# STC SA01105WI-D

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Honeywell International Inc., United States
- Description: Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors.  This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine).
- Applied: July 15, 2002
- Status date: August 24, 2007
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A12SO](https://openairdocs.org/tcds/A12SO), [TCDS A00011LA](https://openairdocs.org/tcds/A00011LA), [TCDS 2A3](https://openairdocs.org/tcds/2A3), [TCDS 1A10](https://openairdocs.org/tcds/1A10), [TCDS 2A13](https://openairdocs.org/tcds/2A13), [TCDS A19SO](https://openairdocs.org/tcds/A19SO), [TCDS A1EA](https://openairdocs.org/tcds/A1EA), [TCDS A20SO](https://openairdocs.org/tcds/A20SO), [TCDS A3SO](https://openairdocs.org/tcds/A3SO), [TCDS A7SO](https://openairdocs.org/tcds/A7SO), [TCDS A51EU](https://openairdocs.org/tcds/A51EU), [TCDS A-806](https://openairdocs.org/tcds/A-806), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 3A19](https://openairdocs.org/tcds/3A19), [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS 3A17](https://openairdocs.org/tcds/3A17), [TCDS A13CE](https://openairdocs.org/tcds/A13CE), [TCDS A20CE](https://openairdocs.org/tcds/A20CE), [TCDS 5A6](https://openairdocs.org/tcds/5A6) and 16 more
- Certificate PDF: https://openairdocs.org/files/sha256/f0/c1/f0c18fcd8bd10c727a1f091b262ca7e4f7b14d022e87bae5be4c7b14f41c624a
- Approved model list and other attachments: [SA01105WI-D_AML.pdf](https://openairdocs.org/files/sha256/36/49/3649741652e795195cbe64a70463d79d3d064b6a5d4c8d4ca04b27668624d93d)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177362993020260115150931.0001
- DRS record last changed: January 15, 2026
- Page: https://openairdocs.org/stc/SA01105WI-D

## ADs that name it (0)

None.

## Approved models (317, 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 150 ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- 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 (USAF T-41A) ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172G ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172H (USAF T-41A) ([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 177B ([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))

All 317: https://openairdocs.org/stc/SA01105WI-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: SA01105WI-D This certificate issued to: Honeywell International Inc.

23500 W. 105th Street Olathe, KS 66061 Part * of the" Regulations.

Original Product - -Type Certificate Number: * See attached FAA Approved Model List Make: (AML) No. 159-08288-0001 for the list of Model: * approved airplane models and applicable airworthiness regulations.

Installation of the Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors.

REQUIRED DATA: AML No. 159-08288-0001, Revision -, dated 8-16-2002. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate.

1. Compatibility of this design with previously approved modifications must be determined by the installer.

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.

The FAA will reissue the certificate in the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number To (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

*U.S.G.P.O: 1989-662-030

### SA01105WI-D_AML.pdf

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

Issue Date: 8/16/2002 AML AMDT Date 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 159-08288-0001 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 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity A17WE ЗА15 ЗА16 A23CE A12CE 3А19 Aircraft Model PA-60-600, PA-60-601, PA-60-601P, PA-60-602P 35-B33, 35-C33, 35-C33А, 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, 58P, 58PA, 58TC, 58TCА 150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 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 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 159-08288-0001 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 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity ЗА 12 ЗА17 A13CE A20CE 5A6 3А13 3A24 Aircraft Model 172E, 172F, 172G, 172H, 1721, 172K, 172L, 172M, 172N, 172P, 172Q, 172R, 172S 172RG 177, 177А, 177B 177RG 180H, 180J, 180K 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182, 1825, 182T, 185D, 185E, A185E, A185F Make Cessna Cessna Cessna Cessna Cessna Cessna Cessna Item 10. 11. 12. 13. Sheet 2 of 9

AML AMDT Date 7/15/05 8/16/02 8/24/07 8/16/02 159-08288-0001 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 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity A4CE A16CE A37CE ЗА21 Aircraft Model 7206C, P2DD, PA.,PE, U206. U206A, U206B, U206C, U206D, U206E, U206F, U206G, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H 207, T207, 207A, T207A 208, 208A, 208B 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, T210R, P210R Make Cessna Cessna Cessna Cessna Item 14. 15. 16. 17. Sheet 3 of 9

AML AMDT Date 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 8/16/02 159-08288-0001 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 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity ЗА10 3A25 ЗА25 A2CE A6CE 3A25 Aircraft Model 310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, 310K, 310L, 310N, 310P T310R. 310Q, T310Q, 310R, 320D, 320Е, 320. 320В, 320С, 337, 337А, 337В, M337B, T337B, 337C, T337C, 337D, T337D, 337E, T337E, 337F, T337F, 337G, T337G, 337H, P337H, T337H, T337H-SP 335 336 340, 340A Make Cessna Cessna Cessna Cessna Cessna Cessna Item 18. 19. 20. 21. 22. 23. Sheet 4 of 9

AML AMDT Date 8/16/02/ 8/16/02 8/16/02 8/16/02 8/16/02/ 5/31/07 8/16/02 8/16/02 159-08288-0001 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 (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 14CFR 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 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity A7CE A25CE A28CE A12SO A-806 A00011LA 2A3 1A10 Aircraft Model 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 404, 406 441. 112, 112TC, 112B, 112TCА, 114, 114А, 114B, 114TC DHC-2 Mark i. DHC-2 Mark III 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 Cessna Cessna Commander Aircraft DeHavilland Bombardier Gippsland Aeronautics Mooney Piper Item 24. 25 26. 27. 28 29. 30. 31. Sheet 5 of 9

