STC SA00827WI-D

FAA Form 8110-2 (5/14) Page 1 of 3 Number: SA00827WI-D This certificate issued to: Honeywell International Inc.

21111 N 19th Ave Phoenix, Arizona 85027 Part 23 of the Federal Air 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 150 MFD Multi-Function Display.

REQUIRED DATA: 1. Master Drawing List 159-08248-0001, Rev. A, dated 1-6-00; and 2. Airplane Flight Manual Supplement 006-00872-0000, Rev.-, dated 1-20-00.

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: October 11, 1999 Date Reissued: April 16, 2020 Date of Issuance: January 20, 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: SA00827WI-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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