# STC SA4443NM

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: LASAR Inc., United States
- Description: Installation of gap seals and speed fairings involving 10 kits.
- Applied: February 28, 2020
- 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/ca/fc/cafc02a2da1ae3fbd5d1bc9b6d911bf0bb6324ab231067352a9547ad6cac16d4
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186307435220240221164833.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA4443NM

## ADs that name it (0)

None.

## Approved models (8)

- Mooney Aircraft Corporation M20B ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- 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))
- Mooney Aircraft Corporation M20F ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20G ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20J ([TCDS 2A3](https://openairdocs.org/tcds/2A3))
- Mooney Aircraft Corporation M20K ([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 SA4443NM

FAA Form 8110-2 (03/21) 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 M20B, M20C, M20D, M20E, M20F, M20G, M20J, M20K

Description of Type Design Change : Installation of gap seals and speed fairings in accordance with the FAA Approved Reports listed on Page 3 dated as shown or later FAA approved revisions.

Limitations and Conditions: The approval of this change in type design applies to the basic aircraft of the specified models that are otherwise unmodified. 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 another person to use this certifica te to alter the product, the holder shall give the other person written evidence of that permission.

Date of application : November 26, 1981 Date of issuance : July 9, 1982

Date reissued : February 28, 2020; January 29, 2024

(Signature) For Gregory S. DiLibero Manager, West Certification Branch Compliance and Airworthiness Division Aircraft Certification

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA4443NM

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/ca/fc/cafc02a2da1ae3fbd5d1bc9b6d911bf0bb6324ab231067352a9547ad6cac16d4)
- February 28, 2020: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/00/0a/000af296adae0d098c181719fea75f7cf8cbd53be212c8077e3e77e1e5b37a65)

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