# STC SA01953WI

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Avcon Industries Inc, United States
- Description: Installation of Retractable EO/IRSensor (large) Mechanism and External Pod
- Applied: May 13, 2019
- Status date: September 29, 2020
- Product: Aircraft
- Certification basis: Part 23
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/63/27/6327bcdef69fafb1c48622f3582ab8732b3c08dc58671d544d52661b1a3109c6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/155637960FB50B6C86258646006029B7.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01953WI

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. B300C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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 Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title Avcon Industries, Inc.

714 N. Oliver, Hangar M Newton, KS 67114 2 SA01953WI Federal Aviation Regulations. 23 Textron Aviation (Beechcraft) B300, B300C Installation of Retractable EO/IR Sensor (large) Mechanism and External Pod. Data required:

1. Master Drawing List, Document No. 05201000, Rev. IR, dated August 8, 2020, or later FAA Approved revision; and

2. Airplane Flight Manual Supplement, Document No. 05207100, Rev. 0, dated August 25, 2020 or later FAA Approved revision.

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

2. Operation of the aircraft without the complete fairing installation invalidates the approved STC configuration. The inclusion or attachment of any external stores or provisions invalidates the approval status of this STC, as it does not comply with the approved configuration. In order to operate in any alternate configuration, the changes must be re-evaluated per 14 CFR part 21, 21.93(b), and possibly require acoustic evaluation to assure compliance with 14 CFR part 36.

May 13, 2019 September 29, 2020 A24CE Grant Youngdahl Program Manager Wichita ACO Branch

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):

2 SA01953WI

## Every issue (1)

- September 29, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/63/27/6327bcdef69fafb1c48622f3582ab8732b3c08dc58671d544d52661b1a3109c6)

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