# STC SA12438IB

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT-Propeller Entwicklung GmbH, Germany
- Description: MT-Propeller Entwicklung MTV-37-1-E-C-F-R(P)/CFR205-353( )
- Applied: March 30, 2026
- Status date: July 14, 2026
- Product: Aircraft, Small Airplane
- Certification basis: Part 23
- Foreign approvals: EASA STC 10089486
- Data sheets: [TCDS A25SO](https://openairdocs.org/tcds/A25SO)
- Certificate PDF: https://openairdocs.org/files/sha256/55/bd/55bd1ac66aba0cdb1a4102bfd9fe1ffe1528c0d956cb759d69fcf8ae73299182
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID121403571120260715145251.0001
- DRS record last changed: July 15, 2026
- Page: https://openairdocs.org/stc/SA12438IB

## ADs that name it (0)

None.

## Approved models (2)

- Piper Aircraft Inc. PA-46-600TP ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Piper Aircraft Inc. PA-46-701TP ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))

## 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.

IMPORT SA12438IB MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting Germany Part 23 Title 14 Code of Federal Regulations A25SO Piper Aircraft Inc.

PA-46-600TP, PA-46-701TP

1. This Supplemental Type Certificate (STC) is applicable to all serial numbers of these models.

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

(See continuation sheet 3) 03/30/2026 07/14/2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

1. MT-Propeller Entwicklung MTV-37-1-E-C-F-R(P)/CFR205-353( ) propeller manufactuered in accordance with the MT-Propeller Master Documentation List E-4504, Revision 0, dated February 11, 2026, or later European Union Aviation Safety Agency (EASA) accepted revision; and installed in accordance with Installation Instructions E-4507, Revision 1, dated March 19, 2026 ,or later EASA-accepted revision.

Description of Type Design Change (continued):

2. Maintained in accordance with the MT-Propeller Instructions for Continued Airworthiness (ICA) E-4508, Revision 0, dated February 11, 2026, or later EASA accepted revision.

3. Operated in accordance with the MT-Propeller Airplane Flight Manual Supplement (AFMS) E-4506, Revision 0, dated February 11, 2026, or later EASA approved revisions.

3. The aircraft must be operated in accordance with the Limitations section of the AFMS referenced in the Description section.

4. The aircraft must be maintained in accordance with the Limitations section of the ICA referenced in the Description section.

5. 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.

Certification Basis:

The certification basis for the modified Piper Aircraft Inc. PA-46-600TP and PA-46-701TP is as shown on TCDS A25SO plus Part 36 at Amendment 36-32

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## Every issue (1)

- July 14, 2026: Issued, Current. [certificate](https://openairdocs.org/files/sha256/55/bd/55bd1ac66aba0cdb1a4102bfd9fe1ffe1528c0d956cb759d69fcf8ae73299182)

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