# STC SA01969SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Mid-Continent Instruments and Avionics, United States
- Description: Installation of a Mid-Continent MD302 Standby Attitude Module
- Applied: March 25, 2013
- Status date: October 14, 2015
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23, Part 25, Part 27, Part 29
- Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE), [TCDS A19SW](https://openairdocs.org/tcds/A19SW), [TCDS A22NM](https://openairdocs.org/tcds/A22NM), [TCDS A17EU](https://openairdocs.org/tcds/A17EU), [TCDS A29EU](https://openairdocs.org/tcds/A29EU), [TCDS A14CE](https://openairdocs.org/tcds/A14CE), [TCDS A24CE](https://openairdocs.org/tcds/A24CE), [TCDS 3A15](https://openairdocs.org/tcds/3A15), [TCDS 3A16](https://openairdocs.org/tcds/3A16), [TCDS A23CE](https://openairdocs.org/tcds/A23CE), [TCDS 3A20](https://openairdocs.org/tcds/3A20), [TCDS A31CE](https://openairdocs.org/tcds/A31CE), [TCDS A37CE](https://openairdocs.org/tcds/A37CE), [TCDS A28CE](https://openairdocs.org/tcds/A28CE), [TCDS A27CE](https://openairdocs.org/tcds/A27CE), [TCDS A00014WI](https://openairdocs.org/tcds/A00014WI), [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH), [TCDS A57CE](https://openairdocs.org/tcds/A57CE), [TCDS A47CE](https://openairdocs.org/tcds/A47CE), [TCDS A00008DE](https://openairdocs.org/tcds/A00008DE) and 42 more
- Certificate PDF: https://openairdocs.org/files/sha256/cb/1a/cb1ae0bf7dc5ddca50611e90f9c241d5d35aaba569e50288c87bd717a4a8a2da
- Approved model list and other attachments: [SA01969SE_AML.pdf](https://openairdocs.org/files/sha256/66/c7/66c7f1b8c05065bcaa0c3885cdcd7cd4179e49cafffab2a76665e17a9e610f6c)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/19E197239A6E0E1386257EE500538A8B.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01969SE

## ADs that name it (0)

None.

## Approved models (462, 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))
- Air Tractor Inc. AT-602 ([TCDS A19SW](https://openairdocs.org/tcds/A19SW))
- Air Tractor Inc. AT-802 ([TCDS A19SW](https://openairdocs.org/tcds/A19SW))
- Air Tractor Inc. AT-802A ([TCDS A19SW](https://openairdocs.org/tcds/A19SW))
- Aviat Aircraft Inc A-1 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Aviat Aircraft Inc A-1A ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Aviat Aircraft Inc A-1B ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Aviat Aircraft Inc A-1C-180 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Aviat Aircraft Inc A-1C-200 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- B-N Group Ltd. BN-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-2 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-3 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-6 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-8 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2A-9 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-20 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-21 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-26 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2B-27 ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN-2T-4R ([TCDS A17EU](https://openairdocs.org/tcds/A17EU))
- B-N Group Ltd. BN2A MK. III ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- B-N Group Ltd. BN2A MK. III-2 ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- B-N Group Ltd. BN2A MK. III-3 ([TCDS A29EU](https://openairdocs.org/tcds/A29EU))
- Beechcraft Corporation 100 ([TCDS A14CE](https://openairdocs.org/tcds/A14CE))
- Beechcraft Corporation 1900 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 1900C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 1900C (C-12J) ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 1900D ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 200C ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 300 ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 300LW ([TCDS A24CE](https://openairdocs.org/tcds/A24CE))
- Beechcraft Corporation 35-33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-A33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-B33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-C33 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 35-C33A ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 36 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation 56TC ([TCDS 3A16](https://openairdocs.org/tcds/3A16))
- Beechcraft Corporation 58 ([TCDS 3A16](https://openairdocs.org/tcds/3A16))

All 462: https://openairdocs.org/stc/SA01969SE/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.

United States of America Department of Transportation – Federal Aviation Administration Supplemental Type Certificate Number SA01969SE This Certificate issued to: Mid-Continent Instruments and Avionics 9400 East 34th Street North Wichita, KS 67226 Part 23 of the Federal Aviation Regulations.

Original Product - Type Certificate Number: See attached FAA-Approved Model List (AML) issued 17 January 2014 or later FAA-approved revisions for the list Make: of approved airplane models, applicable installation data Model: requirements, and specific limitations.

