STC SA02098SE

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Issued
Status date
December 15, 2010
Applied
October 8, 2010
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDS3A20

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 and strakes on the engine nacelles.

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 Oppe Certificate Number: SA02098SE 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: 3A20 Make: Hawker Beechcraft Model: 65-90, 65-A90, 65-A90-1, U-21A, RU-21A, RU-21D, JU-21A, U-21G, RU-21H, 65-A90-2, RU-21B, 65-A90-3, RU-21C, 65-A90-4, RU-21E, B90, C90, C90A, C90GT, C90GTI, E90, H90, T-44A Description of Type Design Change: Installation of vortex generators on the wings and tail surfaces and strakes on the engine nacelles in accordance with Micro AeroDynamics Drawing Package MA2236, Revision IR, dated October 06, 2010, Installation Manual MA2237, Revision IR, dated December 01, 2010, and Instructions for Continued Airworthiness MA0666, Revision A, or later FAA-approved revision.

NOTE: If more than five vortex generators, or either nacelle strake, 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 effect upon the airworthiness of that aircraft. This STC has been found to be compatible with STC SA10747SC dated October 06, 2009.

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 08, 2010 Date Reissued:

Date of Issuance: December 15, 2010 Date Amended:

FEDERAL AVIATION By Direction of the Administrator TOMNIST RATION OLEU (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
Hawker Beechcraft Corporation65-903A20
Hawker Beechcraft Corporation65-A903A20
Hawker Beechcraft Corporation65-A90-13A20
Hawker Beechcraft Corporation65-A90-23A20
Hawker Beechcraft Corporation65-A90-33A20
Hawker Beechcraft Corporation65-A90-43A20
Hawker Beechcraft CorporationB903A20
Hawker Beechcraft CorporationC903A20
Hawker Beechcraft CorporationC90A3A20
Hawker Beechcraft CorporationC90GT3A20
Hawker Beechcraft CorporationC90GTi3A20
Hawker Beechcraft CorporationE903A20
Hawker Beechcraft CorporationH903A20