# STC SA01604SE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of the full feathering 5-blade constant speed MTV-5-1-E-C-F/CF220-54 propeller installed and maintained.
- Applied: July 4, 2005
- Status date: September 29, 2005
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 27
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/db/84/db84945b225b78ac8355df94879e5ab18159790f44dfd52ad45dbfd3967efbe9
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/159BE0324279B1968625709900541E12.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01604SE

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- The Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate Number SA01604SE This certificate, issued to: MT-Propeller Entwicklung GmbH Flugplatzstr.1 94348 Atting Germany

Part 27 of the Federal Aviation Regulations.

Original Product⎯Type Certificate Number: A4CE Make: Cessna Aircraft Company Model: U206G, TU206G

Description of the Type Design Change: Installation of the full feathering 5-blade constant speed MTV-5-1- E-C-F/CF220-54 propeller installed and maintained in accordance with Installation Instruction and Instructions for Continued Airworthiness, Doc. No. E-1208, dated July 4, 2005 or installation of the reversing and full feathering 5-blade constant speed MTV-5-1-E-C-F-R(M)/CFR220-54 propeller installed and maintained in accordance with Installation Instruction and Instructions for Continued Airworthiness, Doc. No. E-1206, dated July 4, 2005 on aircraft modified per Soloy STC No. SA2353NM.

Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only that are equipped with Soloy Turbine Pac (STC SA2353NM). This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those 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 the FAA approved Airplane Flight Manual Supplement (AFMS), Doc. No. E-1205, dated September 29, 2005 or AFMS, Doc. No. E-1207, dated September 29, 2005 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: July 4, 2005 Date reissued Date of issuance: September 29, 2005 Date amended:

(Signature)

Acting Manager, Seattle Aircraft Certification Office (Title)

## Every issue (1)

- September 29, 2005: Issued, Current. [certificate](https://openairdocs.org/files/sha256/db/84/db84945b225b78ac8355df94879e5ab18159790f44dfd52ad45dbfd3967efbe9)

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