STC ST10652SC-D

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