What it approves
Installation of vortex generators on the wings and vertical tail surfaces of the above model aircraft per Drawing Package MA2081, Revision IR, dated January 15, 2002, and Installation Manual MA2082, Revision IR, dated February 13, 2002, 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 SA01065SE This certificate, issued to Micro AeroDynamics, Inc.
4000 Airport Road, Suite D Anacortes, WA 98221 certifies that the change in the type design for the follo wing product with the limitations and conditions therefor as specified hereon meets the airw orthiness requirements of Part 3 of the Civil Air Regulations.
Original ProductType Certificate Number: 3A19 A13EU Make: Cessna Cessna Model: 150F, 150G, 150H, 150J F150G, F150H, F150J, 150K, 150L, 150M, A150K, F150K, F150L, F150M, A150L, A150M, 152, A152 FA150K, FA150L, F152, FA152
Description of the Type Design Change: Installation of vortex generators on the wings and vertical tail surfaces of the above model aircraft in accordance with Drawing Package MA2081, Revision IR, dated January 15, 2002, and Installation Manual MA2082, Revision IR, dated February 13, 2002, 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 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 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.
This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is ot herwise established by the Administrator of the Federal Aviation Administration.
Date of application: January 18, 2002 Date reissued:
Date of issuance: March 18, 2002 Date amended:
(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.
Approved models · 20
| Make | Model | Data sheet |
|---|---|---|
| Reims Aviation S.A. | F150 Series | A13EU |
| Reims Aviation S.A. | F150G | A13EU |
| Reims Aviation S.A. | F150H | A13EU |