# STC SA2053WE

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Consulting Aerospace Engineers Inc, United States
- Description: An adjustable lateral trim capability through spring bungee control of aileron per Strato Engineering Company.
- Status date: May 23, 1973
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A19](https://openairdocs.org/tcds/3A19)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/094C7159731C0A9C85256CC10083D5AA.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA2053WE

## ADs that name it (0)

None.

## Approved models (6)

- The Cessna Aircraft Company 150 ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- The Cessna Aircraft Company 150A ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- The Cessna Aircraft Company 150B ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- The Cessna Aircraft Company 150C ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- The Cessna Aircraft Company 150D ([TCDS 3A19](https://openairdocs.org/tcds/3A19))
- The Cessna Aircraft Company 150E ([TCDS 3A19](https://openairdocs.org/tcds/3A19))

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