STC SA01924WI

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the

Signature

Title Avcon Industries, Inc.

714 N. Oliver, Hangar M Newton, KS 67114 3 SA01924WI Federal Aviation Regulations. 23 Installation of an External Pod and Retractable EO/IR Sensor Lift Mechanism. Data required:

1. Master Data List, Document No. 04601001, Rev. IR, dated June 3, 2019 or later FAA Approved revision; and (Continued on Page 3)

1. Installation of the Sensor Lift Mechanism requires prior or concurrent installation of STC SA01902WI.

2. Compatibility of this design with previously approved modifications must be determined by the installer.

3. Model A200CT: S/N eligibility is limited to BP-24 and BP-29.

Textron Aviation (Beechcraft) 200, 200C, A200, A200CT, B200, B200C August 26, 2022, July 24, 2023 August 7, 2018 June 4, 2019 A24CE for Paul Nguyen Manager, Central Certification Branch Compliance & Airworthiness Division Aircraft Certification Service

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

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

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

3 SA01924WI

This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the proper ty of the STC holder.

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

3 Date amended: July 24, 2023 Description of Type Design Change (continued from page 1):

2. Airplane Flight Manual Supplement, Document No. 04607101, or No. 04607102, or No. 04607103, all at Rev. 0, all dated May 28, 2019, or later FAA Approved revision, or

3. Airplane Flight Manual Supplement, Document No. 04607104 or No. 04607105, both at Rev. IR, and dated August 26, 2022, or later FAA Approved revision, or

4. Airplane Flight Manual Supplement, Document No. 04607106, Rev. IR, and dated July 6, 2023, or later FAA Approved revision.

Certification Basis (continued from Page 1):

In accordance with 14 CFR 21.101 and 21.115, and the procedures specified in FAA Order 8110-48 and FAA AC 21.101, the certification basis for this modification is as follows:

1. The type certification basis for areas not changed or affected by this modification remain as specified in the applicable TCDS.

2. The certification basis for areas changed or affected by this modification since the date of allocation, August 7, 2018, was determined to be: Models 200, 200C, A200, A200CT, B200, B200C.

a. In accordance with 14 CFR Part 23, effective February 1, 1965, as amended by Amendment 21-1 through 23-9, and Part 36 as amended through 36-20, except for Models B200 and B200C:

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23.301(a)(b)(c)

23.305(a)(b)

23.337(a)(b)

23.341

23.473

23.561(a)(b)(2)(e)

23.603

23.605

23.607

23.611

23.613 Amdt 23-48 23-45 23-48 23-48 23-48 23-48 23-23 23-23 23-48 23-48 23-45 Section

36.1(a)(2)(b)

36.2(b)

36.1581(a)(2)(c) G36.105 G36.107 G36.111 G36.201 G36.301(b) Amdt 36-31 36-24 36-25 36-24 36-22 36-27 36-22 36-28