STC ST10922SC-D

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title ST10922SC-D Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 25 Federal Aviation Regulations.

Hawker Beechcraft Corporation 4000 See Sheet 4 for certification basis 5 T00013WI Installation of Cabin Interior Furnishings and Systems in accordance with STC Master Documents List (MDL) No.

240-2001 Revision 69 dated August 30, 2012, 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.

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.

For Configurations 3 and 9: This system is intended to provide internet connections and email services using portable electronic devices (PEDs). Any other intended function of this equipment will require a re-examination of the certification basis.

(see continuation sheet 3 of 5) September 1, 2017 8/5/09; 12/5/09; 12/11/09; 5/19/10; 6/15/10;

9/3/10; 8/30/11; 9/1/11; 5/16/12; 10/3/12 March 24, 2008 May 29, 2009 Mark Fuller STC ODA administrator ODA-100129-CE

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 5 ST10922SC-D Date of Issuance: May 29, 2009 Date Amended: October 3, 2012 Date Reissued: September 1, 2017

Limitations and Conditions (cont'd):

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.

Configuration Drawing Airplane Flight Manual Completions Manual Airworthiness Limitations Supplement

Configuration 1 240-590001-0001 Rev 2 401-590001-0047 dated 401-590001-0047 Chapter 4 240-044000 Rev 3 Dated June 19, 2009 May 4, 2009 or later approved August 5, 2009 or dated July 19, 2009 or later accepted Revision. later FAA approved revision FAA Approved Revision

Configuration 2 240-590001-0003 Rev 1 240-590011-0001-RC-21 240-590011-0003C approved 240-044100 Rev 17 Dated June 26, 2009 dated July, 2009 or later August, 2010 or later FAA dated May 20, 2011 or later accepted Revision. approved Revision FAA Approved Revision

Configuration 3 240-590001-0007 Rev 3 23-10-65-HBC10003P dated 23-10-65-HBC10003P dated 240-044300 Rev 3 Dated September 18, 2012 August, 2010 or later accepted August, 2010 or later accepted dated May 11, 2012 or later or later FAA Approved Revision and 44-30-20- Revision and 44-30-20-HBC10009 FAA Approved Revision Revision HBC10009 dated January, 2012 dated January, 2012 or later or later accepted Revision accepted Revision.

Configuration 4 240-590001-0005 Rev 2 240-590011-0001-RC-27 240-590011-0003C approved 240-044200 Rev 5 dated August 31, 2011 dated October, 2009 or August, 2010 or later FAA dated April 5, 2010 or later later accepted Revision approved Revision FAA Approved Revision

Configuration 6 240-590001-0003 Rev 2 2240-590011-0001-4600 240-590011-0003C approved 240-044600 Rev 18 dated Dated August 31, 2011 or dated June, 2010 or later August, 2010 or later FAA August 27, 2012 or later later FAA Approved Revision accepted Revision approved Revision FAA Approved Revision

Configuration 8 240-590001-0005 Rev 2 240-590011-0001-RC-43 240-590011-0003C approved 240-044800 Rev 9 Dated August 31, 2011 dated February, 2010 or August, 2010 or later FAA dated March 9, 2012 or later or later FAA Approved later accepted Revision. approved Revision FAA Approved Revision Revision

Configuration 9 240-590001-0007 Rev 3 23-10-65-HBC10003P dated 23-10-65-HBC10003P dated, 240-044900 Rev 3 dated Dated September 18, 2012 or August, 2010 or later accepted August 2010 or later accepted May 11, 2012 or later later FAA Approved Revision Revision and 44-30-20-HBC10009 Revision and 44-30-20-HBC10009 FAA Approved Revision dated January, 2012 or later dated January, 2012 or later accepted Revision accepted Revision

FAA Form 8110-2 (5/14) Page 4 of

5 Date of Issuance: May 29, 2009 Date Amended: October 3, 2012 Date Reissued: September 1, 2017

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]

25.113 [25-92] 25.119 [25-94] 25.121 [25-84]

25.123(a)(b) [Basic] 25.251 [25-77] 25.301 [25-23]

25.303 [25-23] 25.305(a)(b)(c)(e) [25-86] 25.307(a) [25-72]

25.321 (a) [25-86] 25.365(e)(2)(3) [25-87] 25.561 [25-91]

25.562 [25-64] 25.571(a)(b)(c)(e)(1) [25-96] 25.581 [25-23]

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

25.607 [25-23] 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] 25.629 [25-77]

25.771(a)(e) [25-4] 25.773(a) [25-72] 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) [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] 25.841(a)(2) [25-87] 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]

25.863(a)(b)(3) [25-46] 25.867(a) [25-23] 25.869(a)(c) [25.72]

25.901(c) [25-46] 25.903 (c) [25-100] 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]

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] ST10922SC-D

FAA Form 8110-2 (5/14) Page 5 of

ST10922SC-D 5 Date of Issuance: May 29, 2009 Date Amended: October 3, 2012 Date Reissued: September 1, 2017

Certification Basis (cont'd):

14 CFR 25, Amendment In Square Brackets

25.1411(a)(b)(c)(d)(f)(g) [25-79] 25.1415 [25-82] 25.1419(a) [25-72]

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] 25.1587(b) [25-105] 25-162-SC (HIRF) 25-279-SC (Side-Facing Single-Occupant Seats) ELOS 25.119(b) TC1258WI-T-F-1 ELOS 25.121(c)(d) TC1258WI-T-F-1 ELOS 25.813(e) TC1258WI-T-A-8 ELOS 25.811(d)(1) TC1258WI-T-A-5 ELOS 25.807(i) TC1258WI-T-A-6 ELOS 25.812 (b)(1)(i) TC1258WI-T-A-5 ELOS 25.811 (e)(4) TC1258WI-T-A-9 Exemption No. 7512B

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