# STC SA04067NY - Type: Supplemental type certificate - Status: Current, Issued - Holder: MT- Propeller Entwicklung GmbH, Germany - Description: Installation of MT-Propeller Entwicklung GmbH's Model# MTV-14-D/195-30b 4-Blade constant speed propeller and spinner on Textron Aviation Inc. Model LC41-550FG aircraft - Applied: January 18, 2016 - Status date: March 19, 2018 - Product: Aircraft, Small Airplane - Certification basis: Part 21, Part 36 - Data sheets: [TCDS A00003SE](https://openairdocs.org/tcds/A00003SE) - Certificate PDF: https://openairdocs.org/files/sha256/75/80/758024c579baad0253b08049126112c9416631d19c51a052e92d7f748fa898aa - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/31DB824C491456568625826E004CEEDB.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA04067NY ## ADs that name it (0) None. ## Approved models (1) - Textron Aviation Inc. LC41-550FG ([TCDS A00003SE](https://openairdocs.org/tcds/A00003SE)) ## 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. FAA Form 8110-2 (5/14) Page 1 of Part of the Signature Title SA04067NY MT-Propeller Entwicklung GmbH Flugplatzstrasse 1 94348 Atting, Germany Federal Aviation Regulations. 1. Installation of MT-Propeller Entwicklung GmbH's Model# MTV-14-D/195-30b 4-Blade constant speed propeller and spinner on Textron Aviation Inc. Model LC41-550FG aircraft in accordance with the configuration stated in Master Operational Manual List, Doc. No. E-2201, Rev. 2, dated March 2, 2018 or later EASA approved revision and Installation Instructions, Doc. No. E-2203, Rev. 1, dated November 2, 2016 or later EASA approved revision. (See Description of Type Design Change continued on Page 3 of 3) 1. The aircraft must be operated in accordance with the "Limitations" section of Airplane Flight Manual Supplement, Doc. No. E-2202, Rev. 2, dated March 2, 2018, or later EASA approved revision. 2. The installer must determine whether this design change is compatible with previously approved modifications. 3. 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. Kevin Dickert Acting Manager New York ACO Branch Textron Aviation Inc. LC41-550FG January 18, 2016 March 19, 2018 IMPORT A00003SE 3 FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) 3 SA04067NY FAA Form 8110-2 (5/14) Page 3 of 3 Date of Issuance: March 19, 2018 Description of Type Design Change (continued): 2. Operation must be in accordance with Airplane Flight Manual Supplement, Doc. No. E-2202, Rev. 2, dated March 2, 2018, or later EASA approved revision, and is required as part of this installation. 3. Maintenance must be in accordance with Instructions for Continued Airworthiness, Doc. No. E-2204, Rev. 0, dated July 23, 2012, or later EASA accepted revision, and is required as part of this installation. Certification Basis: Based on 14 CFR §21.115 and §21.101, and FAA Order 8110.48, the certification basis for this modification to Textron Aviation Inc. LC41-550FG aircraft is as follows: a) The type certification basis for the Textron Aviation Inc. LC41-550FG aircraft as shown on TCDS A00003SE for parts not changed or not affected by the change. b) The type certification basis for the Textron Aviation Inc. LC41-550FG aircraft as shown on TCDS A00003SE for parts changed or affected by the change with the following exception: ● Compliance with 14 CFR Part 36 at Amendment 36-30. ----------END---------- SA04067NY ## Every issue (1) - March 19, 2018: Issued, Current. [certificate](https://openairdocs.org/files/sha256/75/80/758024c579baad0253b08049126112c9416631d19c51a052e92d7f748fa898aa) --- 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.