# STC SA01010WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Textron Aviation Inc, United States
- Description: Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System
- Applied: September 17, 2001
- Status date: December 12, 2016
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/d9/97/d99772a45cfe6a3a4ca5d7287e50c30dbef4b54027c3bdbfe48de3d184713fc0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/253777F1175E3F998625814800664ACC.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01010WI-D

## ADs that name it (0)

None.

## Approved models (2)

- Hawker Beechcraft Corporation A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Hawker Beechcraft Corporation B36TC ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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 3A15. 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 and 23-54.

SA01010WI-D Textron Aviation Inc.

One Cessna Boulevard Wichita, KS 67215 3 Civil Air Regulations and additional requirements * Beech A36 (S/N E-3430 and after); B36TC (S/N EA-691 and after) Installation of the Bendix/King KMH 880 Multi-Hazard Awareness System and the optional Bendix/King KMD 550 Multi-Function Display System. Required Data:

1. Master Drawing List No. 159-08272-6001, Revision --, dated September 17, 2001; and

2. Airplane Flight Manual Supplement No. 006-00895-0000, Revision --, dated October 12, 2001.

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

2 3A15 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 17, 2001 October 12, 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/d9/97/d99772a45cfe6a3a4ca5d7287e50c30dbef4b54027c3bdbfe48de3d184713fc0)
- March 26, 2007: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/f7/cd/f7cd007496ed12eaaa713b1bf9fde36ce824c190f46ef83c2b392d0399c27679)

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