# STC SA00841WI-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Honeywell International Inc, United States
- Description: Installation of the Bendix/King KMD 150 MFD Multi-Function Display
- Applied: December 9, 1999
- Status date: April 17, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/c7/50/c7509c20148fa0eb52a33b4dadde489fefd5b9f683ef88e8b94f849de61b37ec
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D00395DD4BCC379E8625861400738039.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00841WI-D

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. A36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Textron Aviation Inc. 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 3 Number: SA00841WI-D This certificate issued to: Honeywell International Inc.

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

Make: Beech 3A15 Model: A36, B36TC Description of Type Design Change:

Installation of the Bendix/King KMD 150 MFD Multi-Function Display.

REQUIRED DATA: 1. Master Drawing List 159-08251-0001, Rev. -, dated 12-8-99; and 2. Airplane Flight Manual Supplement 006-00876-0000, Rev.-, dated 1-7-00.

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

1. This approval should not be extended to other specific airplanes 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.

(See continuation sheet) 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: December 9, 1999 Date Reissued: April 17, 2020 Date of Issuance: January 7, 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 3

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

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00841WI-D

FAA Form 8110-2 (5/14) Page 3 of 3 Limitations and Conditions: (continued)

2. The KLN 90B GPS has been evaluated as a navigation input source for the KMD 150 Multi-Function Display and found to be compatible; the interface of this system is approved.

3. The KLN 89 & KLN 89B GPS have been evaluated as a navigation input source for the KMD 150 Multi-Function Display and found to be compatible; the interface of this system is approved.

4. The KMD 150 Multi-Function Display has been evaluated for use under IFR when interfaced to an IFR qualified KLN 90B.

5. The KMD 150 Multi-Function Display has been evaluated for use under IFR when interfaced to an IFR qualified KLN 89B.

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## Every issue (2)

- April 17, 2020: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c7/50/c7509c20148fa0eb52a33b4dadde489fefd5b9f683ef88e8b94f849de61b37ec)
- January 7, 2000: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d4/63/d4635bd02068567608b5e5dd196b5733b53effdf2dd62a342ff2a717ae3002bd)

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