# STC SA02010WI

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Mid-Continent Instruments and Avionics, USA
- Description: Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD)
- Applied: June 28, 2022
- Status date: March 6, 2023
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS A31CE](https://openairdocs.org/tcds/A31CE), [TCDS 5A3](https://openairdocs.org/tcds/5A3), [TCDS A00010WI](https://openairdocs.org/tcds/A00010WI), [TCDS 3A10](https://openairdocs.org/tcds/3A10), [TCDS A00014WI](https://openairdocs.org/tcds/A00014WI), [TCDS A27CE](https://openairdocs.org/tcds/A27CE), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS A7CE](https://openairdocs.org/tcds/A7CE), [TCDS A1WI](https://openairdocs.org/tcds/A1WI), [TCDS 3A25](https://openairdocs.org/tcds/3A25), [TCDS A00003SE](https://openairdocs.org/tcds/A00003SE), [TCDS A16EU](https://openairdocs.org/tcds/A16EU), [TCDS A2PC](https://openairdocs.org/tcds/A2PC) and 9 more
- Certificate PDF: https://openairdocs.org/files/sha256/91/2d/912d79d0c88c474bc7ab1cc6fb3aed4ff21cc76600b247363c7b69f9b3a95175
- Approved model list and other attachments: [SA02010WI_AML.pdf](https://openairdocs.org/files/sha256/a3/82/a38288983642fabf52aae1fcba801ad60784a939e4bf1f56b1644eb8646db741)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID122849357020230412144500.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02010WI

## ADs that name it (0)

None.

## Approved models (209, 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))
- Dornier Luftfahrt GmbH Do 28 D ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Do 28 D-1 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-100 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-101 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-200 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-201 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-202 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Dornier Luftfahrt GmbH Dornier 228-212 ([TCDS A16EU](https://openairdocs.org/tcds/A16EU))
- Mitsubishi Heavy Industries Ltd. MU-2B-25 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-26 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-26A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-36A ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-40 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. MU-2B-60 ([TCDS A10SW](https://openairdocs.org/tcds/A10SW))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B-20 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B-25 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B-26 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B-30 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B-35 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Mitsubishi Heavy Industries Ltd. 203 MU-2B-36 ([TCDS A2PC](https://openairdocs.org/tcds/A2PC))
- Pilatus Aircraft Limited PC-12 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/45 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/47 ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Pilatus Aircraft Limited PC-12/47E ([TCDS A78EU](https://openairdocs.org/tcds/A78EU))
- Piper Aircraft Inc. PA-42 ([TCDS A23SO](https://openairdocs.org/tcds/A23SO))
- Piper Aircraft Inc. PA-42-1000 ([TCDS A23SO](https://openairdocs.org/tcds/A23SO))
- Piper Aircraft Inc. PA-42-720 ([TCDS A23SO](https://openairdocs.org/tcds/A23SO))
- Piper Aircraft Inc. PA-42-720R ([TCDS A32SO](https://openairdocs.org/tcds/A32SO))
- Piper Aircraft Inc. PA-46-310P ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Piper Aircraft Inc. PA-46-350P ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Piper Aircraft Inc. PA-46-500TP ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Piper Aircraft Inc. PA-46-600TP ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Piper Aircraft Inc. PA-46R-350T ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Textron Aviation Inc. 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Textron Aviation Inc. 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 1900C (C-12J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 208 ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- Textron Aviation Inc. 208B ([TCDS A37CE](https://openairdocs.org/tcds/A37CE))
- Textron Aviation Inc. 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Textron Aviation Inc. 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))

All 209: https://openairdocs.org/stc/SA02010WI/models.md

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

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SA02010WI Mid-Continent Instruments and Avionics 9400 East 34th Street North Wichita, KS 67226 Part 23 Federal Aviation Regulations Multiple - AML STC See attached FAA Approved Model List (AML) SA02010WI issued March 6, 2023 or later FAA approved revision for the list of approved models, applicable installation data requirements, and specific limitations.

Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD) on Part 23 aircraft in accordance with Master Data List 22-002-DC4301 specified on the attached FAA Approved Model List (AML) issued March 6, 2023, or later FAA approved revision.

(1) Approval of this change in type design applies to the aircraft listed on the AML only.

(2) The installer must determine whether this design change is compatible with previously approved modifications. (Limitations and Conditions continued on Page 3 of 3) June 28, 2022 March 6, 2023 Kathryn Oatman Aeronautix Project ODA administrator ODA-834865-CE 3

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SA02010WI 3

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Certification Basis (continued from page 1):

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 attached AML.

b. The certification basis for parts changed or affected by the change is as follows:

33 Section

23.1

23.29

23.301(a)(b)(c)

23.303

23.305(a)

23.307(a)

23.337(a)(b)

23.341

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23.619

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23.1301

23.1306(b)

23.1308(b)(c)

23.1309(a)(1)(2)(c)(d)

23.1311(a)(2)

23.1321(c)

23.1323(a)(b)(c)(e)

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### SA02010WI_AML.pdf

FAA Approved Model List (AML) STC No. SA02010WI Mid-Continent Instruments and Avionics For Installation of MD23 FLEX Custom Function Display (CFD) Issued: March 6, 2023 Page 1 of 4

LOG OF REVISIONS Date Description 03/06/2023 Issue Date

**FAA APPROVED**

Kathryn Oatman Project ODA Administrator ODA-834865-CE

Aeronautix 3450 North Rock Road, Suite 300, Wichita, KS 67226

FAA Approved Model List (AML) STC No. SA02010WI Mid-Continent Instruments and Avionics For Installation of MD23 FLEX Custom Function Display (CFD) Issued: March 6, 2023 Page 2 of 4

**APPROVED MODEL LIST**

Aircraft Make Aircraft Model Type Certificate Data Sheet TC Certification Basis* Master Data List Rev/Date ** AFMS Rev/Date ** Original Approval / Amendment Date Aerostar PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P A17WE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.)

