# STC SA01003SE

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: Micro AeroDynamics Inc, United States
- Description: Addition of performance data to allow reduced RPM rating on takeoff. Incorporation of this rating requires the prior or concurrent incorporation of STC SA00887SE.
- Applied: June 29, 2001
- Status date: February 4, 2011
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/a4/c8/a4c8e118b0441c62f1061aa98839e9495043f5681c1b47f3ac4045fc3ccee64d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/2DC7DBCA7B4AC074862578400079898A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01003SE

## ADs that name it (0)

None.

## Approved models (8)

- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company U206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))

## What the certificate says

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: SA01003SE This certificate issued to: Micro AeroDynamics, Inc.

4000 Airport Road, Suite D Anacortes, WA 98221 Part 3 of the Civil Aviation Regulations.

Original Product - Type Certificate Number: A4CE Make: Cessna Model: U206B, U206C, U206D, U206E, U206F, U206G, 207, 207A Description of Type Design Change: Addition of performance data to allow reduced RPM rating on takoff. Incorporation of this rating requires the prior or concurrent incorporation of STC SA00887SE.

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 and Airplane Flight Manual Supplement, dated February 7, 2011, or later FAA-approved revision, 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: June 29, 2001 Date Reissued:

Date of Issuance: October 9, 2001 Date Amended: February 7, 2011 FEDERAL AVIATION By Direction of the Administrator

(Signature) HOMINIS Y RATION Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- February 4, 2011: Amended, Current. [certificate](https://openairdocs.org/files/sha256/a4/c8/a4c8e118b0441c62f1061aa98839e9495043f5681c1b47f3ac4045fc3ccee64d)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.