# STC SA00900WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of Bendix/King KMD 550 Multi-Function Display.
- Applied: August 22, 2000
- Status date: April 20, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A51EU](https://openairdocs.org/tcds/A51EU)
- Certificate PDF: https://openairdocs.org/files/sha256/5d/c9/5dc94af343bbba950af215cff7832cd70b6f7dd9d327cbe7abfd45e609cd3cf6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1179D079B78EDBAD8625861500806427.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00900WI-D

## ADs that name it (0)

None.

## Approved models (5)

- SOCATA - Groupe Aerospatiale TB 10 ([TCDS A51EU](https://openairdocs.org/tcds/A51EU))
- SOCATA - Groupe Aerospatiale TB 20 ([TCDS A51EU](https://openairdocs.org/tcds/A51EU))
- SOCATA - Groupe Aerospatiale TB 200 ([TCDS A51EU](https://openairdocs.org/tcds/A51EU))
- SOCATA - Groupe Aerospatiale TB 21 ([TCDS A51EU](https://openairdocs.org/tcds/A51EU))
- SOCATA - Groupe Aerospatiale TB9 ([TCDS A51EU](https://openairdocs.org/tcds/A51EU))

## 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: SA00900WI-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 23 of the Federal Aviation Regulations.

Make: SOCATA A51EU Model: TB 9, TB 10, TB 20, TB 21, TB 200 Description of Type Design Change:

Installation of the Bendix/King KMD 550 Multi-Function Display.

REQUIRED DATA: Master Drawing List 159-08260-0001, Rev. A, dated 12/11/2000.

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

This approval should not be extended to other specific aircraft of this model on which other previously approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that airplane.

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.

Date of Application: August 22, 2000 Date Reissued: April 24, 2020 Date of Issuance: December 18, 2000 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 20, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5d/c9/5dc94af343bbba950af215cff7832cd70b6f7dd9d327cbe7abfd45e609cd3cf6)
- December 18, 2000: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/b8/a5/b8a5b8c02008f799ab34f96dbf4846ed3807ad05dd73229aa5deaf1a6e1082d1)

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