STC SA00795SE

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Amended
Status date
July 19, 2001
Applied
March 2, 2000
Product
Aircraft · Single-Engine
Certification basis
Part 21, Part 23

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2131, Revision A, dated April 22, 2001, and Installation Manual MA2132, Revision A, dated April 22, 2001, or later FAA approved revision of either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.

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.

Number SA00795SE This certificate, issued to Micro AeroDynamics, Inc.

4000 Airport Rd., Suite D Anacortes, WA 98221 Part 4A of the Civil Aviation Regulations, and Part 23 of the Federal Aviation Regulations.

Original ProductType Certificate Number: A-759, A-21CE Make: American Champion Model: 7ECA, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KC, 7KCAB, (TCDS A-759), 8KCAB, 8GCBC (TCDS A21CE)

Description of the Type Design Change: Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2131, Revision A, dated April 22, 2001, and Installation Manual MA2132, Revision A, dated April 22, 2001, or later FAA approved revision of either of these documents.

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

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 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. A copy of this Certificate 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.

Date of application: March 2, 2000 Date reissued:

Date of issuance: April 18, 2000 Date amended: July 19, 2001

(Signature) Acting Manager, Seattle Aircraft Certification Office (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 · 13

MakeModelData sheet
American Champion Aircraft Corp.7ECAA-759
American Champion Aircraft Corp.7GCA-759
American Champion Aircraft Corp.7GCAA-759
American Champion Aircraft Corp.7GCAAA-759
American Champion Aircraft Corp.7GCBA-759
American Champion Aircraft Corp.7GCBAA-759
American Champion Aircraft Corp.7GCBCA-759
American Champion Aircraft Corp.7HCA-759
American Champion Aircraft Corp.7JCA-759
American Champion Aircraft Corp.7KCA-759
American Champion Aircraft Corp.7KCABA-759
American Champion Aircraft Corp.8GCBCA21CE
American Champion Aircraft Corp.8KCABA21CE