# STC SA01220WI

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of hydraulically controlled variable pitch 3 blade MTV-12-B/183-17 propeller.
- Applied: September 20, 2002
- Status date: April 5, 2004
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A12](https://openairdocs.org/tcds/3A12), [TCDS A4EU](https://openairdocs.org/tcds/A4EU)
- Certificate PDF: https://openairdocs.org/files/sha256/b4/72/b472da313ffbc0d2641cf6de2ef473eb440de4d894e80f33cb1809893e4e5f3a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E00778F0CE9A6CEB862576D9007BFFAF.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA01220WI

## ADs that name it (0)

None.

## Approved models (17)

- Cessna Aircraft Company 172D ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172E ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172F ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172K ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172L ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172M ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172N ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company 172P ([TCDS 3A12](https://openairdocs.org/tcds/3A12))
- Cessna Aircraft Company F172D ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172F ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172G ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172H ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172K ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172L ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172M ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172N ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172P ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMHORT Number: SA01220W1 This certificate issued to: MT-Propeller Entwicklung GmbH Flugplatzstr. 1 94348 Atting, Germany Purt 3 of the Civil Air Porgulations.

Original Product - - Type Certificate Number: 3A12; A4EU Abale: Cessna; Reims Aviation SA Model: Cessna Models: 172D; 172E; 172F (USAF T -41A); 172K; 172L ; 172M ;

Installation of the hydraulically controlled variable pitch 3 blade MTV-12-B/183-17 propeller. Data Required: (1) MT-Propeller Entwicklung GmbH Operation and Installation Manual ATA 61-01-24 (E-124), Issue 26, dated November 29, 2001, stamped FAA Approved December 30, 2003, or later FAA Approved revisions; (2) MT-Propeller Entwicklung GmbH FAA Approved Airplane Flight Manual Supplement dated January 8, 2004, or later FAA Approved revisions.

Limitations and Conditions: Compatibility of this design change with previously approved modifications must be determined by the installer.

If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

Date of Application: September 20, 2002 Dutc reissed:

Date of Issuance: April 05, 2004 Date Amended:

FEDERAL AVIATION By Direction of the Administrator (Signature) Todd Dixon TOMNISTRATO Program Manager Wichita Aircraft Certification Office (Title)

FAA FORM 8110-2110-681 FAGE 1 of 3 PAGES

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) JAHORE Number: SA01220W Date of Issuance: April 5, 2004 Abodel (Continued):

Cessna Models (continued) 172N; 172P Reims Aviation S.A. Models: F172 D; F172F; F172G; F172H; F172K; F172L; F172M; F172N; F172P Limitations and Conditions: (Continued):

Aircraft to be modified must be equipped with the Lycoming O-360-A1A, -AID or -AIF6 engine.

This STC is not to be transferred since its issuance was in accordance with 14 CFR 21.29 and based upon a validation of the German LBA EMZ No. SA 0706.

***END***

47.

## Every issue (1)

- April 5, 2004: Issued, Current. [certificate](https://openairdocs.org/files/sha256/b4/72/b472da313ffbc0d2641cf6de2ef473eb440de4d894e80f33cb1809893e4e5f3a)

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