STC SA03669AT

Title: (for) Robert Capezzuto Acting Manager, East Certification Branch Compliance and Airworthiness Division Aircraft Certification Service SA03669AT Woven Electronics, LLC 16000 Pines Blvd #824431 Pembroke Pines, FL 33082-9599 Part 23 Federal Aviation Regulations A24CE Hawker Beechcraft B200, B200C, B300, B300C, 200, 200C, 200CT, 200T, B200CT, B200T, 300, 300LW Installation of an EMTEQ Aerospace Seat Warmer System (SWS) into a Hawker Beechcraft B200, B200C, B300, B300C, 200, 200C, 200CT, 200T, B200CT, B200T, 300 and 300LW Series Aircraft and associated hardware in accordance with Master Drawing List 2-43183-001 Revision A dated October 14, 2008 or later FAA approved drawing revisions.

(Continued on Sheet 3) March 22, 2007 March 2, 2015; April 10, 2023 January 27, 2009 3

SA03669AT 3

SA03669AT Limitations and Conditions (Continued):

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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.

Instructions for Continued Airworthiness (ICA), EMTEQ Engineering Document No. 2-43183-805, Rev.

IR, dated November 27, 2007, or later FAA accepted revision must be made available to the operator at the time of installation.

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 the Hawker Beechcraft King Air B200, B200C, B300, B300C, 200, 200C, 200CT, 200T, B200CT, B200T, 300 and 300LW Series Aircraft is as follows:

a. The type certification basis for the Hawker Beechcraft King Air B200, B200C, B300, B300C, 200, 200C, 200CT, 200T, B200CT, B200T, 300 and 300LW Series airplanes is shown on TCDS A24CE for parts not changed or not affected by the change.

b. The certification basis for parts changed or affected by the change since the reference date of application, March 22, 2007 is based upon part 23 as amended by Amendment 23-55. 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 23-1 through 23-55 Appendix F

Regulations at an intermediate amendment Appendix H

Regulations at the amendment level in TCDS A24CE Appendix G --------------------- END --------------------- 3 3