STC SA5131NM

Supplemental type certificate · Micro AeroDynamics Inc

Holder
Micro AeroDynamics Inc · United States
Status
Current · Amended
Status date
January 7, 2008
Applied
October 8, 1990
Product
Aircraft · Small Multi-Engine
Certification basis
Part 3, Part 21
Data sheet
TCDSA7CE

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Install vortex genertors on the wing and vertical tail surfaces and an increase in maximum takeoff weight, maximum zero fuel weight, and maximum ramp weight.

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 SA5131NM 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: A7CE Make: Cessna Model: 402C and 414A*

Description of the Type Design Change: Install vortex generators on the wing and vertical tail surfaces and an increase in maximum takeoff weight, maximum zero fuel weight, and maximum ramp weight in accordance with Drawing List DL-402C and Installation Instructions II-402C, both revised July 24, 1992, or later FAA-approved revision.

Option: 1: No change in airspeeds; AFMS not requi red; no change in weights or center of gravity envelope.

Option 2: Change in airspeeds, maximum takeoff weight, zero fuel weight, ramp weight, center of gravity envelope; AFMS required.

*Includes 414A equipped with RAM engine and winglet installations per SA7463SW and SA4934SW, respectively.

Limitations and Conditions: Approval of this change in type design applies to the above aircraft only. The 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 and FAA Approved Flight Manual Supplement (option 2 only) C402C-AFMS-1, Revision B for the 402C, and C414A-AFMS-1, Revision B, for the 414A, both dated August 19, 1996, must be maintained as part of the permanent records for the modified aircraft.

Date of application: October 8, 1990 Date reissued:

Date of issuance: March 4, 1991 Date amended: September 2, 1992; August 23, 1996;

January 7, 2008

(Signature) Acting Manager, Seattle Aircraft Certif nicatio 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 · 2

MakeModelData sheet
The Cessna Aircraft Company402CA7CE
The Cessna Aircraft Company414AA7CE