# STC SA5134SWD

- Type: Supplemental type certificate
- Status: Current, Amended
- Holder: S-TEC Corporation, United States
- Description: S-TEC System 60 pitch stabilization system ST-049 with optional automatic electric trim.
- Status date: August 28, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 2A3](https://openairdocs.org/tcds/2A3)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1888B1617BC2987485256CC2001226E1.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5134SWD

## ADs that name it (0)

None.

## Approved models (3)

- 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))

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