision NC, dated 13-Mar-2008, or later FAA approved revision which includes the following: – Development of Sudden Decompression Load Report (SDLR) based on the final cabin interior arrangement. – Verification that items placed behind the tambour door is attached to or tied down to the lower surface of the compartment. – Final cabin interior arrangement requires FAA authorized interior compliance inspector. – Verification that an FAA approved upper support is present between the Galley and fuselage. – 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. 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) 25-77 (a),(b),(c) 25-86 25.307 (a),(d) 25-72 25.321 (a),(b) 25-23 25.333 (a) O 25.337 (a),(b),(c),(d) 25-23 25.341 (a),(b),(c) 25-72 25.365 (e),(f), (g) 25-54 25.561 (a),(b),(c) 25-23 **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) 25-23 25.785 (k) 25-88 25.787 (a),(b) 25-51 25.789 (a) 25-46 25.801 (b) 25-72 25.803 (a) 25-46 SECT. PARA. AMDT. 25.813 (a) 25-46 25.831 (a),(b),(c) (d),(e),(f) 25-41 25.1301 (a),(b),(c),(d) O 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 (e),(f),(g) 25-54 United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number FAA FORM 8110-2-1(10-69) PAGE 4 of 4 PAGES END ### ST10652SC-D AML.pdf Report No: 40912 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 1 of 4 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 **APPROVED MODEL LIST (AML)** ST10652SC-D Galley Cabinet Structural Installation **REPORT REVISION LEVEL** ISSUE DATE PREPARED BY ODA APPROVED REL NC 1-DEC-11 CLINT ROPER JOHN ROSS 11-5944 A 6-DEC-11 CLINT ROPER JOHN ROSS 11-6031 Report No: 40912 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 2 of 4 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 ISSUE PAGE DESCRI PTION OF CHANGE NC Initial Release of report (No Changes) A 3 Revised System Description 4 Revised Limitations and Conditions Revised areas are denoted by change bar. Report No: 40912 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 3 of 4 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 ST10652SC-D Galley Cabinet Structural Installation Dassault Falcon Jet Corp. 3801 East 10th Street Little Rock, Arkansas 72202-3366 System Description F00-01010-501 This project specifies the structural installation of a monum ent (Galley) on the right 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, high temp oven, microwave oven, coffee maker, glasses, china, silverware, ice and trash. A pocket door is normally attached to the aft face of the Galley. The weights for the various equipment and the pocket door are accounted for in this project but the specific equipment and door installations 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. F00-01010-503 Galley Cabinet Structural Installation to assess the capacity of inserts to redistribute load to adjacent inserts when loaded close to the failure load. The test objective is to load, on each panel specimen, 3 inserts with a linear imposed deformation so that one insert reaches its load saturation level and measure how the load is then redistributed to the 2 other inserts. Certification Basis Item Aircraft Make Aircraft Model Type Certificate Number Certification Basis for Alteration Certification Data List Configuration Installation Instructions Airplane Flight Manual Supplement Instructions for Continued Airworthiness 1 Dassault Aviation Falcon 2000EX A50NM CFR 25 F00- 01010-501 38290 Not Applicable 37914 Rev B, 37917 Rev A, 37918 Rev A, 37919 Rev A, 37920 Rev A, 37419 Rev B, 37420 Rev B, 37950 Rev NC, 38144 Rev A 2 Dassault Aviation Falcon 900EX A46EU CFR 25 F00- 01010-501 38290 Not Applicable 37914 Rev B, 37917 Rev A, 37918 Rev A, 37919 Rev A, 37920 Rev A, 37419 Rev B, 37420 Rev B, 37950 Rev NC, 38144 Rev A Report No: 40912 Revision No: A Model No: Falcon 2000EX / 900EX Page No: 4 of 4 REFERENCE REV DATE WRITTEN DATE EFFECTIVE FR.7.ENC.049 New 5/16/11 5/16/11 Item Aircraft Make Aircraft Model Type Certificate Number Certification Basis for Alteration Certification Data List Configuration Installation Instructions Airplane Flight Manual Supplement Instructions for Continued Airworthiness 3 Dassault Aviation Falcon 2000EX A50NM CFR 25 F00- 01010-503 38290 Not Applicable 37914 Rev B, 37917 Rev A, 37918 Rev A, 37919 Rev A, 37920 Rev A, 37419 Rev B, 37420 Rev B, 37950 Rev NC, 38144 Rev A 4 Dassault Aviation Falcon 900EX A46EU CFR 25 F 00-01010-503 38290 Not Applicable 37914 Rev B, 37917 Rev A, 37918 Rev A, 37919 Rev A, 37920 Rev A, 37419 Rev B, 37420 Rev B, 37950 Rev NC, 38144 Rev A Limitations and Conditions: The installer is required to consider the following items for regulatory compliance. Galley Installation Requirements use Report 38290, revision NC, dated 3-Mar-2008, or later FAA approved revision which includes the following: – Development of Sudden Decompression Load Report (SDLR) based on the final cabin interior arrangement. – Verification that items placed behind the tambour door is attached to or tied down to the lower surface of the compartment. – Final cabin interior arrangement requires FAA authorized interior compliance inspector. – Verification that an FAA approved upper support is present between the Galley and fuselage. – 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. FAA Approved: Robert J. Feazell STC ODA Administrator Dassault Falcon Jet ## Every issue (2) - November 27, 2012: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ea/f9/eaf91659a8f57bfa45c272483f5edb7445efe89d912aa0cb9c91b0f9297eddf8), [ST10652SC-D AML.pdf](https://openairdocs.org/files/sha256/05/5d/055d5577aa4fb66c7b390d6337d4079566158bc8e5e08706b890da7d762b57c8) - December 9, 2011: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/82/35/82353a79b6d5b79a55cbcd7b7ff3a68a5a7e39331e88cdf04c494398e24a9378), [ST10652SC-D AML.pdf](https://openairdocs.org/files/sha256/05/5d/055d5577aa4fb66c7b390d6337d4079566158bc8e5e08706b890da7d762b57c8) --- 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.