# STC SA01205WI-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Honeywell International Inc, United States
- Description: Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.
- Applied: May 30, 2003
- Status date: November 20, 2007
- Product: Aircraft, Single-Engine
- Certification basis: Part 23
- Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS A12SO](https://openairdocs.org/tcds/A12SO), [TCDS 3A10](https://openairdocs.org/tcds/3A10), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A13](https://openairdocs.org/tcds/3A13), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A21](https://openairdocs.org/tcds/3A21), [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 3A25](https://openairdocs.org/tcds/3A25), [TCDS 5A6](https://openairdocs.org/tcds/5A6), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A13EU](https://openairdocs.org/tcds/A13EU), [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS A25CE](https://openairdocs.org/tcds/A25CE), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A2CE](https://openairdocs.org/tcds/A2CE), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE) and 18 more
- Certificate PDF: https://openairdocs.org/files/sha256/72/c5/72c57ec80721c35cecd6382a2296ac80e5c4eee20713edb01bfca6956df00a5a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1DABD72C5E6C414486257608004BEC62.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01205WI-D

## ADs that name it (0)

None.

## Approved models (320, first 50)

- Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Aerostar Aircraft Corporation PA-60-700P (Aerostar 700P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE))
- Cessna Aircraft Company 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150B ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150F ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150G ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150H ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150J ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150K ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150L ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 150M ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 152 ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172F ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172H ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172I ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172Q ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172R ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172RG ([TCDS 3A17](https://openairdocs.org/tcds/3A17))
- Cessna Aircraft Company 172S ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 177 ([TCDS A13CE](https://openairdocs.org/tcds/A13CE))
- Cessna Aircraft Company 177A ([TCDS A13CE](https://openairdocs.org/tcds/A13CE))
- Cessna Aircraft Company 177RG ([TCDS A20CE](https://openairdocs.org/tcds/A20CE))
- Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6))
- Cessna Aircraft Company 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182R ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

All 320: https://openairdocs.org/stc/SA01205WI-D/models.md

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01205WI-D This certificate issued to:

Honeywell International Inc.

23500 W. 105h Street Olathe, KS 66061 Certifies that the change in the type design for the following product with the limilations and conditions therefor as specified horean meets the airworthiness requiroments of Part 23* of the Federal Aviation Regulations Original Product - Type Certificate Number: * See attached FAA Approved Model List Make: * (AML) No. 159-08293-0002 for the list of Model: * approved airplane models and applicable Description of Type Design Change: airworthiness regulations.

Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.

REQUIRED DATA:

1. AML No. 159-08293-0002, Revision -, dated 11-14-2003

2. When the Traffic Information Service (TIS) is installed; Airplane Flight Manual Supplement, 006-10315-0000, Revision -, Dated 11-14-2003.

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

1. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft.

2. 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.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA01205WI-D *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 the appropriate TCDS of the Models listed on AML Number, 159-08293-0002.

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 Section Amdt. Section Amdt.

23.251 23-45 23.1309 (a)(1)(2)(3), 23-49

23.301 (a), (b), (c), (d) 23-48 (b)(1)(4)(i)(ii), (c)(1), (d), (e)

23.303 23.1321 (a) 23-49

23.305 (a), (b) 23-45 23.1322 (a), (b), (c), (d), (e) 23-43

23.307 (a), (b) 23-0 23.1331 (a) 23-43

23.337 (a)(1), (b)(1) 23-48 23.1351 (a)(1)(2)(i) 23-49

23.561 (e) 23-48 23.1357 (a), (b), (c), (d) 23-43

23.601 23.1359 (c) 23-49

23.603 (a), (b) 23-23 23.1365 (a), (b), (d), (e) 23-49

23.605 (a) 23-23 23.1367 (a), (b), (c), (d)

23.607 (a), (b), (c) 23-48 23.1381 (a), (b), (c)

23.609 (a), (b) 23.1431 (a), (b) 23-49

23.611 23-48 23.1501 (a), (b) 23-21

23.613 (a), (b)(1)(2),(c),(d), (e) 23-45 23.1525 23-45

23.1301 (a), (b), (c), (d) 23-20 23.1529 23-26

23.1541 (a)(2), (b)(1)(2) 23-21 Regulations at an intermediate amendment none Regulations at the amendment level shown on TCDS none

FAA FORN B110-2-1 (10-69) PAGE 3 of 3 PAGES icate may be transferred in accordance with FAR 21.47.

AML AMDT Date 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 Certification Basis for design change (See Note 1) 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity A17WE 3A15 3A16 A23CE A12CE 3A19 Aircraft Model PA-60-600, PA-60-601, PA-60-601P, PA-60-602P 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, K35, M35, N35, P35, S35, V35, V35A, 35B, 36, A36, A36TC, B36TC 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B (T-42A), 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 150€, 150F, 1500, 150H, 150J. 150K, A150K, 150L, A150L, 150M, A150M, 152, A152 PA-60-700P 58A 60, A60, B60 Make Aerostar Beech Beech Beech Beech Cessna Item Sheet 1 of 9

