STC ST10922SC

Part 25 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of Cabin Interior Furnishings and Systems in accordance with STC Master Documents List (MDL) No. 240-2001 Revision 9 dated July 19, 2009, or later FAA approved revision.

Use of the FAA approved Airplane Flight Manual Supplement, as listed in the table below, is required. Completions Manual for each specific configuration, as listed in the table below, must be made available to the operator at the time of installation.

Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. If the holder agrees to permit another person to use this certificate to alter a product, the holder must provide the other person written evidence of that permission. Airworthiness Limitations inspections per 14 CFR 25, Appendix H are contained in Chapter 4 of the Completions Manual. Refer to the table below for the specific Airworthiness Limitations for each configuration.

Hawker Beechcraft Corporation 2400 Grundfest Little Rock, AR 72206 T00013WI Make: Hawker Beechcraft Corporation Model: 4000 Date of application: March 24, 2008

Date of issuance: May 29, 2009

Date amended: August 05, 2009

( Signature) Gary A. Sharon Acting Manager, Special Certification Office Southwest Region

( Title)

FAA Form 8110-2-1(10-69) Page 2 of 4

Number ST10922SC Date of Issuance: May 29, 2009 Date Amended: August 05, 2009

FAA Form 8110-2-1(10-69) Page 3 of 4

Number ST10922SC Date of Issuance: May 29, 2009 Date Amended: August 05, 2009

Configuration Drawing Aircraft Fli ght Manual Supplement Completions Manual Airworthiness Limitations Configuration 1 240-044000 Rev 3 dated July 19, 2009 or later FAA Approved Revision 240-590001-0001 Rev 1 Dated April 14, 2009 or later FAA Approved Revision

401-590001-0047 dated May 4, 2009 or later accepted Revision 401-590001-0047 Chapter 4 approved August 5, 2009 or later FAA approved revision Configuration 2 240-044100 Rev 1 dated July 19, 2009 or later FAA Approved Revision 240-590001-0003 Rev 1 Dated June 26, 2009 or later FAA Approved Revision

240-590011-0001 dated July 1, 2009 or later accepted Revision 240-590011-0003 approved August 5, 2009 or later FAA approved Revision

Certification Basis:

14 CFR 25, Amendment In Square Brackets

25.1 [Basic] 25.21(a) [25-72] 25.23 [Basic]

25.25 [25-63] 25.27 [Basic] 25.29 [25-72]

25.301 [25-23] 25.303 [25-23] 25.305(a)(b) [25-86]

25.307(a) [25-72] 25.321(a) [25-86] 25.561 [25-91]

25.562 [25-64] 25.581 [25-23] 25.601 [Basic]

25.603 [25-46] 25.605(a) [25-46] 25.609 [Basic]

25.611 [25-23] 25.613 [25-72] 25.619 [25-23]

25.621 [Basic] 25.623 [Basic] 25.625 [25-72]

25.771(a) [25-4] 25.785 [25-88] 25.787 [25-51]

25.789 [25-46] 25.791 [25.72] 25.793 [25-51]

25.803(a) [25-72] 25.807(a)(b)(e)(g)(i) [25-94]

25.809 (a)(b)(c)(e)(f)(i) [25-72] 25.811 [25-88] 25.812 [25-88]

25.813 [25-88] 25.815 [25-38] 25.817 [25-15]

25.831 [25-89] 25.832 ]25-94] 25.851(a) [25-74]

25.853(a)(c)(e)(f)(g)(h) [25-83] 25.855(a)(b)(d)(e)(f)(g)(h)(i) [25-93]

25.856(a) [25-111] 25.857(b) [25-93]

25.858 [25-93] 25.867(a) [25-23] 25.869(a)(c) [25-72]

25.981(a)(3)(b) [25-102] 25.1301 [Basic] 25.1307(c) [25-72]

25.1309(a)(b)(c)(d)(g) [25-41] 25.1316 [25-80] 25.1321(a) [25-41]

FAA Form 8110-2-1(10-69) Page 4 of 4

Number ST10922SC Date of Issuance: May 29, 2009 Date Amended: August 05, 2009

Certification Basis (Continued):

25.1322(c)(d) [25-38] 25.1351(a) [25-72] 25.1353(a)(b) [25-42]

25.1355(a) [25-38] 25.1357(a)(b)(c)(d)(e) [Basic] 25.1381 [25-72]

25.1411(a)(b)(c)(d)(f)(g) [25-79] 25.1415 [25-82] 25.1423 [25-79]

25.1431(a)(c) [Basic] 25.1438(a)(c) [25-41] 25.1439 [25-41]

25.1441 [Basic] 25.1443 [Basic] 25.1445 [Basic]

25.1447 [25-87] 25.1449 [Basic] 25.1453 [Basic]

25.1455 [25-23] 25.1501 [25-42] 25.1519 [Basic]

25.1529 [25-54] 25.1541 [Basic] 25.1557(a)(c)(d) [25-72]

25.1561(a)(b)(c)(e) [25-46] 25.1581(a )(b)(d) [25-72] 25.1583(c) [25-105]

25.1585(a)(b) [25-105] 25-162-SC (HIRF) ELOS 25.811(d)(1) TC1258WI-T-A-5 ELOS 25.812(b)(1)(i) TC1258WI-T-A-5

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