STC SA03775NY

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 SA03775NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Federal Aviation Regulations.

1. The installation of MT-Propeller Entwicklung GmbH's Model# MTV-14-D/195-30b 4-Blade constant speed propeller and spinner on Piper Aircraft, Inc. Model PA-46-310P aircraft or aircraft with TCM TSIO-550-C engine installed via SA00380AT in accordance with the configuration stated in the Master Operation Manual List, Doc. No. E-1967, Rev. 2, dated March 08, 2016, or later EASA approved revision and Installation Instructions, Doc. No. E-1969, Rev. 0, dated December 06, 2010, or later EASA approved revision.

(See Description of Type Design Change Continued on Page 3 of 3)

1. The aircraft must be operated in accordance with the “Limitations” section of Airplane Flight Manual Supplement, Doc. No E-1968 Rev. 1, dated March 08, 2016. or E-1968-1, Rev. 1, dated March 08, 2016 or later EASA accepted revisions.3

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 the certificate to alter the product, the holder must give the other person written evidence of that permission.

Raymond H. Reinhardt Acting Manager New York Aircraft Certification Office Piper Aircraft, Inc.

PA-46-310P November 18, 2013 July 28, 2016 IMPORT A25SO 3

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):

3 SA03775NY

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

3 Date of Issuance: July 28, 2016

Description of Type Design Change (continued):

2. Operation must be in accordance with Aircraft Flight Manual Supplement, Doc. No Doc. No E-1968,Rev. 1, dated March 08, 2016 or E-1968-1, Rev. 1, dated March 08, 2016, or later EASA accepted revisions, and is required as part of this installation.

3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No. E-1970, Rev. 0, dated December 06, 2010, or later EASA accepted revision.

Certification Basis:

Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48, the certification basis for this modification to the Piper Aircraft PA-46-310P aircraft is as follows:

a) The type certification basis for the Piper Aircraft PA-46-310P aircraft as shown on TCDS A25SO for parts not changed or not affected by the change.

b) The type certification basis for the Piper Aircraft PA-46-310P aircraft as shown on TCDS A25SO for parts changed or affected by the change with the following exceptions:

● Compliance with 14 CFR Part 36 at Amendment 36-30.

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