STC ST10583SC-D

United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number ST10583SC-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.

40366, revision A, or later FAA approved airplane models, applicable installation data requirements and specific limitations. Make: Model:

Galley Pocket Door Installation in accordance with Data List Report No. F00-01005 Revision AR dated April 3, 2011, 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.

Date of application: March 12, 2007

Date of issuance: July 16, 2007

Date reissued: 23-Oct-2008, 10-Jun-2010

Date amended:30-Jun-2009 Rev 1, 13-Apr-2011 Rev 2

(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 ST10583SC-D Revision 2 Issue Date: April 13, 2011

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

The following is required for the F00-01005-501:

FAA Approved AFM Supplement, Report 37887-1 dated 7/16/07 or later FAA approved revision is required.

Maintenance Manual Supplemental, Report 37798, revision B, dated 6/28/07 or later FAA approved revision is required prior to April 2011.

Instructions for Continue Airworthiness, Report ICA-F00-01005-501, revision Original, dated 25-Jan-2011 or later FAA approved revision is required for installations after April 2011.

The following is required for the F00-01005-503:

FAA Approved AFM Supplement, Report 37887-2 dated 6/30/09 or later FAA approved revision is required.

Instructions for Continue Airworthiness, Report ICA-F00-01005-503, revision NC, dated 2/25/09 or later FAA approved revision is required Limitations and Conditions (Continued):

(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 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

25.21 (a) 25-72

25.301 (a),(b) 25-23

25.303 - 25-23

25.305 (a),(b) 25-86

25.307 (a) 25-72

25.321 (a),(b),(c),

(d) 25-86

25.331 (a),(b),(c),

(d) 25-91

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

25.337 (a) 25-23

25.341 (a) 25-86

25.365 (a),(b),(c),

(g) 25-87 SECT. PARA. AMDT.

25.561 (a),(b),

(c),(d) 25-64

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) 25-72

25.625 (a),(c) 25-72

25.789 (a) 25-46

25.803 (a) 25-46

25.813 (a),(f) 25-46

25.853 (a) 25-83

25.855 (d) 25-93 SECT. PARA. AMDT.

25.1301 (a),(b),

25.1309 (a),(b),(d) 25-41

25.1519 - O

25.1529 - 25-54

25.1541 (a),(b) O

25.1557 (d) 25-72

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