AML AMDT Date 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 Certification Basis for design change (See Note 1) 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity 3A12 3A17 A13CE A20CE 5A6 3A13 3A24 Aircraft Model 172E, 172F, 172G, 172H, 1721, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S 172RG 177, 177A, 177B 177RG 180H, 180J, 180K 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182, 182S, 182T, T182T 185D, 185E, A185E, A185F Make Cessna Cessna Cessna Cessna Cessna Cessna Cessna Item 10. 11. 12. 13. Sheet 2 of 9

AML AMDT Date 11/14/03 11/14/03 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 Certification Basis for design change (See Note 1) 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity A4CE A16CE 3A21 3A10 Aircraft Model 206, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, 206H, U206B, U206C, U206E, U206F, U206G, TP206А, TP206B, TP206C, T206H, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, 207, T207, 207A, T207A 210, 210-5 (205), 210-5A (205A), 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N, T210N, P210N, 210R, 310, 310A, 310B, 310C, 310D, 3310н, 3161,310J, 3105-1. 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, TU206G T210R, P210R T310R Make Cessna Cessna Cessna Cessna Item 14. 15. 16. 17. Sheet 3 of 9

AML AMDT Date 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 Certification Basis for design change 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity 3A25 3A25 A2CE A6CE 3A25 A7CE A25CE A28CE Aircraft Model 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F 335 336 337, 337A, 337B, M337B, T337B, 337C, T337C, 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, P337H, T337H, T337H-SP 340, 340A 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 404, 406 441 Make Cessna Cessna Cessna Cessna Cessna Cessna Cessna Cessna Item 18. 19 20 21. 22 23. 24. 25. Sheet 4 of 9

AML AMDT Date 11/14/03 11/14/03 11/14/03 03/17/06 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 Certification Basis for design change (See Note 1) 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity A37CE A12SO A-806 A00011LA 2A3 1A10 Aircraft Model 208, 208A, 208B 112, 112TC, 112B, 112TCA, 114, 114A, 114B, 114TC DHC-2 Mark I. DHC-2 Mark i, GA8 M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S PA-23, PA-23-160, PA-23-235, PA-23-250, PA-E23-250 Make Cessna Commander Aircraft DeHavilland Bombardier Gippsland Aeronautics Mooney Piper Item 26 27. 28 29. 30. 31. Sheet 5 of g

AML AMDT Date 11/14/03 11/14/03 11/14/03 10/23/07 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 See Note 2 Certification Basis for design change (See Note 1) 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity 2A13 A1EA A20SO A3SO A7SO A19SO Aircraft Model PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA-28-161, PA-28-180, PA-28-235, PA-28S-160, PA-28R-180, PA-28S-180, PA-28-181, PA-28R-200, PA-28R-201, PA28R-201T, PA-28RT-201, PA-28RT-201T, PA-28-201T, PA-28-236 PA-30, PA-39, PA-40 PA-31, PA-31-300, PA-31-325, PA-31-350 PA-32R-300 PA-32R-301 (SP), PA-32R-301(HP), PA-32R-301T, PA-32-301, PA-32-301T PA-34-220T PA-44-180, PA-44-180T Make Piper Piper Piper Piper Piper Piper Item 33 34. 36. 37. Sheet 6 of 9

AML AMDT Date 11/14/03 11/14/03 159-08293-0002 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 Certification Basis for design change (See Note 1) 14 CFR Part 23 Amdt 23-1 thru 23-54 14 CFR Part 23 Amdt 23-1 thru 23-54 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Original Type Certificate Serial Number Number Effectivity A25SO A51EU Aircraft Model PA-46-310P, PA-46-350P TB9, TB 10, TB20, TB21, TB200 Make Piper Socata Item 38 39 Sheet 7 of g

FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 250 Multi-Function Display System with Optional Traffic and Weather Sensors SA01205WI-D Note 1: To comply with the airworthiness requirements in effect on the date of application for this project, the certification basis for each design change is shown. These requirements will be applied regardless of the original certification basis of the airplane (CAR 3 or FAR 23.) 10u revision to th. - dated et-14-20 List. If the TIS option is installed, Airplane Flight Manual Supplement 006-10315-0000, Rev. - dated 11-14-2003. Later FAA Approved revisions to the above data are incorporated without revision to this Approved Model List. 159-08293-0002 Rev. C Note 1: To ange is stin. These requirements Note 2: Master Drawing List 159-08293-0001, Rev. A dated 10-20-2003.

Sheet 8 of 9

## Every issue (6)

- November 20, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/72/c5/72c57ec80721c35cecd6382a2296ac80e5c4eee20713edb01bfca6956df00a5a)
- November 20, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/72/c5/72c57ec80721c35cecd6382a2296ac80e5c4eee20713edb01bfca6956df00a5a)
- May 18, 2004: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/4f/36/4f36dc573b41332e74822d4890a411129f3878f70712c4e7e9a49a5e8b92e9f9)
- May 18, 2004: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/4f/36/4f36dc573b41332e74822d4890a411129f3878f70712c4e7e9a49a5e8b92e9f9)
- November 14, 2003: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/4f/36/4f36dc573b41332e74822d4890a411129f3878f70712c4e7e9a49a5e8b92e9f9)
- November 13, 2003: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/4f/36/4f36dc573b41332e74822d4890a411129f3878f70712c4e7e9a49a5e8b92e9f9)

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