# STC SA00458DE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: MT- Propeller Entwicklung GmbH, Germany
- Description: Installation of a hydraulically controlled variable pitch 3-bladed propeller Model MTV-9-B-C/C203-46.
- Applied: January 15, 2001
- Status date: August 20, 2001
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A8SO](https://openairdocs.org/tcds/A8SO)
- Certificate PDF: https://openairdocs.org/files/sha256/0d/8c/0d8ce18be60b9e98f2e33e94eee252f8b056c4811ba3997d9f395f6781f99fc2
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3EF36DE3C9D80EB885256CC1007DC93A.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA00458DE

## ADs that name it (0)

None.

## Approved models (1)

- Sky International Inc. S-2B ([TCDS A8SO](https://openairdocs.org/tcds/A8SO))

## What the certificate says

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

Department of Transportation Federal Aviation Administration Supplemental Type Certificate IMPORT Number: SA00458DE This certificate issued to: MT- Propeller Entwicklung GmbH Flugplatzstr. 1 94348 Atting - Germany Part 21.29 of the Federal Aviation Regulations.

Original Product - Type Certificate Number. A8SO Make: Sky International, Inc.

Model: Pitts S-2B Description of Type Design Change:

Installation of a hydraulically controlled variable pitch 3-bladed propeller Model MTV-9-B-C/C203-46 in accordance with MT-Propeller Entwicklung GMBH Installation Instruction No. E - 661 -E, dated January 11, 2001 or later FAA approved revision.

1.) Compatibility of this design change with previously approved modifications must be determined by the

2.) A copy of this certificate and FAA approved Airplane Flight Manual Supplement E-662-E, Revision No. 1, dated August 20, 2001 or later FAA approved revision must be maintained as part of the permanent records of

3.) Instructions for Continued Airworthiness will be implemented through Document No. ATA 61-01-24 (E-124), Operation and Installation Manual, Issue 25, dated March 3, 2000 or later FAA approved revision (Issue) and Service Bulletin No. 1W, EB-Nr. I - EC 34, dated March 8, 1999 or later FAA approved revision and is a required part of the permanent records for the modified aircraft, and defines inspection, TBO, and maintenance

4.) 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: January 15, 2001 Date Reissued:

Date of Issuance: August 20, 2001 Date Amended:

FEDERAL By Direction of the Administrator Te Cros David T. Grossman Signature) Rotorcraft Program Manager AOMINISTRATIOT Denver Aircraft Certification Office Northwest Mountain Region, Denver, Colorado (Title)

## Every issue (1)

- August 20, 2001: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0d/8c/0d8ce18be60b9e98f2e33e94eee252f8b056c4811ba3997d9f395f6781f99fc2)

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