# STC SA03542NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of the Model MTV-27-1-E-C-F-R(P)/CFR203-58d 5-bladed constant speed, full-feathering, and reversing propellers
- Applied: November 14, 2014
- Status date: June 18, 2015
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 36
- Data sheets: [TCDS A25SO](https://openairdocs.org/tcds/A25SO)
- Certificate PDF: https://openairdocs.org/files/sha256/92/5a/925a95119145c4406756ca9af393e29716f33504f43eb8099bfe7c2d8a1c7814
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C11621106B114DC486257F6C00587264.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03542NY

## ADs that name it (0)

None.

## Approved models (2)

- Piper Aircraft Inc. PA-46-310P ([TCDS A25SO](https://openairdocs.org/tcds/A25SO))
- Piper Aircraft Inc. PA-46-350P ([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.

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA03542NY MT- Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Federal Aviation Regulations.

1. Installation of the Model MTV-27-1-E-C-F-R(P)/CFR203-58d 5-bladed constant speed, full-feathering, and reversing propellers in accordance with MT-Propeller documents “Master Operation Manual List,” Doc. No. E-2448, Revision 0, dated June 26, 2014 or later EASA approved revisions, and “Installation Instructions,” Doc. No. E-2450, Revision 0, dated June 26, 2014 or later EASA approved revisions.

2. The following MT-Propeller documents are required with this installation: EASA approved “Airplane Flight Manual Supplement,” Doc. No. E-2449, Revision 0 dated June 26, 2014 or later EASA approved revisions, and “Instructions for Continued Airworthiness,” Doc. No. E-2451, Revision 0, dated June 26, 2014 or later EASA accepted revisions.

1. This STC is only valid for Piper PA-46-310P and PA-46-350P aircraft modified by FAA STC No. ST00541SE which installs the Pratt and Whitney turbine engine model PT6A-21, PT6A-34, or PT6A-35.

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

3. 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.

Gaetano Sciortino Manager New York Aircraft Certification Office Piper Aircraft, Inc.

PA-46-310P and PA-46-350P November 14, 2014 June 18, 2015 IMPORT A25SO 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA03542NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date: June 18, 2015 Certification Basis:

Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for changes that are not significant in FAA Order 8110.48, the certification basis for this modification are as follows:

a. The type certification basis for the Piper Aircraft, Inc. models PA-46-310P and PA-46-350P aircraft is shown on TCDS No. A25SO for parts not changed or not affected by the change.

b. The type certification basis for the Piper Aircraft, Inc. models PA-46-310P and PA-46-350P aircraft is shown on TCDS No. A25SO for parts changed or affected by the change with the following 14 CFR exceptions

14 CFR Part 36 Amendment 36-28

----------END---------- SA03542NY

## Every issue (1)

- June 18, 2015: Issued, Current. [certificate](https://openairdocs.org/files/sha256/92/5a/925a95119145c4406756ca9af393e29716f33504f43eb8099bfe7c2d8a1c7814)

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