STC SA00097SE

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Reissued
Status date
August 20, 2004
Applied
May 4, 1994
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheets
TCDS1A4TCDS1A6

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

What it approves

Installation of a vortex generator kit.

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.

United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate Number SA00097SE

This certificate, issued to: Micro Aerodynamics, Inc.

4000 Airport Road, Suite D Anacortes, WA 98221

Part * of the * Regulations.

Original Product⎯Type Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA00097SE for a list of approved airplane Model: models and applicable airworthiness regulations.

Description of the Type Design Change: Installation of vortex generators on the wings and tail surfaces in accordance with the provisions of AML SA00097SE.

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 model aircraft listed above only. This approval should not be extended to aircraft of these models on which other previously approved modifications are incorporated unless it is determined by the installer 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: May 4, 1994 Date reissued:

Date of issuance: June 9, 1994 Date amended: August 20, 2004

(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
The New Piper Aircraft Inc.PA-201A4
The New Piper Aircraft Inc.PA-20-\"115\"1A4
The New Piper Aircraft Inc.PA-20-\"135\"1A4
The New Piper Aircraft Inc.PA-20S1A4
The New Piper Aircraft Inc.PA-20S-\"115\"1A4
The New Piper Aircraft Inc.PA-20S-\"135\"1A4
The New Piper Aircraft Inc.PA-221A6
The New Piper Aircraft Inc.PA-22-1351A6
The New Piper Aircraft Inc.PA-22-1501A6
The New Piper Aircraft Inc.PA-22-1601A6
The New Piper Aircraft Inc.PA-22S-1351A6
The New Piper Aircraft Inc.PA-22S-1501A6
The New Piper Aircraft Inc.PA-22S-1601A6