95, B95, B95A, D95A, E95, 95- 55, 95-A55, 95-B55, 95-B55A, 95-B55B (T-42), 95-C55, 95- C55A, D55, D55A, E55, E55A, 56TC, A56TC, 58, 58A, G58 3A16 CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.)

65 (L-23F), A65, A-65-8200, 65- 80, 65-A80, 65-A80-8800, 65- B80, 65-88, 65-90, 65-A90, 65- A90-1 (JU-21A), 65-A90-1 (U- 21A), 65-A90-1 (RU-21A), 65- A90-1 (RU-21D), 65-A90-1 (U- 21G), 65-A90-1 (RU-21H), 65- A90-2 (RU-21B), 65-A90-3 (RU- 21C), 65-A90-4 (RU-21E), 65- A90-4 (RU-21H), 70, C90, C90A, C90GT, C90GTi, B90, E90, H90 (T-44A) 3A20 CAR 3

14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.)

99, 99A, 99A (FACH), A99, A99A, B99, C99, 100, A100 (U- 21F), B100 A14CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.) 58P, 58PA, 58TC, 58TCA A23CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.)

200, 200C, B200, B200C, B200T, B200CT, B200GT, 1900, 1900C, 1900C (C-12J), 1900D, 300, 300LW, B300, B300C, B300C(MC-12W), B300C (UC- 12W) A24CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.) F90 A31CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Beechcraft (Textron Aviation Inc.)

45(YT-34), A45 (T-34A, B-45), D45(T-34B) 5A3 CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original

FAA Approved Model List (AML) STC No. SA02010WI Mid-Continent Instruments and Avionics For Installation of MD23 FLEX Custom Function Display (CFD) Issued: March 6, 2023 Page 3 of 4

Aircraft Make Aircraft Model Type Certificate Data Sheet TC Certification Basis* Master Data List Rev/Date ** AFMS Rev/Date ** Original Approval / Amendment Date Beechcraft (Textron Aviation Inc.) 390 A00010WI 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.)

310, 310A (USAF U-3A), 310B, 310C, 310D, 310E (USAF U-3B), 310F, 310G, 310H, E310H, 310I, 310J, 310J-1, E310J, 310K, 310L, 310N, 310P, T310P, 310Q, T310Q, 310R, T310R 3A10 CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.) 510 A00014WI 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.) 501, 551 A27CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.) 441 A28CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.) 208, 208B A37CE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.)

401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 A7CE CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.) 525, 525A, 525B, 525C A1WI 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.)

320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 335, 340, 340A 3A25 CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Cessna (Textron Aviation Inc.)

LC40-550FG, LC41-550FG, LC42-550FG, T240 A00003SE 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Dornier Luftfahrt GmbH Do 28D, Do 28D-1, Dornier 228- 100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, Dornier 228-212 A16EU 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original

FAA Approved Model List (AML) STC No. SA02010WI Mid-Continent Instruments and Avionics For Installation of MD23 FLEX Custom Function Display (CFD) Issued: March 6, 2023 Page 4 of 4

Aircraft Make Aircraft Model Type Certificate Data Sheet TC Certification Basis* Master Data List Rev/Date ** AFMS Rev/Date ** Original Approval / Amendment Date Mitsubishi MU-2B-25, MU-2B-26, MU-2B- 26A, MU-2B-35, MU-2B-36, MU-2B-36A, MU-2B-40, MU- 2B-60 A10SW CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Mitsubishi MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, MU-2B-25, MU-2B- 26, MU-2B-30, MU-2B-35, MU2B-36 A2PC CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Pilatus PC-12, PC-12/45, PC-12/47, PC-12/47E A78EU 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Piper Aircraft, Inc PA-42, PA-42-720, PA-42-1000 A23SO 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Piper Aircraft, Inc PA-46-310P, PA-46-350P, PA- 46R-350T, PA-46-500TP, PA-46- 600TP A25SO 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Piper Aircraft, Inc PA-42-720R A32SO 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Twin Commander 690, 690A, 690B, 690C, 690D, 695, 695A, 695B 2A4 CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Twin Commander 500, 500-A, 500-B, 500-U, 520, 560, 560-A, 560-E, 500-S 6A1 CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Twin Commander 700 A12SW 14 CFR Part 23 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original Viking Air Limited (Twin Otter) DHC-6-1, DHC-6-100, DHC-6- 200, DHC-6-300, DHC-6-400 A9EA CAR 3 22-002-DC4301, Rev. 0, 03/06/2023 22-002-FT2901, Rev. 0, 01/30/2023 Original

* see Type Certificate Data Sheet applicable to aircraft for complete TC certification basis ** or later FAA Approved Revision

## Every issue (1)

- March 6, 2023: Issued, Current. [certificate](https://openairdocs.org/files/sha256/91/2d/912d79d0c88c474bc7ab1cc6fb3aed4ff21cc76600b247363c7b69f9b3a95175), [SA02010WI_AML.pdf](https://openairdocs.org/files/sha256/a3/82/a38288983642fabf52aae1fcba801ad60784a939e4bf1f56b1644eb8646db741)

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