# STC SA00195SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Micro AeroDynamics Inc, United States
- Description: Installation of vortex generators on the wing and vertical tail surfaces.
- Applied: March 13, 1995
- Status date: December 8, 1995
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 5A4](https://openairdocs.org/tcds/5A4)
- Certificate PDF: https://openairdocs.org/files/sha256/ed/73/ed734414718ea11671b3b1498b331aaa27159ed962a74d804030ba9ebc93cf10
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6EE18063EBBCD2CC862579AB0059F8F3.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00195SE

## ADs that name it (0)

None.

## Approved models (13)

- Hawker Beechcraft Corporation 50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation B50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation C50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation D50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation D50A ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation D50B ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation D50C ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation D50E ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation E50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation F50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation G50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation H50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))
- Hawker Beechcraft Corporation J50 ([TCDS 5A4](https://openairdocs.org/tcds/5A4))

## What the certificate says

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

Thatted Bates of America Department of Transportation Federal Aviation Administration COPY Supplemental Type Certificate Number: SA00195SE This certificate issued to: Micro AeroDynamics, Inc.

4000 Airport Rd. Suite D Anacortes, WA 98221 98221 Part 3 of the Civil Air Regulations.

Original Product -Type Certificate Number: 5A4 Make: Beech Model: 50, B50, C50, D50, D50A, D50B, D50C, D50E, E50, F50, G50, H50, and J50 Description of Type Design Change: Installation of vortex generators on the wing and vertical tail surfaces in accordance with Drawing Package MA2050, Revision IR, dated April 12, 1995, and Installation Manual no May 6. 8505080.

MA2051, Revision IR, dated May 8, 1995, or later FAA approved revision.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only.

This approval should not be extended to aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. Additionally, if more than 5 vortex generators are damaged or missing, the aircraft is not to be considered airworthy. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft.

Date of Application: March 13, 1995 Date Reissued:

Date of Issuance: June 1, 1995 Date Amended: December 8, 1995 FEDERAL AVIATIO By firection of she l fortres nator, elviar но.

(Signature) Acting Manager, Seattle/Aircraft Certification Office (Title)

## Every issue (1)

- December 8, 1995: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ed/73/ed734414718ea11671b3b1498b331aaa27159ed962a74d804030ba9ebc93cf10)

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