STC SA04472NY

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IMPORT SA04472NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany 3/23 Civil Air/Federal Aviation Regulations 2A13 Piper Aircraft, Inc.

PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201

1. Installation of MT-Propeller Entwicklung GmbH model MTV-12-B/188-59( ) 3-blade, constant speed propeller and spinner on Piper Aircraft, Inc. PA-28R-180, PA-28R-200, PA-28R-201, and PA-28RT-201 model aircraft equipped with Lycoming IO-360-B or IO-360-C series engine models in accordance with the configuration stated in Master Operational Manual List, Doc. No. E-3493, Rev. 4, dated October 5, 2020 or later EASA approved revision and Installation Instructions, Doc. No. E-3495, Rev. 1, dated March 2, 2020 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-3494, Rev. 4, dated October 5, 2020, or later EASA approved revision.

(See Limitations and Conditions continued on Page 3 of 3) 01/20/2020 10/19/2020 Timothy J. Hadsall Acting Manager, New York ACO Branch Compliance & Airworthiness Division 3

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Date oI transfer:

IMPORT SA04472NY 3

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IMPORT SA04472NY Date of Issuance: October 19, 2020

Description of Type Design Change (continued):

2. Operation must be in accordance with Airplane Flight Manual Supplement, Doc. No.

E-3494, Rev. 4, dated October 5, 2020, or later EASA approved revision, and is required as part of this installation.

3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No. E-3496, Rev. 1, dated March 2, 2020, or later EASA accepted revision, and is required as part of this installation.

2. For the PA-28R-180 model aircraft, this installation approval is limited to aircraft equipped with Lycoming IO-360-B1E engines. For the PA-28R-200 model aircraft, this installation approval is limited to 1180 kg or 1202 kg MTOW configurations.

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

4. 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:

Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48, the certification basis for this modification to Piper Aircraft, Inc. PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201 aircraft is as follows:

a) The type certification basis for the Piper Aircraft, Inc. PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201 aircraft as shown on TCDS 2A13 for parts not changed or not affected by the change.

b) The type certification basis for the Piper Aircraft, Inc. PA-28R-180, PA-28R-200, PA-28R-201, PA-28RT-201 aircraft as shown on TCDS 2A13 for parts changed or affected by the change with the following exceptions:

• Compliance with 14 CFR Part 36 at Amendment 36-31.

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