STC SA02468LA

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

Part of the

Signature

Title Aviation Fabricators, Inc.

804 North Fourth Street Clinton, MO 64735 3 SA02468LA Federal Aviation Regulations. (*See page 3) 23* Installation of Aviation Fabricators Aft Toilet Cabinet Seat (including oxygen, air and light systems) in accordance with the FAA Approved Aviation Fabricators Master Data List, No. AF-482MDL, Rev B, dated June 11, 2013, or later FAA approved revision.

This approval should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previous approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted aircraft models only. A copy of this STC must be included in the permanent records of the modified aircraft. (See Continuation Sheet page 3) Hawker Beechcraft 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, B200GT, B200CGT, B300, B300C January 7, 2016 July 23, 2009 July 3, 2013 A24CE David Fairback Program Manager Wichita Aircraft Certification Office

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA02468LA

FAA Form 8110-2 (5/14) Page 3 of

3 Issued date: July 3, 2013 Amended date: January 7, 2016

Limitations and Conditions (continued from page 1):

Aviation Fabricators Instructions for Continued Airworthiness (ICA) Document No. AF-483, Rev A, dated November 30, 2009 or Document No. AF-570, Rev IR, dated October 30, 2013, or later FAA accepted revision, must be made available to the operator at the time of installation.

Certification Basis (continued from page 1):

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis is stated below:

1. For Models B300 and B300C: the type certification basis is shown on TCDS A24CE.

2. For Models 200, 200C, 200CT, 200T, B200, B200C, B200CT, B200T, B200GT, B200CGT:

a. The type certification basis for parts not changed or not affected by the change is shown on TCDS A24CE.

b. The type certification basis for parts changed or affected by the changes since the date of application of July 23, 2009, is 14 CFR Part 23 as amended by Amendment 23-62. 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 modification was determined to be:

Regulations at the latest amendment 23-0 through 23-62:

23.1351, 23.1438, 23.1529, 23.1541, Appendix G.

Regulations at an intermediate amendment:

23.853 Amendment 23-34

23.1301 Amendment 23-14

23.1309 Amendment 23-34

23.1357 Amendment 23-20

23.1365 Amendment 23-14

Regulations at the amendment level in TCDS A24CE (Amendment 23-0 through 23-9):

23.301, 23.303, 23.305, 23.307, 23.321, 23.333, 23.337, 23.341, 23.561, 23.601, 23.603, 23.605, 23.607, 23.609, 23.611,

23.613, 23.615, 23.619, 23.623, 23.625, 23.785, 23.831, 23.1441, 23.1443, 23.1447, 25.831(d) Amendment 25-41.

---------- END ------------ SA02468LA