# STC SA01511SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: MT- Propeller Entwicklung GmbH, Germany - Description: Installation of MTV-14-B propellers - Applied: October 19, 2004 - Status date: February 18, 2005 - Product: Aircraft, Single-Engine - Certification basis: Part 21, Part 23 - Data sheets: [TCDS A17WE](https://openairdocs.org/tcds/A17WE) - Certificate PDF: https://openairdocs.org/files/sha256/81/28/81288cafeab729a509b5102b2ca44d1726771682364278187c556939ff62681c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B0FDA34F7560C05E8625770A005CD417.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA01511SE ## ADs that name it (0) None. ## Approved models (4) - Aerostar Aircraft Corporation PA-60-600 (Aerostar 600) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-601 (Aerostar 601) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-601P (Aerostar 601P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) - Aerostar Aircraft Corporation PA-60-602P (Aerostar 602P) ([TCDS A17WE](https://openairdocs.org/tcds/A17WE)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. Number SA01511SE This certificate, issued to MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting G e r m a n y Part 23 of the Federal Aviation Regulations. Original Product⎯Type Certificate Number: A17WE Make: Aerostar Model: PA-60-600, -601, -601P, -602P Description of the Type Design Change: Installation of MTV-14-B propellers as listed under Limitations and Conditions on Continuation Sheet, Page 3. Limitations and Conditions: Incorporation of this modification requires the prior or concurrent incorporation of Machen Inc. STC SA1658NM. Approval of this change in type design applies to the above models only. This approval should not be extended to aircraft of these models on which other previously approved modifications are incorporated unless it is determined that the relationships between this change and any of those other previously approved modifications including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate SA01511SE and the applicable FAA approved Airplane Flight Manual Supplement shall be maintained as part of the permanent records for the modified aircraft. 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. (See Continuation Sheets Page 3) Date of application: October 19, 2004 Date reissued: Date of issuance: February 18, 2005 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) United States of America Department of Transportation_Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number SA01511SE MT-Propeller Entwicklung GmbH Reissued: Amended: Limitations and Conditions: (cont’d) MODEL ENGINES PROPELLERS AFMS *** INSTALLATION **INSTRUCTIONS** **INSTRUCTIONS FOR** **CONTINUED** AIRWORTHINESS 650 PA-60-600 PA-60-601 IO-540-S1A5-MM* (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 650 PA-60-601P PA-60-602P IO-540-S1A5-MM* OR IO-540-AA1A5-MM* (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 680 PA-60-600 PA-60-601 IO-540-S1A5-MM* OR IO-540-AA1A5-MM* (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 680 PA-60-601P PA-60-602P IO-540-S1A5-MM* OR IO-540-AA1A5-MM* (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 680 PA-60-601P PA-60-602P IO-540-S1A5-MM* OR IO-540-AA1A5-MM* (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 700 PA-60-601P PA-60-602P IO-540-S1A5-MM* OR IO-540-AA1A5-MM* (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 700A PA-60-600 PA-60-601 TIO-540-U2A (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 700A PA-60-601P PA-60-602P TIO-540-U2A (2 EA) MTV-14-B-C-F/CF188-30d E-1106 Dated February 18, 2005 E-1108 Dated October 19, 2004 E-1108 Dated October 19, 2004 700CR PA-60-600 PA-60-601 **ONE EACH TIO-540-U2A LTIO-540-U2A** ONE EACH MTV-14-B-C-F/CF188-30d and one each MTV-14-B-C-F/CFL188-30d E-1107 Dated February 18, 2005 E-1109 Dated October 19, 2004 E-1109 Dated October 19, 2004 700CR PA-60-601P PA-60-602P **ONE EACH TIO-540-U2A LTIO-540-U2A** ONE EACH MTV-14-B-C-F/CF188-30d and one each MTV-14-B-C-F/CFL188-30d E-1107 Dated February 18, 2005 E-1109 Dated October 19, 2004 E-1109 Dated October 19, 2004 **FAA FORM 8110-2- 1 (10-69) PAGE 3 OF 3 PAGES** ## Every issue (1) - February 18, 2005: Issued, Current. [certificate](https://openairdocs.org/files/sha256/81/28/81288cafeab729a509b5102b2ca44d1726771682364278187c556939ff62681c) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.