STC SA00244WI-D

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SA00244WI-D This certificate issued to: Honeywell International Inc.

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

Original Product – Type Certificate Number: Make: Mooney Model:

2A3 M20C

Installation of the Bendix/King KLN 89 GPS(Global Positioning System) Navigation Receiver for VFRoperations;

installation of the KLN 89BGPSNavigation Receiver for IFRenroute and non-precision approach operations.

REQUIRED DATA: 1. Master Drawing List 159-08139-0001, Rev. 4, dated 5-15-95and 2. For the KLN 89B only, Airplane Flight Manual Supplement 006-00839-0000, Rev. 0, dated 6-23-95. Later FAA approved revisionsto the above listed data are incorporated without further revision to this Supplemental Type Certificate.

1. The KLN 89 GPSNAV islimited to use for visual rules operation only. A placard stating this limitation is required to be affixed to the instrument panel.

Date of Application: 3-30-95 Date Reissued: 11-4-98; 2-28-00; 4-14-20

Date of Issuance: 6-23-95 Date Amended:

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SA00244WI-D

Limitationsand Conditions: (continued)

2. This approval should not be extended to other specific airplanesof this model on which other previously approved modificationsare incorporated, unlessit isdetermined that the interrelationship between this change and any of those other previously approved modificationswill introduce no adverse effect upon the airworthinessof that airplane.

3. The KLN 89 and 89BGPShave been evaluated asa navigation input source for the KFC150 Series Automatic Flight Control System and found to be compatible; the interface of these systemsisapproved.

4. Additional equipment required for the specific type of operation must be installed and operational prior to use the KLN 89B under Instrument Flight Rules (IFR).

5. The Shadin Fuel Air Data Computer hasbeen evaluated asa fuel flow, temperature, and altitude input source for the KLN 89 and KLN 89BGPSand found to be compatible.

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.

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