Description of Type Design Change: Installation of a Mid -Continent MD302 Standby Attitude Module in accordance with Master Data List AM0261 -DL02-00, specified on the attached FAA-Approved Model List (AML) issued 17 January 2014, or later FAA -approved revision. Altered aircraft must be maintained in accordance with t he Instructions fo r Continued Airworthiness (ICA) document AM0261-IC01-00, Revision “—”, dated 11 November 2013 or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies to the aircraft listed on the AML only. This approval should not be applied to an eligible aircraft model on which other previously-approved modifications are incorporated unless it is determined by the installer that the relationship between this change and the other previously -approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

(Limitations and Conditions continued on Page 3 of 3)

Date of application: March 25, 2013 Date reissued:

Date of issuance: January 17, 2014 Date amended:

(Signature) ODA Administrator (Title)

United States of America Department of Transportation – Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01969SE

The MD302 cannot be used as a primary display. For aircraft that require the pilot to hold a type rating, the candidate aircraft must be equipped with primary flight displays that include vertical tape displays of airspeed and altitude. This AML STC is only applicable to 14 CFR part 23 Class I, II, III, and IV aircraft as defined in Advisory Circular 23.1309- 1(). 14 CFR part 25, 27, and 29 aircraft are not authorized under this STC.

For airplanes with maximum gross weights of 6000 lbs or more (AC 23.1309- 1() Class II and IV aircraft), the primary display systems must consist of at least two displays of airspeed, altitude, and attitude. If the primary display system does not include two displays of airspeed, altitude, and attitude, the installer must obtain an independent approval addressing the system safety aspects of the applicable amendment of 14 CFR 23.1309, Equipment, Systems, and Installations.

A copy of this certificate and the FAA -approved AML must be maintained as part of the permanent records for the modified aircraft.

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.

-------------------------------END-------------------------------

FAA Form 8110-2.1(10-69) Page 3 of 3

### SA01969SE_AML.pdf

FAA Approved Model List (AML) No. SA01969SE Mid-Continent Instruments For Installation of MD302 Attitude Module Page 1 of 6

Original Issue Date: January 17, 2014 Item Aircraft Make Aircraft Model TCDS Certification Basis for Alteration MDL Number / Revision / Date ** AFMS Number / Revision / Date ** AML Amendment Date 1 Aerostar PA-60-600, PA-60-601, PA-60-601P, PA-60-602P, PA-60-700P A17WE 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 2 Air Tractor AT-602, AT-802, AT-802A A19SW 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 3 Aviat Aircraft A-1, A-1A, A-1B, A-1C-180, A-1C-200 A22NM 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 11/4/2014 4 Beechcraft 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33, E33A, E33C, F33, F33A, F33C, G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36, G36, A36TC, B36TC 3A15 CAR 3 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014 5 Beechcraft 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, 95, B95 3A16 CAR 3 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014 6 Beechcraft 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-A90-1 (RU-21B), 65-A90-1 (RU-21C), 65-A90-1 (RU-21E), 65-A90-1 (RU-21H), 70, C90, C90A, C90GT, C90GTi, B90, E90, H90 (T-44A) 3A20 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 11/4/2014 7 Beechcraft 99, 99A, 99A (FACH), A99, A99A, B99, C99, 100, A100 (U-21F), B100 A14CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 11/4/2014 8 Beechcraft 58P, 58PA, 58TC, 58TCA A23CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014 9 Beechcraft 200, 200C, B200†, B200C†, B200T†, B200CT†, B200GT, 1900*, 1900C*, 1900C (C-12J)*, 1900D* A24CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 10 Beechcraft 300, 300LW A24CE 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 11 Beechcraft F90 A31CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original

FAA Approved Model List (AML) No. SA01969SE Mid-Continent Instruments For Installation of MD302 Attitude Module Page 2 of 6

Item Aircraft Make Aircraft Model TCDS Certification Basis for Alteration MDL Number / Revision / Date ** AFMS Number / Revision / Date ** AML Amendment Date 12 B-N Group Ltd.

BN-2, BN-2A, BN-2A-6, BN-2A-8, BN-2A-2, BN-2A-9, BN-2A-3, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A-27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN-2T-4R A17EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 13 B-N Group Ltd. BN2A MK. III, BN2A MK. III -2, BN2A MK. III -3 A29EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 14 Cessna 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 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 15 Cessna 182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M, 182N, 182P, 182Q, 182R, 182S, 182T, R182, T182, T182T, TR182 3A13 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 16 Cessna 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, P210N, T210N, 210R, P210R, T210R 3A21 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 17 Cessna 320, 320-1, 320A, 320B, 320C, 320D, 320E, 320F, 335, 340, 340A 3A25 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 18 Cessna LC40-550FG, LC41-550FG, LC42-550FG, T240 A00003SE 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 19 Cessna 510 A00014WI 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014 20 Cessna 501*, 551* A27CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 21 Cessna 441 A28CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014 22 Cessna 208, 208B A37CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014

