STC SA00037IB

IMPORT SA00037IB MT- Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting Part 23 Title 14 Code of Federal Aviation Regulations A7SO PIPER AIRCRAFT INC.

PA-34-200

1. Installation of the Model MTV-12-B-C-F/CF(L)183-59, 3- blade hydraulically actuated, full feathering, constant speed propeller on Piper Aircraft PA-34-200 Series in accordance with MT- Propeller Master drawing list, Doc No. E-3549 Rev 5, dated May 18, 2022 or later EASA approved revisions.

(Description of Type Design Change continued on page 3 of 4)

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

(Limitations and Conditions continued on page 3 of 4) June 16, 2021 June 9, 2022 Anthony E. Gallo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 4

IMPORT SA00037IB 4

IMPORT SA00037IB Date Issued: June 9, 2022

Description of Type Design Change: (continued from page 1 of 4)

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

E-3551 Rev 2, dated May 18, 2022 or later EASA approved revisions.

3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No. E-3552 Rev 1, dated April 13, 2022 or later EASA approved revisions.

Limitations and Conditions: (continued from page 1 of 4)

2. The EASA approved Airworthiness Limitations section of the Instructions for Continued Airworthiness referenced in the Description of the Type Design Section of this STC is mandatory.

3. The aircraft must be operated in accordance with the Operation Limitations section of the Airplane Flight manual Supplement Referenced in the Description of Type Design section of this STC.

4. This STC is applicable to all serial numbers for this PA-34-200.

IMPORT SA00037IB Date Issued: June 9, 2022 Certification Basis:

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

a. The Type Certification basis for the Piper Aircraft Inc., model PA-34-200 is shown on TCDS A7SO for parts not changed or not affected by the change.

b. The Type Certification basis for the Piper Aircraft Inc., model PA-34-200 is shown on TCDS A7SO for parts changed or affected by the change with the following 14 CFR exceptions:

Section 36 Amendment 36-31

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