# STC SA3541NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: LASAR Inc., United States - Description: Installation of fiberglass belly fairing - Applied: June 10, 1986 - Status date: January 29, 2024 - Product: Aircraft, Small Airplane - Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3) - Certificate PDF: https://openairdocs.org/files/sha256/f0/2b/f02b1529987a31dc91f4b43fabc9174f000108ca8628fb01d1f4896d0118409c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117269744820240221161232.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA3541NM ## ADs that name it (0) None. ## Approved models (3) - Mooney Aircraft Corporation M20C ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) - Mooney Aircraft Corporation M20D ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) - Mooney Aircraft Corporation M20E ([TCDS 2A3](https://openairdocs.org/tcds/2A3)) ## 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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA3541NM Mm FAA Form 8110-2 (3/21) SUPERSEDES PREVIOUS EDITION Page 1 of 2 This Certificate issued to LASAR, Inc. 4439 SW Airport Way Prineville, Oregon 97754 Part 3* of the Civil Air Regulations. *Effective November 1, 1949, as amended, to May 18, 1954. Original Product - Type Certificate Number : 2A3 Make : Mooney M20C, M20D, M20E Description of Type Design Change: Installation of fiberglass belly fairing in accordance with FAA Approved Lake Aero Styling and Repair Drawing List Report No. 129B”NC” dated May 14, 1986, or later FAA approved revisions. Part manufactured in accordance with Lake Aero Styling and Repair Drawing L129 -310322, Rev. A, dated January 1, 1986, or later FAA approved revisions. Limitations and Conditions: This approval should not be extended to other aircraft of these models on which other previously modifications are incorporated unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect on the airworthiness of those aircraft. If the holder agrees to permit a nother person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission. Date of application : June 10, 1986 Date of issuance : September 24, 1987 Date reissued : February 28, 2020; January 29, 2024 (Signature) For Gregory S. DiLibero Manager, West Certification Branch, AIR-770 Compliance and Airworthiness Division Aircraft Certification Service FAA Form 8110-2 (03/21) SUPERSEDES PREVIOUS EDITION Page 2 of 2 ## Every issue (2) - January 29, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f0/2b/f02b1529987a31dc91f4b43fabc9174f000108ca8628fb01d1f4896d0118409c) - February 28, 2020: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/1a/d9/1ad9791ad0eb778e0be0b7be5af5cb4a27387633ddc480e69e927a9dbc12f014) --- 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.