FAA Approved Model List (AML) No. SA01969SE Mid-Continent Instruments For Installation of MD302 Attitude Module Page 3 of 6

Item Aircraft Make Aircraft Model TCDS Certification Basis for Alteration MDL Number / Revision / Date ** AFMS Number / Revision / Date ** AML Amendment Date 23 Cessna 206, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, 206H, U206B, U206C, U206D, U206E, U206F, U206G, TP206A, TP206B, TP206C, T206H, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G A4CE CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 24 Cessna 401, 401A, 401B, 402, 402A, 402B, 402C, 411, 411A, 414, 414A, 421, 421A, 421B, 421C, 425 A7CE CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 25 Cirrus SR20, SR22, SR22T A00009CH 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 5/16/2014 26 Diamond Aircraft Industries GmbH DA 40, DA 40 F, DA 40 NG A47CE JAR 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 27 Diamond Aircraft Industries GmbH DA 42, DA 42 NG, DA 42 M-NG A57CE JAR 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 28 Dornier Luftfahrt GmbH Do 28 D, Do 28 D-1, Dornier 228-100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 228-202, Dornier 228-212 A16EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 29 EADS SOCATA TBM 700 A60EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 30 Embraer EMB-500* A59CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 31 Embraer EMB-505* A60CE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 32 Gippsland Aeronautics Pty. Ltd.

GA8, GA8-TC320 A00011LA 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 33 Interceptor 200, 200A, 200B, 200C, 200D, 400 3A18 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 34 Liberty Aerospace XL-2 A00008DE 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015

FAA Approved Model List (AML) No. SA01969SE Mid-Continent Instruments For Installation of MD302 Attitude Module Page 4 of 6

Item Aircraft Make Aircraft Model TCDS Certification Basis for Alteration MDL Number / Revision / Date ** AFMS Number / Revision / Date ** AML Amendment Date 35 M7 Aerospace SA227-CC, SA227-DC (C-26B) A18SW CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 36 M7 Aerospace SA26-T, SA26-AT, SA226-T, SA226-AT, SA226-T(B), SA227-AT, SA227-TT A5SW CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 37 M7 Aerospace SA226-TC, SA227-AC (C-26A), SA227-PC, SA227-BC (C-26A) A8SW 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 38 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 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 11/4/2014 39 Mitsubishi MU-2B*, MU-2B-10*, MU-2B-15*, MU-2B-20*, MU-2B-25*, MU-2B-26*, MU-2B-30*, MU-2B-35*, MU-2B-36* A2PC CAR 3 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 11/4/2014 40 Mooney M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, M20TN 2A3 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 41 Mooney M22 A6SW CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 42 Pacific Aerospace 750XL A50CE 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 43 Piaggio P-180 A59EU 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 44 Pilatus PC-6, PC-6-H1, PC-6-H2, PC-6/350, PC-6/350-H1, PC-6/350-H2, PC-6/A, PC-6/A-H1, PC-6/A-H2, PC-6/B-H2, PC-6/B1-H2, PC-6/B2-H2, PC-6/B2-H4, PC-6/C-H2, PC-6/C1-H2 7A15 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 45 Pilatus PC-7 A50EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 46 Pilatus PC-12, PC-12/45, PC-12/47, PC-12/47E A78EU 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 47 Piper PA-24, PA-24-250, PA-24-260, PA-24-400 1A15 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015

FAA Approved Model List (AML) No. SA01969SE Mid-Continent Instruments For Installation of MD302 Attitude Module Page 5 of 6

