What it approves
Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA01215SE 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 following product with the limitations and conditions therefor as specified hereon meets the airworthiness requivements of Part * of the * Regulations.
Original Product - Type Certificate Number: *See attached FAA Approved Model List (AML) Make: No. SA01215SE for a list of approved airplane Model: models and applicable airworthiness regulations.
Description of Type Design Change: Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers in accordance with Micro AeroDynamics Drawing List MA2182, Revision IR, dated March 21, 2003, and Installation Manual MA2183, Revision IR, dated April 15, 2003, or later FAA approved revision to either 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.
Date of Application: March 21, 2003 Date Reissued:
Date of Issuance: May 13, 2003 Date Amended:
FEDERAL By direction the Administrator (Signature) TOMINIST RATION Acting Manager, Seattle Aircraft Certification Office (Title)
FAA APPROVED MODEL LIST NO. SA01215SE MICRO AERODYNAMICS INC.
INSTALLATION OF VORTEX GENERATORS ORIGINAL ISSUE May 13, 2003
ITEM AIRCRAFT AIRCRAFT TYPE CERTIFICATION FAA SEALED INSTALLATION AML
MAKE MODEL CERTIFICATE BASIS DRAWING LIST INSTRUCTIONS, REVISION
NUMBER FOR REVISION AND DATE
ALTERATION NUMBER REV DATE 1 Cessna 336 A2CE CAR 3 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 2 Cessna 337 A6CE CAR 3 MA2182 TR MA2183 Rev IR Original 3/21/03/ 4/15/03 Issue 3 Cessna 337A A6CE CAR 3 MA2182 IR MA2183 Rev IR Original (USAF 02B) 3/21/03 4/15/03/ Issue 4 Cessna 337B A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 5 Cessna M337B A6CE CAR 3 MA2182 IR MA2183 Rev IR Original (USAF 02A) 3/21/03 4/15/03/ Issue 6 Cessna T337B A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03/ 4/15/03/ Issue 7 Cessna 337C A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue Cessna T337C A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03/ 4/15/03 Issue 9 Cessna 337D A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03/ Issue 10 Cessna T337D A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 11 Cessna 337E A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 1 of 3
FAA APPROVED MODEL LIST NO. SA01215SE MICRO AERODYNAMICS INC.
INSTALLATION OF VORTEX GENERATORS ORIGINAL ISSUE May 13, 2003
ITEM AIRCRAFT AIRCRAFT TYPE CERTIFICATION FAA SEALED INSTALLATION AML
MAKE MODEL CERTIFICATE BASIS DRAWING LIST INSTRUCTIONS, REVISION
NUMBER FOR REVISION AND DATE
ALTERATION NUMBER REV DATE 12 Cessna T337E A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03/ 4/15/03 Issue 13 Cessna 337F A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 14 Cessna T337F A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 15 Cessna 337G A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03/ Issue 16 Cessna T337G A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 17 Cessna 337H A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 18 Cessna P337H A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 19 Cessna T337H A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 20 Cessna T337H-SP A6CE FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 21 Cessna F337E A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 2 of 3
FAA APPROVED MODEL LIST NO. SA01215SE MICRO AERODYNAMICS INC.
INSTALLATION OF VORTEX GENERATORS ORIGINAL ISSUE May 13, 2003
ITEM AIRCRAFT AIRCRAFT TYPE CERTIFICATION FAA SEALED INSTALLATION AML
MAKE MODEL CERTIFICATE BASIS DRAWING LIST INSTRUCTIONS, REVISION
NUMBER FOR REVISION AND DATE
ALTERATION NUMBER REV DATE 22 Cessna FT337E A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 23 Cessna F337F A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03/ 4/15/03 Issue 24 Cessna FT337F A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 25 Cessna F337G A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03/ Issue 26 Cessna FT337GP A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03/ 4/15/03 Issue 27 Cessna F337H A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03 Issue 28 Cessna FT337HP A23EU FAR 23 MA2182 IR MA2183 Rev IR Original 3/21/03 4/15/03/ Issue Approved Acting Manager, Seattle Aircraft Certification Office 3 of 3
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 28
| Make | Model | Data sheet |
|---|---|---|
| Cessna Aircraft Company | 336 | A2CE |
| Cessna Aircraft Company | 337 | A6CE |
| Cessna Aircraft Company | 337A | A6CE |