# STC SA1351CE

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Engineering Plating & Processing, Inc., United States
- Description: Chrome-plated brake disc installation.
- Status date: August 22, 1977
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A24](https://openairdocs.org/tcds/3A24)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A3A3B11A7215513685256CC100820F5F.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1351CE

## ADs that name it (0)

None.

## Approved models (6)

- The Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))
- The Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24))

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