Item Aircraft Make Aircraft Model TCDS Certification Basis for Alteration MDL Number / Revision / Date ** AFMS Number / Revision / Date ** AML Amendment Date 48 Piper PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28-235, PA-28S-160, PA-28S-180, PA-28R-180, PA-28R-200, PA-28-151, PA-28-161, PA-28-181, PA-28R-201, PA-28R-201T, PA-28-236, PA-28RT-201, PA-28RT-201T, PA-28-201T 2A13 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 49 Piper PA-44-180, PA-44-180T A19SO 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 50 Piper PA-31, PA-31-300, PA-31-325, PA-31-350 A20SO CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 51 Piper PA-42 , PA-42-720, PA-42-1000 A23SO 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 52 Piper PA-46-500TP A25SO 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 53 Piper PA-46-310P, PA-46-350P, PA-46R-350T A25SO 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 54 Piper PA-42-720R A32SO 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 55 Piper PA-32-260, PA-32-300, PA-32S-300, PA-32R-300, PA-32RT-300, PA-32RT-300T, PA-32-301FT, PA-32-301XTC, PA-32R-301 (SP), PA-32R-301 (HP), PA-32R-301T, PA-32-301, PA-32-301T A3SO CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 56 Piper PA-34-200, PA-34-200T, PA-34-220T A7SO 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 57 Piper PA-31P, PA-31T, PA-31T1, PA-31T2, PA-31T3, PA-31P-350 A8EA CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 58 Quest Kodiak 100 A00007SE 14 CFR Part 23 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 11/4/2014 59 SOCATA TB 9, TB 10, TB 20, TB 21, TB 200 A51EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 60 Twin Commander 690C, 690D, 695, 695A, 695B 2A4 CAR 3 AML0261-DL02-00; Rev -, 1/17/2014 AML0261-FM01-00; Rev -, 1/17/2014 Original 61 Twin Commander 690, 690A, 690B 2A4 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 62 Twin Commander 500, 500A, 500B, 500U, 520, 560, 560A, 560E, 500S 6A1 CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015

FAA Approved Model List (AML) No. SA01969SE Mid-Continent Instruments For Installation of MD302 Attitude Module Page 6 of 6

Item Aircraft Make Aircraft Model TCDS Certification Basis for Alteration MDL Number / Revision / Date ** AFMS Number / Revision / Date ** AML Amendment Date 63 Twin Commander 700 A12SW 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 64 Viking Air DHC-6-1, DHC-6-100, DHC-6-200, DHC-6-300, DHC-6-400 A9EA CAR 3 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 65 Vulcanair S.p.A.

P.68, P.68B, P.68C, P.68C-TC, P.68 "Observer", AP68TP-300 "Spartacus", P.68TC "Observer", AP68TP.600 "Viator", P.68 "Observer 2", P.68R A31EU 14 CFR Part 23 AM0261-DL02-00; Rev A, 9/15/2015 AM0261-FM01-00; Rev -, 1/17/2014 10/14/2015 ** or later FAA Approved revision

FAA Approved:_Original signed by Daniel Hilton Daniel Hilton Associate ACO Manager Electrical Systems and Avionics, ACE-119W Wichita Aircraft Certification Office

General Notes

1. This STC is only applicable to 14 CFR Part 23 Class I, II, III & IV aircraft as defined in Advisory Circular 23.1309-1( ). 14 CFR Part 25, 27, & 29 aircraft are not authorized under this STC.

2. Unless otherwise indicated on this AML, MD302 part number 6420302-( ) is eligible for installation on aircraft shown on this listing.

3. This AML is arranged alphabetically by aircraft make.

Model-Specific Notes * Candidate aircraft must be currently equipped with primary flight displays that include vertical tape displays of airspeed and altitude.

† Candidate 200/B200 series aircraft that require a type rating must be currently equipped with primary flight displays that include vertical tape displays of airspeed and altitude.

## Every issue (4)

- October 14, 2015: Amended, Current. [certificate](https://openairdocs.org/files/sha256/cb/1a/cb1ae0bf7dc5ddca50611e90f9c241d5d35aaba569e50288c87bd717a4a8a2da), [SA01969SE_AML.pdf](https://openairdocs.org/files/sha256/66/c7/66c7f1b8c05065bcaa0c3885cdcd7cd4179e49cafffab2a76665e17a9e610f6c)
- November 4, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/cb/1a/cb1ae0bf7dc5ddca50611e90f9c241d5d35aaba569e50288c87bd717a4a8a2da), [SA01969SE_AML.pdf](https://openairdocs.org/files/sha256/5f/6e/5f6e5d792160de6f44bba158d46b41f6afda3c525c005dab63851dba79aa65b7)
- May 16, 2014: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/cb/1a/cb1ae0bf7dc5ddca50611e90f9c241d5d35aaba569e50288c87bd717a4a8a2da), [SA01969SE_AML.pdf](https://openairdocs.org/files/sha256/de/f7/def7b505062600857da1c542d7052d74f2dd6be60f12c74f2afca2a95fdc2bcc)
- January 17, 2014: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/cb/1a/cb1ae0bf7dc5ddca50611e90f9c241d5d35aaba569e50288c87bd717a4a8a2da), [AML SA01969SE.pdf](https://openairdocs.org/files/sha256/f4/eb/f4ebd09bf8a19e515523d4cd4c94bc3c3fcefa0f78eb199ddc660582c5b27b63)

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