STC SA01439SE

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Amended
Status date
November 30, 2017
Applied
May 11, 2004
Product
Aircraft · Small Airplane
Certification basis
Part 3, Part 21
Data sheet
TCDS2A3

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of vortex generators on the wings and tail surfaces of the above model aircraft

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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)

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 17

MakeModelData sheet
Mooney Aircraft CorporationM202A3
Mooney Aircraft CorporationM20A2A3
Mooney Aircraft CorporationM20B2A3
See all 17 models

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
November 30, 2017Amended, currentCertificate
November 19, 2012Amended, earlier issueCertificate
August 4, 2004Issued, earlier issueCertificate