AML AMDT Date 8/16/02 8/16/02 8/16/02 7/15/05 7/15/05 159-08288-0001 Rev. C Master Drawing List and Flight Manual Supplement See Note 2 See Note 2 See Note 2 See Note 2 See Note 3 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 FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity 2A13 A1EA A20SO A3SO 3246018 & up 3257001 & up A3SO 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-301 (SP), PA-32R-301 (HP), PA-32R-301T, PA-32-301, PA-32-301T, PA-32-301FT, PA-32-301XTC PA-32R-301(HP), PA-32R-301T PA-32-301FT, PA-32-301XTC Make Piper Piper Piper Piper Piper Item 32. 33. 34. 35. 36. Sheet 6 of 9

Rev. C AML AMDT Date 8/16/02 8/16/02 8/16/02 8/16/02 Master Drawing List and Flight Manual Supplement See Note 2 See Note 3 See Note 2 See Note 2 159-08288-0001 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 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D Original Type Certificate Serial Number Number Effectivity A7SO 3449001 & up A7SO A19SO A51EU Aircraft Model PA-34-200, PA-34-200T, PA-44-180, PA-44-180T TB9, TB 10, TB20, TB21, PA-34-220T PA-34-220T TB200 Make Piper Piper Piper Socata Item 37. 38. 39. 40. Sheet 7 of 9

FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-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.) If the KMH 980 is installed, Airplane Flight Manual Supplement 006-10305-0000, Rev. - dated 8-16-2002. If the KTA 970 is installed, Airplane Flight Manual Supplement 006-10305-0001, Rev. - dated 8-16-2002. If the KMH 880 is installed, Airplane Flight Manual Supplement 006-10305-0002, Rev. - dated 8-16-2002. If the KTA 870 is installed, Airplane Flight Manual Supplement 006-10305-0003, Rev. - dated 8-16-2002. If the KGP 560 is installed, Airplane Flight Manual Supplement 006-10305-0004, Rev. - dated 8-16-2002. If the KGP 860 is installed, Airplane Flight Manual Supplement 006-10305-0005, Rev. - dated 7-15-2005. Later FAA approved revisions to the above data are incorporated without revision to this Approved Model List. If the KMH 980 is installed, Airplane Flight Manual Supplement 006-10306-0000, Rev. - dated 8-16-2002. If the KMH 880 is installed, Airplane Flight Manual Supplement 006-10306-0001, Rev. - dated 8-16-2002. Later FAA approved revisions to the above data are incorporated without revision to this Approved Model List. 159-08288-0001 Rev. C Note 2: Master Drawing List 159-08288-0200, Rev. A dated 8-6-2002. Note 3: Master Drawing List 159-08288-0100, Rev. A dated 8-6-2002.

Sheet 8 of 9

159-08288-0001 Rev. C APPROVED Robert G. Murray DAS Administrator Honeywell International Inc. DAS-500863-CE Robert G. Murray DAS Administrator Honeywell International Inc. DAS-500863-CE Richard B. Sleigh / for Chris Durkin DAS Administrator Honeywell International Inc. DAS-500863-CE the 13.83 faR Chris Durkin DAS Administrator Honeywell International Inc. DAS-500863-CE FAA Approved Model List (AML) Honeywell International Inc. for the Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic, Terrain and Weather Sensors SA01105WI-D REVISIONS DATE DESCRIPTION 8-16-02 Original Issue. 7-15-05 Corrected Item 14 to show Correct Models. Add PA-32-301FT and PA-32-301XTC to item 33 & 34. Added "Later FAA Approved Revisions" verbiage. Add KGP 860 AFMS to note 2. Added Revision History/Approval page. Reformatted to 8 sheets 5/31/2007 Added Gippsland Aeronautics GA8 as new item 28. Re-numbered original items 28 through 38 as 29 through 39, respectively. 8/24//2007 Changed to revision C Added Cessna 208, 208A, and 208B as new item 16. Re-numbered original items 16 through 39 as 17 through 40, respectively.

SHT 1-7 liV REV Sheet 9 of 9

## Every issue (6)

- August 24, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f0/c1/f0c18fcd8bd10c727a1f091b262ca7e4f7b14d022e87bae5be4c7b14f41c624a), [SA01105WI-D_AML.pdf](https://openairdocs.org/files/sha256/36/49/3649741652e795195cbe64a70463d79d3d064b6a5d4c8d4ca04b27668624d93d)
- August 24, 2007: Amended, Current. [certificate](https://openairdocs.org/files/sha256/f0/c1/f0c18fcd8bd10c727a1f091b262ca7e4f7b14d022e87bae5be4c7b14f41c624a), [SA01105WI-D_AML.pdf](https://openairdocs.org/files/sha256/36/49/3649741652e795195cbe64a70463d79d3d064b6a5d4c8d4ca04b27668624d93d)
- May 31, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3f/de/3fde725497229b1c1516dac314155a50f7c2e86514f7e016550102736d17d835)
- May 31, 2007: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3f/de/3fde725497229b1c1516dac314155a50f7c2e86514f7e016550102736d17d835)
- July 15, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3f/de/3fde725497229b1c1516dac314155a50f7c2e86514f7e016550102736d17d835)
- July 15, 2005: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/3f/de/3fde725497229b1c1516dac314155a50f7c2e86514f7e016550102736d17d835)

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