STC SA12421IB

Supplemental type certificate · MT-Propeller Entwicklung GmbH

Holder
MT-Propeller Entwicklung GmbH · Germany
Status
Current · Issued
Applied
January 28, 2026
Product
Aircraft · Small Airplane
Data sheet
TCDS2A3
Foreign approvals
EASA STC 10088863 12/11/2025

From FAA DRS, with our copy of the certificate PDF. DRS record last changed July 1, 2026.

What it approves

Installation of the MT-Propeller Entwicklung GmbH MTV-12-B/180-59() propeller

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

IMPORT SA12421IB MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting Germany Part 3 Civil Air Regulations 2A3 Mooney International Corporation

M20A, M20B, M20C, M20D

1. Installation of the MT-Propeller Entwicklung GmbH MTV-12-B/180-59() propeller on the Mooney International Corporation M20A, M20B, M20C, and M20D aircraft must be done in accordance with the MT-Propeller Entwicklung GmbH Master Documentation List (MDL), Doc. # E-4154 Revision 4, dated April 27, 2026, or later European Union Aviation Safety Agency (EASA) accepted revsions, and the Installation Instructions, Doc # E-4157, Revision 2, dated April 27, 2026, or later EASA accepted revisions.

1. This Supplemental Type Certificate (STC) is applicable to all serial numbers for this Make-Model.

(See continuation sheet 3) January 28, 2026 June 30, 2026 John Yoo Manager, International Validation Branch Compliance & Airworthiness Division Aircraft Certification Service 3

IMPORT SA12421IB 3

IMPORT SA12421IB Date Issued: June 30, 2026

Description of Type Design Change (continued):

2. Maintenance must be in accordance with the MT-Propeller Entwicklung GmbH Instructions for Continued Airworthiness, Doc. # E-4158, Revision 2, dated April 14, 2026, or later EASA accepted revisions.

3. Operations must be in accordance with the MT-Propeller Entwicklung GmbH Supplement Airplane Flight Manual, # E-4156, Revision 0, dated May 26, 2025, or later EASA approved revisions.

2. The aircraft must be operated in accordance with the Limitations section of the Supplement Airplane Flight Manual referenced in the Description section.

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 Title 14 Code of Federal Regulations (CFR) 21.115 and 21.101, and the Federal Aviation Administration (FAA) policy for design changes that are identified as not significant in FAA Order 8110.48, the type certification basis for the modified Mooney International Corporation M20A, M20B, M20C, and M20D is as follows:

a. The type certification basis for the Mooney International Corporation M20A, M20B, M20C, and M20D is as shown on Type Certification Data Sheet (TCDS) 2A3 for areas not changed or not affected by the change.

b. The type certification basis for the Mooney International Corporation M20A, M20B, M20C, and M20D for areas changed or affected by the change is as shown on TCDS 2A3 with the following exceptions:

• 14 CFR Part 36 at Amendment 36-32.

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ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 4

MakeModelData sheet
Mooney International CorporationM20A2A3
Mooney International CorporationM20B2A3
Mooney International CorporationM20C2A3
Mooney International CorporationM20D2A3