# STC SA04450NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of MTV-27-1-E-C-F-R(P)/CFR240-55() propeller and spinner
- Applied: June 27, 2019
- Status date: July 20, 2020
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A00007SE](https://openairdocs.org/tcds/A00007SE)
- Certificate PDF: https://openairdocs.org/files/sha256/e5/e5/e5e53e6ddd7a8e357bd88e2d102c6f67b45b3ab9fc459f6a214995fbc02a134d
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B490FB12477E282F862585D90060A129.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA04450NY

## ADs that name it (0)

None.

## Approved models (1)

- Daher Aircraft Design LLC Kodiak 100 ([TCDS A00007SE](https://openairdocs.org/tcds/A00007SE))

## 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 The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 1 of This certificate issued to:

Part of the Original Product – Type Certificate Number: Make:

By Direction of the Administrator Signature Title SA04450NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Federal Aviation Regulations.23

1. Installation of MTV-27-1-E-C-F-R(P)/CFR240-55() propeller and spinner in accordance with MT-Propeller Entwicklung GmbH Master Documentation List No. E-3113, Revision 4, dated July 16, 2020or later EASA approved revisions.

2. Aircraft operation in accordance with MT-Propeller Entwicklung GmbH Airplane Flight Manual Supplement documentation No. E-3115, Revision 0, dated February 11, 2019, or later EASA approved revisions.

3. Maintenance in accordance with MT-Propeller Entwicklung GmbH Instructions for Continued Airworthiness documentation No. E-3117, Revision 1, dated February 06, 2020 or later EASA accepted revisions.

1. The installer must determine whether this design change is compatible with previously approved modifications.

2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Timothy J. Hadsall Acting Manager, New York ACO Branch C li d Ai hi Di i i Daher Aircraft Design LLC Kodiak 100 June 27, 2019 July 20, 2020 IMPORT A00007SE 2

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate The STC’s supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property oft h eS T C holder.

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement):

2 SA04450NY

## Every issue (1)

- July 20, 2020: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e5/e5/e5e53e6ddd7a8e357bd88e2d102c6f67b45b3ab9fc459f6a214995fbc02a134d)

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