# STC SA01009WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of Bendix/King KMH 880 multi-hazard awareness system and Bendix/King KMD 850 multi-function display system. Approved for models 58 and 58A, serial numbers TH-2000 and after.
- Status date: December 12, 2016
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/0f/81/0f819a02ebfd06faec8a88aa55d7aa2938634bea425aa7105d1d9af360376011
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C9D8A3CFEAAEA11A862581480066496A.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01009WI-D

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Hawker Beechcraft Corporation 58A ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

## 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 * as specified in TCDS 3A16. To comply with the airworthiness requirements in effect on the date of application, the additional certification basis applicable to this change is Title 14 CFR Part 23, Amendments 23-1 through 23-54.

SA01009WI-D Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 Civil Air Regulations and additional requirements * Beech 58, 58A (S/N TH-2000 and after) Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System and the Bendix/King KMD 850 Multi-Function Display System. Required Data:

1. Master Drawing List No. 159-08273-6001, Revision --, dated September 4, 2001; and

2. Airplane Flight Manual Supplement No. 006-00896-0000, Revision --, dated October 1, 2001.

Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate.

2 3A16 Compatibility of this design with previously approved modifications must be determined by the installer. 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.

November 29, 2001; March 26, 2007;

December 12, 2016 September 12, 2001 October 1, 2001 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 (2)

- December 12, 2016: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0f/81/0f819a02ebfd06faec8a88aa55d7aa2938634bea425aa7105d1d9af360376011)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/25/33/25338d82d6e5a95af7cdd5a7462d6d176f8a6f34b73252c838f6769a1a06d447)

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