# STC SA02331LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Install and maintain Switches and Wiring for Electro-Optical/Infra-Red lift and Turret
- Applied: January 22, 2010
- Status date: November 16, 2016
- Product: Aircraft, Small/Large Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE)
- Certificate PDF: https://openairdocs.org/files/sha256/cb/1c/cb1c6ac38b3102673d76c374a5ebdd0683f091db68635f0698ddd8c86fd2b21f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0519351D9A09F284862581480049D749.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02331LA

## ADs that name it (0)

None.

## Approved models (2)

- Beechcraft Corporation B300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 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.

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

Part of the

Signature

Title *Certification basis is set forth in Type Certificate Data Sheet A24CE.

SA02331LA Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 23* Federal Aviation Regulations.

Hawker Beechcraft B300, B300C 2 A24CE Install and maintain Switches and Wiring for Electro-Optical/Infra-Red Lift and Turret in accordance with Master Data List 300E404584, Revision 3, dated November 9, 2010 or later FAA approved revision and FAA Approved Flight Manual Supplement, Document No. 130-590031-403, dated December 3, 2010, or later FAA approved revisions.

This STC is a part of an existing belly mounted radar installation, and may only be installed on aircraft which have previously installed STC Number SA02253LA. The installation should not be incorporated into any other aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. The approval of this modification applies to the above noted airplane model series only. 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.

September 23, 2013; November 16, 2016 January 22, 2010 December 6, 2010 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)

## Every issue (3)

- November 16, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/cb/1c/cb1c6ac38b3102673d76c374a5ebdd0683f091db68635f0698ddd8c86fd2b21f)
- September 23, 2013: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6e/14/6e14c62ae3b90d15ce55b2815aadec934f9afc502db85290e7b92ecc15e3224a)
- December 6, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/dc/7f/dc7fd74b8f1f2d8dd9efdbbbea31f00e7176feb3514bc47fe1bc0ec3b54886c5)

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