STC SA01299SE

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Issued
Status date
November 14, 2003
Applied
October 1, 2003
Product
Aircraft · Single-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDS1A15

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 Micro AeroDynamics , Inc. Drawing Package Document MA2191, Revision IR, dated September 17, 2003, and Installation Manual MA2192, Revision IR, dated October 27, 2003, or later FAA approved revision to either of these documents.

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 SA01299SE 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: 1A15 Make: Piper Model: PA-24, PA-24-250, PA-24-260

Description of the Type Design Change: Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics , Inc. Drawing Package Document MA2191, Revision IR, dated September 17, 2003, and Installation Manual MA2192, Revision IR, dated October 27, 2003, or later FAA approved revision to 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 other previously approved modifications, including changes in type design, will introduce no adverse effects 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: October 1, 2003 Date reissued:

Date of issuance: November 14, 2003 Date amended:

(Signature) Acting Manager, Seattle Aircraft Certificat ion 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 · 3

MakeModelData sheet
The New Piper Aircraft Inc.PA-241A15
The New Piper Aircraft Inc.PA-24-2501A15
The New Piper Aircraft Inc.PA-24-2601A15