STC SA03637NY

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

Part of the

Signature

Title SA03637NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Federal Aviation Regulations.

1. The installation of MT-Propeller Entwicklung GmbH's 4-Blade Model# MTV-14-B / 195-30b propellers and spinners containing Lycoming TIO-540-AE2A model engines or turbo-supercharged variance of Lycoming's TIO-540-AEA model engine in accordance with the configuration stated in the Master Operation Manual List, Doc. No. E-2030, November 17, 2015, Rev. 2 or later EASA approved revision and Installation Instructions, Doc. No. E-2031, December 6, 2010, Rev. 0 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 “Limitation” section of MT-Propeller Entwicklung GmbH Airplane Flight Manual Supplement, Doc. No E-2029 & E-2029-1, November 17, 2015, Rev. 1 or later EASA accepted revision, and is required for this installation.

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

PA-46-350P & PA-46R-350T November 18, 2013 December 15, 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 SA03637NY

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

3 Date of issuance: December 15, 2015

Description of Type Design Change (continued):

2. Operation must be in accordance with Aircraft Flight Manual Supplement, Doc. No E-2029 & E-2029-1, November 17, 2015, Rev. 1 or later EASA accepted revision, and is required for this installation.

3. Maintenance must be in accordance with Instruction for Continued Airworthiness, Doc. No. E-2032, December 6, 2010, Rev. 0 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 PA-46-350P & PA-46R-350T aircraft is as follows:

a) The type certification basis for the Piper PA-46-350P & PA-46R-350T aircraft as shown on TCDS A25SO for pasts not changed or not affected by the change.

b) The type certification basis for the Piper PA-46-350P & PA-46R-350T aircraft as shown on TCDS A25SO for pasts changed or affected by the change with the following exceptions:

o Compliance with 14 CFR §23.1529 at Amendment 23-26.

o Compliance with 14 CFR §23.53, 23.55, 23.57, 23.59, 23.61, 23.721, 23.803, & 23.815 at Amendment 23-34.

o Compliance with 14 CFR §23.811, 23.813 at Amendment 23-36.

o Compliance with 14 CFR §23.831 at Amendment 23-42.

o Compliance with 14 CFR §23.905 & 23.934 at Amendment 23-43.

o Compliance with 14 CFR §23.251, 23.305, 23.397, 23.573, 23.672, 23.773, 23.851, 23.1507, & 23.1549 at Amendment 23-45.

o Compliance with 14 CFR §23.805 & 23.812, at Amendment 23-46.

o Compliance with 14 CFR §23.301, 23.337, 23.341, 23.393, 23.571, 23.574, & 23.575, at Amendment 23-48.

o Compliance with 14 CFR §23.677, 23.691, 23.703, 23.745, 23.775, 23.783, 23.791, 23.841, 23.853, 23.855, &

23.867 at Amendment 23-49.

o Compliance with 14 CFR §23.63, 23.66, 23.69, 23.71, 23.73, 23.237, 23.1543, 23.1545, 23.1555, 23.1559,

23.1581, 23.1583, & 23.1585 at Amendment 23-50.

o Compliance with 14 CFR §23.777 at Amendment 23-51.

o Compliance with 14 CFR §23.907 at Amendment 23-59.

o Compliance with 14 CFR part 36 at Amendment 36-28.

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