# STC SA01439SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Micro AeroDynamics Inc, United States
- Description: Installation of vortex generators on the wings and tail surfaces of the above model aircraft
- Applied: May 11, 2004
- Status date: November 30, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 3, Part 21
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3)
- Certificate PDF: https://openairdocs.org/files/sha256/2a/b9/2ab95a383f3b0115dbb355de33ad5d9966513c1bca5b6c5ca9a8febcd12aec0d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ECDB0FDCE6111EDB862581EC005C5B68.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01439SE

## ADs that name it (0)

None.

## Approved models (17)

- Mooney Aircraft Corporation M20 ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20A ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20B ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20C ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20D ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20E ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20F ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20G ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20J ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20K ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20L ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20M ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20R ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20S ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aviation Company Inc M20TN ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney International Corporation M20U ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney International Corporation M20V ([TCDS 2A3](https://openairdocs.org/tcds/2A3))

## 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.

Un ited S tates of Am erica Department of Transportation - Federal Aviation Administration Supplemental Type Certificate

Number SA01439SE

This certificate, issued to Micro AeroDynamics, Inc.

4000 Airport Road, Suite D Anacortes, WA 98221

Part 3 of the Civil Air Regulations.

Original ProductType Certificate Number: 2A3 Make: Mooney International Corporation Model: M20, M20A, M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K, M20L, M20M, M20R, M20S, M20TN, M20U, and M20V.

Description of the Type Design Change: Installation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package Document MA2198, Revision B, or later Federal Aviation Administration (FAA) approved revision, and Micro AeroDynamics Installation Instructions, Document MA2199, Revision B, or later FAA-approved revision. Maintained in accordance with Micro AeroDynamics Instructions for Continued Airworthiness (ICA), Document MA0666, Revision B, or later FAA-accepted 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 other aircraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and the ICA must be maintained as part of the permanent records for the modified aircraft.

NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.

Date of application: May 11, 2004 Date reissued:

Date of issuance: August 4, 2004 Date amended: 11/19/12; 11/30/17

FAA FORM 8110-2 (5/14) PAGE 1 OF 2 PAGES By direction of the Administrator

(Signature)

Manager, Seattle ACO Branch (Title)

## Every issue (3)

- November 30, 2017: Amended, Current. [certificate](https://openairdocs.org/files/sha256/2a/b9/2ab95a383f3b0115dbb355de33ad5d9966513c1bca5b6c5ca9a8febcd12aec0d)
- November 19, 2012: Amended, Historical. [certificate](https://openairdocs.org/files/sha256/a1/24/a124661e4c6e6135b7cf51a10eab7b37b7286ad2a4a042eb12a3465e93f1e29c)
- August 4, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d2/7f/d27fd4a1742ae9e43e8eb7d8388b11dd716c4ac8097d539b655c8c67e0af8a19)

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