# STC SA00975WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King KMH 880/KTA 870 Multi-Hazard Awareness System/Traffic Advisory System and optional Bendix/King KMD 850 Multi-Function display system.
- Applied: January 24, 2001
- Status date: April 28, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21, Part 23
- Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16)
- Certificate PDF: https://openairdocs.org/files/sha256/0b/15/0b1544e9fe6055f29d5269655a814a2a0b51a9c144f4db6056a6a8774a7ace6a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4CAF6C428397BBF78625861600516014.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA00975WI-D

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Textron Aviation Inc. E55A ([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 2 Number: SA00975WI-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 3 of the Civil Air Regulations.

Make: Beech 3A16 Model: E55, E55A Description of Type Design Change:

Installation of the Bendix/King KMH 880/KTA 870 Multi-Hazard Awareness System/Traffic Advisory System and the optional Bendix/King KMD 850 Multi-Function Display System.

REQUIRED DATA: 1. Master Drawing List 159-08265-0001, Revision A, dated 5-17-2001; 2. If the KMH 880 is installed, Airplane Flight Manual Supplement 006-00884-0000, Revision -, dated 6-7-2001; or 3. If the KTA 870 is installed, Airplane Flight Manual Supplement 006-00884-0001, Revision -, dated 6-7-2001.

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

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

2. 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.

Certification Basis:

To comply with the airworthiness requirements 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.

Date of Application: 1-24-2001 Date Reissued: 4-28-2020 Date of Issuance: 6-7-2001 Date Amended:

By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

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

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

## Every issue (2)

- April 28, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/0b/15/0b1544e9fe6055f29d5269655a814a2a0b51a9c144f4db6056a6a8774a7ace6a)
- June 7, 2001: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/23/d5/23d575b2850640953c691c8f5a95208bcd50e62b45cf9fa26829ad4cce42c1e9)

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