STC SA00819WI-D

FAA Form 8110-2 (5/14) Page 1 of 4 Number: SA00819WI-D This certificate issued to: Honeywell International Inc.

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

Make: Cessna 3A13 Model: 182S Description of Type Design Change:

Installation of the Bendix/King KMD 150 MFD (Multi-Function Display) and optional L-3 WX 500 Stormscope.

REQUIRED DATA:

A) For the KMD 150 MFD: 1. Master Drawing List 159-08242-0001, Rev. A, dated 9-20-99; and

2. Airplane Flight Manual Supplement 006-00869-0000, Rev.-, dated 10-1-99.

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: July 20, 1999 Date Reissued: April 14, 2020 Date of Issuance: October 1, 1999 Date Amended: December 23, 1999; October 15, 2004 By Direction of the Administrator Signature Richard B. Sleigh Title ODA Administrator, ODA-602216-NM

FAA Form 8110-2 (5/14) Page 2 of 4

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: SA00819WI-D

FAA Form 8110-2 (5/14) Page 3 of 4 Description of Type Design Change: (continued) B) For the KMD 150 MFD with built-in VFR GPS: 1. Master Drawing List 159-08242-0001, Rev. B, dated 12-14-99; and 2.

Airplane Flight Manual Supplement 006-00869-0000, Rev. A, dated 12-23-99 or Airplane Flight Manual Supplement 006-00869-0001, Rev. -, dated 12-23-99.

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

Limitations and Conditions: (continued)

2. The KLN 89, 89B and 94 GPS have been evaluated as a navigation input source for the KMD 150 Multi-Function Display and found to be compatible; the interface of these systems is approved.

3. The KMD 150 MFD has been evaluated for use under IFR when interfaced to an IFR qualified KLN 89B/94.

4. The KMD 150 MFD internal GPS has been evaluated for VFR navigation only.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA00819WI-D

FAA Form 8110-2 (5/14) Page 4 of 4 Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this change is as follows:

a. The certification basis for parts not changed or not affected by this change is shown on TCDS 3A13.

b. The certification basis for parts changed or affected by this change since the date of application is determined to be:

Regulations at the latest amendment

Regulations at an intermediate amendment none Regulations at the amendment level shown on TCDS none ---------------------------------------------------------------------------END-------------------------------------------------------------------------- Section Amdt. Section Amdt.

23.301 All 23-48 23.1301 All 23-20

23.303 23-0 23.1309 a (1) (2), b(1) 23-49

23.305 23-45 23.1321 a, c, e 23-49

23.307 23-0 23.1322 All 23-43

23.337 23-48 23.1331 a 23-43

23.561 e 23-48 23.1351 a, b1 23-49

23.601 23-0 23.1357 a, c 23-43

23.603 All 23-23 23.1365 a, b, e 23-49

23.605 a 23-23 23.1367 23-0

23.607 23-48 23.1431 a, b 23-49

23.609 All 23-0 23.1501 23-21

23.613 All 23-45 23.1529 23-26

23.627 23-0 23.1541 a2, b 23-21

23.777 a, b 23-51